DPW-III DLR-F6 CASE-1 CP Data Form			
----------------------------------			


Date: 3 AUG 2006			


PARTICIPANT INFORMATION			
-----------------------			
               Name:  			Edward N. Tinoco
              Email:  			edward.n.tinoco@boeing.com
              Phone:  			425-234-1147
            Address:  			Boeing Commercial Airplanes
            Address:  			Mail Code 67-LK
            Address:  			P.O. Box 3707
            Address:  			"Seattle, WA 98124"
            Address:  			USA
            Address:  			


SOLVER INFORMATION			
--------------------			
        Method Name:  			CFL3D/Zeus - Thin Layer NS
    Basic Algorithm:  			Finite Volume
   Turbulence Model:  			Spalart-Allmaras
      Miscellaneous:  			


GRID INFORMATION			
--------------------			
Grid-Generator Name:  			BCA-Advancing Front
          Grid Type:  			"Structured Block, Point-to-Point Matched"



VERY FINE GRID SIZE  			WB	WB
----------------------------------------				
              Zones:  			58	58
        Field Nodes:			"30,751,522"	"30,751,522"
        Field Cells:  			"27,185,664"	"27,185,664"
     Boundary Nodes:  			"126,307"	"126,307"
     Boundary Faces:  			"114,208"	"114,208"
   BL 1st-Cell Size:  			y+~0.40	y+~0.40
 BL Max-Growth Rate:  			<1.2 	<1.2 
           BL Cells:  			48	48
      Miscellaneous:  				



CASE 1.A:  SINGLE-POINT GRID CONVERGENCE STUDY - FINE GRID CP AND CF DISTRIBUTIONS						
----------------------------------------------------------------------------------						

WING/BODY						

GRID_SIZE	MACH	ALPHA				
30751522	0.75	-0.152				

WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m) - LOWER SURFACE						
XOC	CP	CFprime				
0.0003	0.9483	0.001130				
0.0005	0.9441	0.001010				
0.0007	0.9317	0.000910				
0.0009	0.9201	0.000990				
0.0012	0.9064	0.001150				
0.0016	0.8905	0.001340
0.0020	0.8717	0.001540
0.0025	0.8499	0.001730
0.0031	0.8255	0.001920
0.0037	0.7988	0.002100
0.0044	0.7700	0.002260
0.0052	0.7396	0.002420
0.0060	0.7078	0.002570
0.0069	0.6750	0.002710
0.0079	0.6413	0.002840
0.0090	0.6072	0.002960
0.0102	0.5726	0.003090
0.0114	0.5377	0.003200
0.0128	0.5029	0.003300
0.0142	0.4688	0.003390
0.0157	0.4356	0.003470
0.0173	0.4028	0.003560
0.0190	0.3708	0.003630
0.0208	0.3397	0.003700
0.0226	0.3096	0.003750
0.0246	0.2806	0.003800
0.0267	0.2528	0.003850
0.0288	0.2262	0.003890
0.0311	0.2007	0.003920
0.0335	0.1764	0.003950
0.0359	0.1532	0.003970
0.0385	0.1311	0.003990
0.0412	0.1102	0.004010
0.0439	0.0904	0.004010
0.0468	0.0718	0.004020
0.0498	0.0544	0.004020
0.0529	0.0379	0.004010
0.0561	0.0223	0.004010
0.0595	0.0073	0.004010
0.0629	-0.0070	0.004000
0.0665	-0.0206	0.004000
0.0701	-0.0334	0.003980
0.0739	-0.0455	0.003970
0.0778	-0.0569	0.003950
0.0819	-0.0676	0.003940
0.0860	-0.0778	0.003930
0.0903	-0.0874	0.003910
0.0948	-0.0966	0.003900
0.0993	-0.1055	0.003880
0.1040	-0.1140	0.003870
0.1088	-0.1221	0.003850
0.1137	-0.1300	0.003840
0.1188	-0.1376	0.003820
0.1240	-0.1449	0.003800
0.1293	-0.1518	0.003780
0.1348	-0.1583	0.003770
0.1404	-0.1642	0.003750
0.1462	-0.1695	0.003720
0.1521	-0.1741	0.003700
0.1581	-0.1779	0.003670
0.1643	-0.1807	0.003640
0.1706	-0.1825	0.003600
0.1771	-0.1834	0.003570
0.1837	-0.1836	0.003530
0.1905	-0.1839	0.003510
0.1973	-0.1846	0.003490
0.2044	-0.1865	0.003480
0.2115	-0.1900	0.003480
0.2189	-0.1954	0.003490
0.2263	-0.2027	0.003510
0.2339	-0.2109	0.003520
0.2416	-0.2178	0.003520
0.2494	-0.2236	0.003520
0.2574	-0.2294	0.003510
0.2655	-0.2343	0.003500
0.2737	-0.2379	0.003480
0.2821	-0.2406	0.003460
0.2905	-0.2425	0.003430
0.2991	-0.2443	0.003420
0.3078	-0.2466	0.003400
0.3167	-0.2569	0.003410
0.3256	-0.2623	0.003430
0.3346	-0.2702	0.003460
0.3437	-0.2794	0.003470
0.3529	-0.2865	0.003460
0.3622	-0.2888	0.003420
0.3716	-0.2873	0.003370
0.3810	-0.2846	0.003330
0.3905	-0.2828	0.003310
0.4001	-0.2834	0.003300
0.4098	-0.2859	0.003300
0.4195	-0.2879	0.003290
0.4293	-0.2889	0.003280
0.4391	-0.2897	0.003260
0.4489	-0.2912	0.003260
0.4588	-0.2947	0.003270
0.4687	-0.3011	0.003310
0.4786	-0.3105	0.003350
0.4886	-0.3212	0.003380
0.4985	-0.3304	0.003400
0.5084	-0.3371	0.003390
0.5183	-0.3402	0.003360
0.5282	-0.3374	0.003290
0.5380	-0.3287	0.003200
0.5478	-0.3151	0.003090
0.5576	-0.2980	0.002980
0.5673	-0.2786	0.002870
0.5770	-0.2580	0.002760
0.5866	-0.2371	0.002660
0.5961	-0.2164	0.002570
0.6056	-0.1958	0.002480
0.6150	-0.1751	0.002390
0.6244	-0.1545	0.002310
0.6337	-0.1344	0.002230
0.6429	-0.1156	0.002170
0.6520	-0.0967	0.002100
0.6611	-0.0776	0.002030
0.6700	-0.0578	0.001950
0.6789	-0.0373	0.001860
0.6876	-0.0161	0.001770
0.6962	0.0059	0.001670
0.7048	0.0281	0.001580
0.7132	0.0501	0.001490
0.7216	0.0713	0.001410
0.7298	0.0913	0.001340
0.7379	0.1101	0.001270
0.7460	0.1273	0.001220
0.7539	0.1428	0.001190
0.7617	0.1563	0.001160
0.7694	0.1678	0.001150
0.7770	0.1773	0.001150
0.7845	0.1852	0.001160
0.7918	0.1917	0.001170
0.7991	0.1972	0.001180
0.8061	0.2019	0.001200
0.8131	0.2061	0.001210
0.8199	0.2099	0.001230
0.8266	0.2135	0.001230
0.8332	0.2169	0.001240
0.8396	0.2202	0.001250
0.8459	0.2232	0.001270
0.8521	0.2256	0.001280
0.8581	0.2276	0.001290
0.8640	0.2293	0.001310
0.8697	0.2308	0.001320
0.8753	0.2321	0.001330
0.8808	0.2331	0.001350
0.8862	0.2340	0.001360
0.8914	0.2345	0.001380
0.8965	0.2348	0.001390
0.9015	0.2348	0.001410
0.9063	0.2345	0.001430
0.9110	0.2339	0.001450
0.9156	0.2330	0.001470
0.9201	0.2318	0.001490
0.9244	0.2303	0.001510
0.9286	0.2286	0.001530
0.9327	0.2267	0.001560
0.9367	0.2247	0.001580
0.9406	0.2227	0.001600
0.9444	0.2206	0.001620
0.9481	0.2186	0.001630
0.9516	0.2166	0.001650
0.9551	0.2146	0.001670
0.9584	0.2126	0.001680
0.9617	0.2106	0.001700
0.9648	0.2085	0.001720
0.9679	0.2064	0.001740
0.9709	0.2040	0.001750
0.9737	0.2015	0.001780
0.9765	0.1987	0.001800
0.9792	0.1955	0.001830
0.9819	0.1919	0.001860
0.9844	0.1877	0.001900
0.9868	0.1827	0.001940
0.9892	0.1767	0.002000
0.9915	0.1693	0.002080
0.9938	0.1597	0.002210
0.9959	0.1470	0.002540
0.9980	0.1281	0.004280
1.0000	0.0986	0.004280
						
WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m) - UPPER SURFACE						
XOC	CP	CFprime				
0.0002	0.9022	0.001240				
0.0001	0.9188	0.000990				
0.0000	0.9316	0.000740				
0.0000	0.9408	0.000490				
0.0000	0.9463	0.000220				
0.0001	0.9489	-0.000060				
0.0002	0.9491	-0.000460				
0.0003	0.8813	0.001500				
0.0003	0.9469	-0.000710				
0.0005	0.8559	0.001790				
0.0008	0.8248	0.002130				
0.0010	0.7849	0.002560				
0.0014	0.7331	0.002960				
0.0018	0.6761	0.003270
0.0024	0.6173	0.003560
0.0030	0.5532	0.003880
0.0037	0.4845	0.004190
0.0045	0.4114	0.004490
0.0055	0.3342	0.004790
0.0065	0.2538	0.005070
0.0076	0.1717	0.005320
0.0089	0.0895	0.005520
0.0103	0.0077	0.005710
0.0117	-0.0732	0.005880
0.0133	-0.1529	0.006030
0.0150	-0.2307	0.006160
0.0168	-0.3061	0.006260
0.0188	-0.3786	0.006340
0.0208	-0.4479	0.006390
0.0230	-0.5126	0.006400
0.0253	-0.5718	0.006380
0.0277	-0.6251	0.006330
0.0302	-0.6724	0.006260
0.0329	-0.7137	0.006180
0.0356	-0.7487	0.006080
0.0385	-0.7778	0.005970
0.0416	-0.8016	0.005860
0.0447	-0.8208	0.005750
0.0480	-0.8364	0.005650
0.0514	-0.8490	0.005540
0.0549	-0.8572	0.005410
0.0585	-0.8615	0.005290
0.0623	-0.8641	0.005190
0.0662	-0.8656	0.005090
0.0702	-0.8658	0.005000
0.0744	-0.8647	0.004910
0.0787	-0.8629	0.004830
0.0831	-0.8606	0.004750
0.0876	-0.8582	0.004680
0.0923	-0.8559	0.004620
0.0971	-0.8540	0.004570
0.1021	-0.8525	0.004520
0.1072	-0.8510	0.004470
0.1124	-0.8494	0.004430
0.1178	-0.8471	0.004370
0.1233	-0.8426	0.004270
0.1289	-0.8288	0.004100
0.1347	-0.8108	0.004020
0.1407	-0.8032	0.004070
0.1468	-0.8075	0.004150
0.1530	-0.8167	0.004180
0.1593	-0.8200	0.004110
0.1659	-0.8137	0.004040
0.1725	-0.8091	0.004030
0.1793	-0.8104	0.004030
0.1863	-0.8094	0.003990
0.1934	-0.8051	0.003940
0.2007	-0.8001	0.003910
0.2080	-0.7984	0.003910
0.2156	-0.8000	0.003910
0.2233	-0.7983	0.003870
0.2311	-0.7921	0.003810
0.2390	-0.7856	0.003790
0.2471	-0.7827	0.003770
0.2554	-0.7763	0.003700
0.2637	-0.7634	0.003620
0.2722	-0.7511	0.003580
0.2809	-0.7406	0.003550
0.2896	-0.7300	0.003500
0.2985	-0.7162	0.003430
0.3075	-0.6993	0.003360
0.3166	-0.6835	0.003330
0.3258	-0.6730	0.003340
0.3351	-0.6662	0.003340
0.3446	-0.6599	0.003340
0.3541	-0.6536	0.003340
0.3637	-0.6478	0.003340
0.3734	-0.6428	0.003340
0.3832	-0.6384	0.003330
0.3930	-0.6329	0.003320
0.4030	-0.6269	0.003310
0.4130	-0.6212	0.003290
0.4230	-0.6156	0.003280
0.4331	-0.6102	0.003270
0.4433	-0.6050	0.003270
0.4535	-0.6001	0.003260
0.4637	-0.5954	0.003250
0.4740	-0.5909	0.003240
0.4843	-0.5867	0.003240
0.4945	-0.5827	0.003230
0.5048	-0.5789	0.003230
0.5151	-0.5753	0.003230
0.5254	-0.5720	0.003220
0.5356	-0.5688	0.003220
0.5459	-0.5656	0.003220
0.5561	-0.5626	0.003210
0.5663	-0.5596	0.003210
0.5764	-0.5565	0.003200
0.5865	-0.5533	0.003200
0.5965	-0.5500	0.003190
0.6064	-0.5464	0.003170
0.6163	-0.5425	0.003160
0.6261	-0.5382	0.003150
0.6359	-0.5336	0.003140
0.6455	-0.5286	0.003120
0.6550	-0.5227	0.003100
0.6645	-0.5157	0.003060
0.6738	-0.5076	0.003030
0.6831	-0.4983	0.002990
0.6922	-0.4879	0.002950
0.7012	-0.4765	0.002900
0.7101	-0.4643	0.002860
0.7189	-0.4515	0.002810
0.7275	-0.4384	0.002760
0.7360	-0.4252	0.002720
0.7444	-0.4122	0.002680
0.7527	-0.3995	0.002640
0.7608	-0.3873	0.002600
0.7688	-0.3760	0.002570
0.7766	-0.3657	0.002550
0.7843	-0.3563	0.002540
0.7919	-0.3476	0.002520
0.7993	-0.3394	0.002500
0.8065	-0.3314	0.002490
0.8137	-0.3236	0.002470
0.8206	-0.3156	0.002450
0.8274	-0.3073	0.002430
0.8341	-0.2987	0.002400
0.8406	-0.2896	0.002370
0.8470	-0.2800	0.002330
0.8532	-0.2699	0.002290
0.8593	-0.2593	0.002240
0.8652	-0.2482	0.002190
0.8710	-0.2367	0.002140
0.8766	-0.2251	0.002090
0.8821	-0.2138	0.002050
0.8874	-0.2027	0.002000
0.8926	-0.1914	0.001940
0.8977	-0.1798	0.001890
0.9026	-0.1680	0.001830
0.9074	-0.1561	0.001770
0.9120	-0.1441	0.001700
0.9165	-0.1320	0.001640
0.9209	-0.1201	0.001580
0.9252	-0.1082	0.001520
0.9293	-0.0966	0.001460
0.9333	-0.0852	0.001400
0.9372	-0.0740	0.001340
0.9410	-0.0631	0.001270
0.9446	-0.0524	0.001220
0.9482	-0.0420	0.001170
0.9516	-0.0320	0.001120
0.9549	-0.0222	0.001060
0.9582	-0.0127	0.001010
0.9613	-0.0034	0.000970
0.9644	0.0055	0.000920
0.9673	0.0143	0.000870
0.9702	0.0228	0.000830
0.9729	0.0312	0.000780
0.9756	0.0394	0.000740
0.9782	0.0475	0.000690
0.9807	0.0554	0.000640
0.9832	0.0633	0.000600
0.9855	0.0710	0.000560				
0.9878	0.0785	0.000520				
0.9900	0.0858	0.000480				
0.9921	0.0928	0.000440				
0.9942	0.0995	0.000440				
0.9962	0.1056	0.000530				
0.9981	0.1121	0.001110				
1.0000	0.1059	0.001110				
						
WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.8144	-0.001940				
0.0000	0.8239	-0.001340				
0.0001	0.8326	-0.000510				
0.0002	0.8367	-0.000130				
0.0004	0.8366	0.000200				
0.0006	0.8315	0.000540
0.0010	0.8208	0.000880
0.0014	0.8049	0.001200
0.0019	0.7846	0.001500
0.0025	0.7601	0.001780
0.0032	0.7317	0.002050
0.0039	0.7001	0.002290
0.0048	0.6659	0.002510
0.0057	0.6298	0.002700
0.0067	0.5927	0.002870
0.0079	0.5551	0.003010
0.0091	0.5174	0.003140
0.0104	0.4798	0.003270
0.0118	0.4424	0.003390
0.0132	0.4053	0.003490
0.0148	0.3691	0.003580
0.0165	0.3351	0.003640
0.0182	0.3029	0.003700
0.0201	0.2713	0.003770
0.0220	0.2408	0.003820
0.0241	0.2117	0.003870
0.0262	0.1840	0.003910
0.0284	0.1579	0.003940
0.0307	0.1332	0.003960
0.0331	0.1099	0.003980
0.0356	0.0881	0.004000
0.0383	0.0675	0.004010
0.0410	0.0481	0.004010
0.0438	0.0299	0.004020
0.0467	0.0126	0.004020
0.0497	-0.0036	0.004020
0.0529	-0.0190	0.004020
0.0561	-0.0335	0.004010
0.0595	-0.0474	0.004010
0.0629	-0.0607	0.004000
0.0665	-0.0733	0.004000
0.0702	-0.0853	0.003990
0.0740	-0.0967	0.003980
0.0780	-0.1075	0.003970
0.0820	-0.1178	0.003960
0.0862	-0.1276	0.003950
0.0905	-0.1371	0.003940
0.0949	-0.1463	0.003930
0.0995	-0.1552	0.003920
0.1041	-0.1639	0.003910
0.1090	-0.1724	0.003900
0.1139	-0.1807	0.003900
0.1190	-0.1889	0.003890
0.1242	-0.1968	0.003880
0.1295	-0.2044	0.003870
0.1350	-0.2117	0.003860
0.1406	-0.2186	0.003850
0.1463	-0.2249	0.003830
0.1522	-0.2306	0.003820
0.1582	-0.2357	0.003790
0.1644	-0.2399	0.003770
0.1707	-0.2436	0.003750
0.1771	-0.2467	0.003730
0.1837	-0.2498	0.003710
0.1904	-0.2531	0.003690
0.1973	-0.2568	0.003680
0.2043	-0.2611	0.003680
0.2115	-0.2662	0.003680
0.2188	-0.2723	0.003690
0.2262	-0.2794	0.003700
0.2338	-0.2875	0.003710
0.2415	-0.2962	0.003730
0.2493	-0.3045	0.003730
0.2572	-0.3110	0.003710
0.2653	-0.3160	0.003700
0.2735	-0.3202	0.003680
0.2818	-0.3239	0.003660
0.2902	-0.3271	0.003650
0.2988	-0.3300	0.003630
0.3075	-0.3328	0.003610
0.3162	-0.3359	0.003600
0.3251	-0.3399	0.003610
0.3341	-0.3461	0.003630
0.3432	-0.3542	0.003640
0.3524	-0.3601	0.003630
0.3616	-0.3615	0.003590
0.3709	-0.3597	0.003540
0.3803	-0.3566	0.003490
0.3898	-0.3540	0.003470
0.3993	-0.3530	0.003460
0.4089	-0.3535	0.003450
0.4186	-0.3534	0.003430
0.4283	-0.3513	0.003400
0.4381	-0.3491	0.003380
0.4479	-0.3481	0.003370
0.4577	-0.3482	0.003360
0.4676	-0.3491	0.003360
0.4774	-0.3504	0.003360
0.4873	-0.3521	0.003370
0.4972	-0.3552	0.003380
0.5071	-0.3562	0.003350
0.5169	-0.3511	0.003290
0.5267	-0.3410	0.003200
0.5364	-0.3271	0.003110
0.5462	-0.3100	0.003000
0.5559	-0.2905	0.002890
0.5655	-0.2693	0.002780
0.5752	-0.2469	0.002670
0.5847	-0.2238	0.002570
0.5942	-0.2006	0.002470
0.6037	-0.1774	0.002370
0.6131	-0.1546	0.002280
0.6225	-0.1325	0.002190
0.6318	-0.1111	0.002110
0.6410	-0.0898	0.002030
0.6501	-0.0684	0.001950
0.6591	-0.0468	0.001860
0.6681	-0.0250	0.001780
0.6769	-0.0031	0.001690
0.6857	0.0188	0.001600
0.6944	0.0405	0.001520
0.7029	0.0620	0.001430
0.7114	0.0832	0.001350
0.7198	0.1041	0.001260
0.7280	0.1248	0.001180
0.7362	0.1446	0.001110
0.7443	0.1625	0.001060
0.7523	0.1787	0.001020
0.7601	0.1931	0.000990
0.7679	0.2059	0.000970
0.7755	0.2173	0.000960
0.7831	0.2274	0.000950
0.7905	0.2361	0.000950
0.7977	0.2437	0.000950
0.8049	0.2502	0.000960
0.8119	0.2561	0.000970
0.8188	0.2613	0.000980
0.8255	0.2659	0.000990
0.8321	0.2699	0.001010
0.8386	0.2734	0.001020
0.8450	0.2763	0.001040
0.8512	0.2788	0.001060
0.8572	0.2809	0.001080
0.8631	0.2825	0.001100
0.8689	0.2837	0.001120
0.8746	0.2846	0.001140
0.8801	0.2851	0.001160
0.8855	0.2852	0.001180
0.8908	0.2851	0.001210
0.8959	0.2847	0.001230
0.9009	0.2841	0.001260
0.9058	0.2832	0.001280
0.9105	0.2821	0.001300
0.9151	0.2808	0.001330
0.9196	0.2794	0.001350
0.9240	0.2777	0.001380
0.9282	0.2758	0.001400
0.9324	0.2738	0.001430
0.9364	0.2716	0.001450
0.9403	0.2694	0.001480
0.9441	0.2672	0.001500
0.9478	0.2649	0.001520
0.9513	0.2625	0.001550
0.9548	0.2601	0.001570
0.9582	0.2577	0.001590
0.9615	0.2551	0.001620
0.9646	0.2524	0.001640
0.9677	0.2496	0.001670
0.9707	0.2465	0.001690
0.9736	0.2432	0.001720
0.9764	0.2396	0.001750
0.9791	0.2357	0.001790
0.9818	0.2313	0.001830
0.9843	0.2264	0.001870
0.9868	0.2207	0.001920
0.9892	0.2141	0.001990
0.9915	0.2063	0.002070
0.9937	0.1965	0.002210
0.9959	0.1839	0.002560
0.9980	0.1662	0.004390
1.0000	0.1424	0.004390
						
WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8130	0.003130				
0.0000	0.7989	0.002550				
0.0001	0.7728	0.001910				
0.0002	0.7495	0.001960				
0.0004	0.7203	0.002250				
0.0006	0.6859	0.002630				
0.0008	0.6440	0.003100				
0.0012	0.5937	0.003590				
0.0015	0.5349	0.003980				
0.0019	0.4742	0.004230				
0.0025	0.4158	0.004440				
0.0030	0.3561	0.004700				
0.0037	0.2928	0.004980				
0.0044	0.2259	0.005270
0.0052	0.1565	0.005530
0.0060	0.0865	0.005720
0.0069	0.0181	0.005880
0.0079	-0.0494	0.006050
0.0090	-0.1183	0.006230
0.0101	-0.1880	0.006380
0.0113	-0.2568	0.006510
0.0126	-0.3243	0.006610
0.0139	-0.3903	0.006690
0.0154	-0.4551	0.006770
0.0169	-0.5193	0.006850
0.0185	-0.5843	0.006950
0.0202	-0.6516	0.007080
0.0220	-0.7223	0.007210
0.0239	-0.7940	0.007260
0.0259	-0.8595	0.007180
0.0280	-0.9154	0.007040
0.0302	-0.9638	0.006910
0.0325	-1.0057	0.006780
0.0349	-1.0418	0.006640
0.0375	-1.0725	0.006510
0.0402	-1.0984	0.006390
0.0430	-1.1203	0.006270
0.0460	-1.1391	0.006170
0.0490	-1.1562	0.006100
0.0522	-1.1731	0.006030
0.0556	-1.1884	0.005940
0.0590	-1.1999	0.005840
0.0626	-1.2086	0.005750
0.0664	-1.2159	0.005670
0.0702	-1.2217	0.005590
0.0742	-1.2260	0.005510
0.0784	-1.2290	0.005440
0.0826	-1.2306	0.005370
0.0871	-1.2310	0.005300
0.0916	-1.2301	0.005230
0.0963	-1.2280	0.005170
0.1011	-1.2249	0.005100
0.1061	-1.2206	0.005040
0.1112	-1.2148	0.004960
0.1165	-1.2068	0.004880
0.1219	-1.1953	0.004780
0.1275	-1.1784	0.004660
0.1332	-1.1555	0.004520
0.1390	-1.1277	0.004360
0.1450	-1.0970	0.004190
0.1512	-1.0655	0.004030
0.1575	-1.0340	0.003880
0.1639	-1.0019	0.003730
0.1705	-0.9722	0.003650
0.1773	-0.9501	0.003670
0.1842	-0.9386	0.003750
0.1912	-0.9322	0.003820
0.1984	-0.9246	0.003860
0.2057	-0.9160	0.003850
0.2132	-0.9027	0.003800
0.2208	-0.8864	0.003750
0.2286	-0.8733	0.003710
0.2365	-0.8575	0.003620
0.2446	-0.8304	0.003430
0.2527	-0.7903	0.003140
0.2611	-0.7412	0.002920
0.2695	-0.6969	0.002940
0.2781	-0.6749	0.003090
0.2868	-0.6711	0.003210
0.2957	-0.6702	0.003290
0.3047	-0.6677	0.003320
0.3137	-0.6636	0.003350
0.3230	-0.6610	0.003380
0.3323	-0.6608	0.003420
0.3417	-0.6605	0.003450
0.3512	-0.6594	0.003460
0.3608	-0.6575	0.003460
0.3705	-0.6552	0.003460
0.3803	-0.6527	0.003460
0.3901	-0.6500	0.003460
0.4001	-0.6471	0.003450
0.4101	-0.6440	0.003440
0.4202	-0.6408	0.003430
0.4303	-0.6375	0.003420
0.4404	-0.6342	0.003410
0.4506	-0.6309	0.003400
0.4609	-0.6276	0.003390
0.4712	-0.6244	0.003380
0.4814	-0.6213	0.003370
0.4918	-0.6184	0.003360
0.5021	-0.6154	0.003350
0.5124	-0.6126	0.003340
0.5227	-0.6097	0.003330
0.5330	-0.6069	0.003320
0.5432	-0.6041	0.003310
0.5535	-0.6011	0.003300
0.5637	-0.5981	0.003290
0.5738	-0.5949	0.003280
0.5839	-0.5914	0.003260
0.5940	-0.5876	0.003250
0.6040	-0.5834	0.003230
0.6139	-0.5787	0.003210
0.6238	-0.5735	0.003180
0.6335	-0.5674	0.003150
0.6432	-0.5600	0.003110
0.6528	-0.5513	0.003070
0.6623	-0.5418	0.003030
0.6717	-0.5314	0.002980
0.6809	-0.5200	0.002930
0.6901	-0.5078	0.002870
0.6991	-0.4946	0.002820
0.7081	-0.4806	0.002750
0.7169	-0.4660	0.002690
0.7256	-0.4511	0.002630
0.7341	-0.4364	0.002580
0.7426	-0.4225	0.002540
0.7508	-0.4095	0.002500
0.7590	-0.3968	0.002460
0.7670	-0.3844	0.002420
0.7749	-0.3731	0.002390
0.7826	-0.3625	0.002360
0.7902	-0.3527	0.002340
0.7977	-0.3435	0.002320
0.8050	-0.3345	0.002290
0.8121	-0.3256	0.002270
0.8192	-0.3165	0.002240
0.8260	-0.3071	0.002210
0.8327	-0.2973	0.002170
0.8393	-0.2869	0.002130
0.8457	-0.2758	0.002080
0.8519	-0.2642	0.002030
0.8580	-0.2519	0.001980
0.8640	-0.2392	0.001920
0.8698	-0.2260	0.001850
0.8755	-0.2125	0.001790
0.8810	-0.1988	0.001730
0.8864	-0.1848	0.001660
0.8916	-0.1704	0.001600
0.8967	-0.1558	0.001520
0.9016	-0.1408	0.001450
0.9065	-0.1258	0.001380
0.9111	-0.1107	0.001300
0.9157	-0.0956	0.001230
0.9201	-0.0807	0.001150
0.9244	-0.0659	0.001080
0.9286	-0.0515	0.001000
0.9326	-0.0375	0.000930
0.9365	-0.0238	0.000860
0.9403	-0.0106	0.000800
0.9440	0.0021	0.000740
0.9476	0.0143	0.000680
0.9511	0.0260	0.000630
0.9545	0.0371	0.000570
0.9578	0.0477	0.000530
0.9609	0.0578	0.000480
0.9640	0.0673	0.000440
0.9670	0.0763	0.000400
0.9699	0.0848	0.000360
0.9727	0.0929	0.000320
0.9754	0.1006	0.000290
0.9780	0.1078	0.000260
0.9805	0.1146	0.000230
0.9830	0.1211	0.000200
0.9854	0.1271	0.000180				
0.9877	0.1329	0.000150				
0.9899	0.1382	0.000130				
0.9921	0.1433	0.000130				
0.9941	0.1480	0.000150				
0.9962	0.1520	0.000240				
0.9981	0.1569	0.000640				
1.0000	0.1507	0.000640				
						
WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.7838	-0.002100				
0.0000	0.7983	-0.001330				
0.0002	0.8069	-0.000240				
0.0004	0.8063	0.000350				
0.0007	0.7985	0.000850				
0.0010	0.7826	0.001350
0.0015	0.7597	0.001800
0.0021	0.7309	0.002200
0.0028	0.6977	0.002550
0.0035	0.6611	0.002840
0.0043	0.6223	0.003080
0.0052	0.5822	0.003280
0.0062	0.5416	0.003440
0.0073	0.5012	0.003580
0.0084	0.4614	0.003690
0.0096	0.4226	0.003780
0.0109	0.3852	0.003860
0.0123	0.3495	0.003920
0.0137	0.3156	0.003950
0.0153	0.2835	0.003980
0.0169	0.2533	0.004010
0.0186	0.2247	0.004050
0.0203	0.1971	0.004080
0.0222	0.1709	0.004100
0.0241	0.1469	0.004110
0.0262	0.1247	0.004100
0.0283	0.1042	0.004090
0.0305	0.0852	0.004090
0.0328	0.0676	0.004090
0.0352	0.0512	0.004080
0.0377	0.0357	0.004070
0.0403	0.0212	0.004060
0.0430	0.0074	0.004050
0.0458	-0.0056	0.004050
0.0487	-0.0179	0.004040
0.0517	-0.0295	0.004030
0.0549	-0.0404	0.004010
0.0581	-0.0505	0.003990
0.0614	-0.0599	0.003980
0.0649	-0.0689	0.003970
0.0684	-0.0778	0.003960
0.0721	-0.0868	0.003950
0.0759	-0.0956	0.003950
0.0798	-0.1041	0.003940
0.0839	-0.1125	0.003930
0.0880	-0.1207	0.003930
0.0923	-0.1288	0.003920
0.0967	-0.1368	0.003920
0.1012	-0.1446	0.003910
0.1059	-0.1525	0.003910
0.1107	-0.1603	0.003910
0.1156	-0.1681	0.003900
0.1206	-0.1760	0.003900
0.1258	-0.1838	0.003900
0.1311	-0.1916	0.003900
0.1365	-0.1994	0.003900
0.1421	-0.2070	0.003900
0.1478	-0.2145	0.003890
0.1536	-0.2218	0.003890
0.1596	-0.2288	0.003880
0.1657	-0.2354	0.003880
0.1719	-0.2417	0.003870
0.1783	-0.2476	0.003860
0.1848	-0.2535	0.003850
0.1915	-0.2596	0.003850
0.1983	-0.2660	0.003850
0.2053	-0.2728	0.003850
0.2124	-0.2802	0.003860
0.2196	-0.2881	0.003870
0.2270	-0.2965	0.003880
0.2345	-0.3053	0.003890
0.2421	-0.3140	0.003890
0.2498	-0.3219	0.003900
0.2577	-0.3291	0.003890
0.2656	-0.3361	0.003890
0.2737	-0.3420	0.003870
0.2820	-0.3466	0.003850
0.2903	-0.3503	0.003830
0.2988	-0.3534	0.003810
0.3074	-0.3564	0.003800
0.3161	-0.3599	0.003790
0.3249	-0.3640	0.003790
0.3338	-0.3682	0.003780
0.3427	-0.3712	0.003750
0.3518	-0.3725	0.003720
0.3609	-0.3727	0.003690
0.3701	-0.3718	0.003660
0.3794	-0.3700	0.003630
0.3888	-0.3673	0.003590
0.3982	-0.3642	0.003560
0.4077	-0.3607	0.003520
0.4173	-0.3570	0.003490
0.4269	-0.3530	0.003460
0.4366	-0.3488	0.003430
0.4463	-0.3441	0.003390
0.4560	-0.3390	0.003360
0.4658	-0.3337	0.003330
0.4755	-0.3282	0.003300
0.4853	-0.3225	0.003260
0.4951	-0.3164	0.003220
0.5049	-0.3089	0.003180
0.5146	-0.2993	0.003120
0.5243	-0.2871	0.003040
0.5340	-0.2725	0.002960
0.5436	-0.2559	0.002880
0.5533	-0.2377	0.002790
0.5629	-0.2185	0.002690
0.5724	-0.1987	0.002600
0.5820	-0.1787	0.002520
0.5914	-0.1587	0.002430
0.6009	-0.1387	0.002350
0.6103	-0.1187	0.002270
0.6196	-0.0984	0.002190
0.6288	-0.0780	0.002110
0.6380	-0.0580	0.002030
0.6472	-0.0380	0.001950
0.6562	-0.0181	0.001870
0.6652	0.0018	0.001790
0.6740	0.0216	0.001710
0.6828	0.0415	0.001630
0.6915	0.0612	0.001550
0.7001	0.0809	0.001480
0.7086	0.1006	0.001400
0.7170	0.1202	0.001310
0.7254	0.1397	0.001230
0.7336	0.1584	0.001160
0.7417	0.1762	0.001090
0.7498	0.1927	0.001040
0.7577	0.2081	0.001000
0.7655	0.2222	0.000960
0.7733	0.2350	0.000930
0.7809	0.2467	0.000900
0.7884	0.2572	0.000890
0.7958	0.2665	0.000880
0.8030	0.2747	0.000870
0.8101	0.2818	0.000880
0.8171	0.2879	0.000890
0.8239	0.2931	0.000900
0.8306	0.2974	0.000920
0.8372	0.3009	0.000940
0.8436	0.3036	0.000970
0.8499	0.3055	0.000990
0.8560	0.3068	0.001030
0.8620	0.3075	0.001060
0.8679	0.3076	0.001090
0.8736	0.3073	0.001120
0.8792	0.3064	0.001160
0.8846	0.3052	0.001190
0.8900	0.3037	0.001230
0.8951	0.3018	0.001260
0.9002	0.2997	0.001300
0.9051	0.2974	0.001330
0.9099	0.2950	0.001370
0.9145	0.2923	0.001400
0.9190	0.2896	0.001440
0.9234	0.2867	0.001470
0.9277	0.2837	0.001500
0.9319	0.2806	0.001530
0.9359	0.2773	0.001560
0.9399	0.2741	0.001590
0.9437	0.2707	0.001620
0.9474	0.2672	0.001650
0.9510	0.2637	0.001680
0.9545	0.2600	0.001710
0.9579	0.2562	0.001750
0.9612	0.2523	0.001780
0.9644	0.2482	0.001820
0.9675	0.2439	0.001850
0.9705	0.2394	0.001890
0.9734	0.2346	0.001930
0.9762	0.2295	0.001970
0.9790	0.2241	0.002020
0.9816	0.2182	0.002060
0.9842	0.2118	0.002120
0.9867	0.2047	0.002180
0.9891	0.1967	0.002250
0.9914	0.1875	0.002350
0.9937	0.1763	0.002510
0.9959	0.1624	0.002890
0.9980	0.1436	0.004890
1.0000	0.1211	0.004890
						
WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7828	0.003790				
0.0000	0.7618	0.003310				
0.0002	0.7183	0.002800				
0.0003	0.6787	0.003010				
0.0006	0.6296	0.003510				
0.0009	0.5738	0.004020				
0.0013	0.5126	0.004460				
0.0018	0.4487	0.004810				
0.0023	0.3848	0.005050				
0.0029	0.3222	0.005260				
0.0035	0.2599	0.005450				
0.0042	0.1975	0.005660				
0.0050	0.1351	0.005850				
0.0058	0.0728	0.006020
0.0067	0.0108	0.006160
0.0076	-0.0506	0.006290
0.0086	-0.1115	0.006420
0.0096	-0.1729	0.006550
0.0107	-0.2346	0.006670
0.0119	-0.2955	0.006770
0.0131	-0.3555	0.006860
0.0144	-0.4147	0.006940
0.0158	-0.4735	0.007020
0.0172	-0.5329	0.007120
0.0187	-0.5942	0.007250
0.0203	-0.6593	0.007430
0.0219	-0.7303	0.007670
0.0236	-0.8089	0.007940
0.0254	-0.8929	0.008070
0.0271	-0.9695	0.007880
0.0290	-1.0277	0.007500
0.0311	-1.0690	0.007150
0.0333	-1.0976	0.006840
0.0357	-1.1173	0.006610
0.0381	-1.1315	0.006440
0.0407	-1.1433	0.006330
0.0435	-1.1548	0.006260
0.0463	-1.1669	0.006200
0.0492	-1.1786	0.006120
0.0523	-1.1867	0.005970
0.0556	-1.1889	0.005850
0.0590	-1.1912	0.005810
0.0625	-1.1965	0.005780
0.0662	-1.2010	0.005720
0.0699	-1.2045	0.005660
0.0738	-1.2068	0.005590
0.0779	-1.2080	0.005520
0.0821	-1.2082	0.005460
0.0864	-1.2074	0.005400
0.0909	-1.2060	0.005340
0.0955	-1.2042	0.005290
0.1003	-1.2023	0.005240
0.1052	-1.2003	0.005190
0.1103	-1.1980	0.005150
0.1155	-1.1950	0.005100
0.1208	-1.1912	0.005050
0.1263	-1.1875	0.005020
0.1319	-1.1837	0.004970
0.1377	-1.1789	0.004920
0.1436	-1.1734	0.004880
0.1497	-1.1673	0.004830
0.1560	-1.1608	0.004790
0.1624	-1.1538	0.004740
0.1689	-1.1464	0.004700
0.1756	-1.1384	0.004650
0.1824	-1.1293	0.004600
0.1894	-1.1178	0.004510
0.1965	-1.0980	0.004290
0.2038	-1.0515	0.003620
0.2112	-0.9431	0.002380
0.2188	-0.7981	0.001410
0.2265	-0.6738	0.001490
0.2344	-0.6126	0.002020
0.2424	-0.6061	0.002430
0.2506	-0.6101	0.002760
0.2588	-0.6188	0.003030
0.2673	-0.6297	0.003240
0.2758	-0.6414	0.003420
0.2845	-0.6531	0.003550
0.2933	-0.6643	0.003650
0.3023	-0.6745	0.003730
0.3113	-0.6838	0.003790
0.3205	-0.6922	0.003840
0.3298	-0.6997	0.003870
0.3391	-0.7061	0.003890
0.3486	-0.7114	0.003900
0.3582	-0.7156	0.003900
0.3679	-0.7185	0.003900
0.3777	-0.7203	0.003890
0.3875	-0.7214	0.003880
0.3974	-0.7217	0.003860
0.4074	-0.7213	0.003850
0.4175	-0.7204	0.003830
0.4276	-0.7190	0.003810
0.4377	-0.7173	0.003790
0.4480	-0.7154	0.003770
0.4582	-0.7134	0.003760
0.4685	-0.7114	0.003740
0.4788	-0.7096	0.003730
0.4891	-0.7078	0.003720
0.4994	-0.7063	0.003710
0.5097	-0.7050	0.003700
0.5200	-0.7039	0.003690
0.5303	-0.7031	0.003680
0.5406	-0.7024	0.003680
0.5508	-0.7019	0.003670
0.5611	-0.7015	0.003670
0.5712	-0.7012	0.003660
0.5814	-0.7007	0.003650
0.5915	-0.6997	0.003630
0.6015	-0.6977	0.003610
0.6114	-0.6942	0.003580
0.6213	-0.6884	0.003530
0.6311	-0.6802	0.003480
0.6408	-0.6704	0.003420
0.6504	-0.6596	0.003360
0.6599	-0.6467	0.003280
0.6693	-0.6316	0.003200
0.6786	-0.6148	0.003110
0.6878	-0.5968	0.003020
0.6969	-0.5779	0.002930
0.7059	-0.5585	0.002840
0.7147	-0.5388	0.002760
0.7234	-0.5192	0.002680
0.7320	-0.5000	0.002610
0.7405	-0.4815	0.002540
0.7488	-0.4639	0.002480
0.7570	-0.4468	0.002420
0.7651	-0.4302	0.002370
0.7730	-0.4141	0.002310
0.7808	-0.3985	0.002260
0.7884	-0.3834	0.002210
0.7959	-0.3686	0.002160
0.8032	-0.3542	0.002120
0.8104	-0.3400	0.002070
0.8175	-0.3261	0.002020
0.8244	-0.3123	0.001970
0.8311	-0.2986	0.001930
0.8377	-0.2849	0.001880
0.8442	-0.2712	0.001830
0.8505	-0.2575	0.001770
0.8566	-0.2436	0.001720
0.8626	-0.2296	0.001660
0.8685	-0.2155	0.001600
0.8742	-0.2011	0.001540
0.8797	-0.1869	0.001480
0.8852	-0.1731	0.001420
0.8904	-0.1593	0.001360
0.8956	-0.1456	0.001300
0.9006	-0.1320	0.001240
0.9054	-0.1184	0.001180
0.9102	-0.1049	0.001120
0.9148	-0.0917	0.001060
0.9192	-0.0786	0.001000
0.9236	-0.0658	0.000930
0.9278	-0.0532	0.000880
0.9319	-0.0410	0.000820
0.9358	-0.0292	0.000760
0.9397	-0.0178	0.000710
0.9434	-0.0067	0.000660
0.9471	0.0040	0.000610
0.9506	0.0142	0.000560
0.9540	0.0240	0.000510
0.9573	0.0334	0.000470
0.9605	0.0424	0.000430
0.9636	0.0509	0.000390
0.9666	0.0591	0.000350
0.9695	0.0668	0.000320
0.9724	0.0742	0.000280
0.9751	0.0812	0.000250
0.9778	0.0878	0.000220
0.9803	0.0941	0.000200
0.9828	0.1000	0.000170
0.9852	0.1056	0.000150				
0.9876	0.1108	0.000130				
0.9898	0.1157	0.000110				
0.9920	0.1204	0.000110				
0.9941	0.1248	0.000140				
0.9961	0.1285	0.000240				
0.9981	0.1333	0.000670				
1.0000	0.1279	0.000670				
						
WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.7810	-0.002060				
0.0001	0.8006	-0.001200				
0.0002	0.8072	0.000070				
0.0005	0.7993	0.000800				
0.0009	0.7824	0.001410				
0.0014	0.7564	0.001950
0.0020	0.7241	0.002420
0.0026	0.6867	0.002830
0.0034	0.6458	0.003160
0.0042	0.6030	0.003430
0.0051	0.5597	0.003620
0.0060	0.5171	0.003770
0.0070	0.4755	0.003880
0.0081	0.4353	0.003970
0.0093	0.3965	0.004040
0.0105	0.3593	0.004090
0.0118	0.3239	0.004130
0.0132	0.2906	0.004160
0.0146	0.2427	0.004260
0.0161	0.2154	0.004250
0.0177	0.1906	0.004230
0.0194	0.1681	0.004200
0.0211	0.1473	0.004200
0.0230	0.1270	0.004210
0.0249	0.1078	0.004200
0.0269	0.0906	0.004180
0.0290	0.0751	0.004150
0.0312	0.0612	0.004130
0.0334	0.0485	0.004100
0.0358	0.0369	0.004080
0.0383	0.0262	0.004060
0.0409	0.0163	0.004040
0.0436	0.0070	0.004020
0.0464	-0.0019	0.004000
0.0493	-0.0104	0.003990
0.0523	-0.0185	0.003980
0.0554	-0.0264	0.003960
0.0586	-0.0340	0.003950
0.0619	-0.0413	0.003930
0.0654	-0.0482	0.003920
0.0690	-0.0551	0.003910
0.0726	-0.0620	0.003900
0.0764	-0.0689	0.003900
0.0804	-0.0759	0.003890
0.0844	-0.0829	0.003880
0.0886	-0.0899	0.003880
0.0928	-0.0970	0.003880
0.0973	-0.1043	0.003880
0.1018	-0.1118	0.003880
0.1064	-0.1194	0.003880
0.1112	-0.1272	0.003880
0.1161	-0.1351	0.003890
0.1212	-0.1433	0.003890
0.1263	-0.1515	0.003900
0.1316	-0.1599	0.003900
0.1371	-0.1683	0.003910
0.1426	-0.1767	0.003910
0.1483	-0.1851	0.003910
0.1541	-0.1933	0.003910
0.1601	-0.2014	0.003920
0.1662	-0.2093	0.003920
0.1724	-0.2172	0.003920
0.1788	-0.2252	0.003920
0.1853	-0.2335	0.003920
0.1919	-0.2418	0.003930
0.1987	-0.2508	0.003940
0.2056	-0.2599	0.003960
0.2126	-0.2687	0.003960
0.2198	-0.2775	0.003970
0.2271	-0.2866	0.003980
0.2346	-0.2959	0.003990
0.2421	-0.3054	0.003990
0.2498	-0.3147	0.004000
0.2576	-0.3232	0.003990
0.2655	-0.3309	0.003980
0.2736	-0.3377	0.003970
0.2817	-0.3435	0.003950
0.2900	-0.3483	0.003940
0.2984	-0.3526	0.003920
0.3070	-0.3564	0.003900
0.3156	-0.3601	0.003880
0.3243	-0.3637	0.003870
0.3331	-0.3667	0.003840
0.3420	-0.3684	0.003810
0.3510	-0.3684	0.003780
0.3601	-0.3677	0.003750
0.3693	-0.3667	0.003720
0.3785	-0.3652	0.003690
0.3878	-0.3631	0.003660
0.3972	-0.3604	0.003620
0.4066	-0.3569	0.003580
0.4161	-0.3523	0.003540
0.4256	-0.3467	0.003500
0.4352	-0.3410	0.003460
0.4448	-0.3352	0.003410
0.4545	-0.3286	0.003370
0.4642	-0.3210	0.003320
0.4739	-0.3122	0.003260
0.4836	-0.3025	0.003210
0.4933	-0.2918	0.003150
0.5031	-0.2804	0.003080
0.5128	-0.2680	0.003010
0.5224	-0.2540	0.002920
0.5321	-0.2393	0.002820
0.5417	-0.2224	0.002770
0.5514	-0.2078	0.002750
0.5609	-0.1935	0.002680
0.5705	-0.1762	0.002600
0.5800	-0.1595	0.002530
0.5895	-0.1423	0.002460
0.5989	-0.1249	0.002390
0.6083	-0.1073	0.002310
0.6176	-0.0894	0.002240
0.6268	-0.0714	0.002160
0.6360	-0.0536	0.002090
0.6452	-0.0356	0.002020
0.6542	-0.0172	0.001940
0.6632	0.0014	0.001860
0.6721	0.0201	0.001780
0.6809	0.0388	0.001700
0.6896	0.0573	0.001630
0.6983	0.0757	0.001550
0.7068	0.0939	0.001470
0.7152	0.1121	0.001390
0.7236	0.1305	0.001310
0.7318	0.1490	0.001230
0.7400	0.1671	0.001160
0.7481	0.1843	0.001090
0.7560	0.2007	0.001040
0.7639	0.2212	0.000980
0.7717	0.2349	0.000940
0.7794	0.2475	0.000910
0.7869	0.2591	0.000880
0.7944	0.2694	0.000870
0.8017	0.2785	0.000860
0.8089	0.2866	0.000860
0.8159	0.2935	0.000870
0.8228	0.2994	0.000880
0.8296	0.3042	0.000900
0.8362	0.3080	0.000920
0.8427	0.3108	0.000950
0.8491	0.3128	0.000980
0.8553	0.3139	0.001020
0.8613	0.3144	0.001060
0.8672	0.3142	0.001090
0.8730	0.3134	0.001130
0.8786	0.3121	0.001170
0.8841	0.3104	0.001210
0.8894	0.3082	0.001260
0.8946	0.3057	0.001300
0.8997	0.3030	0.001340
0.9046	0.3001	0.001370
0.9094	0.2970	0.001410
0.9141	0.2938	0.001450
0.9187	0.2905	0.001490
0.9231	0.2871	0.001520
0.9274	0.2835	0.001560
0.9316	0.2799	0.001590
0.9356	0.2762	0.001630
0.9396	0.2724	0.001660
0.9434	0.2684	0.001690
0.9472	0.2644	0.001730
0.9508	0.2603	0.001760
0.9543	0.2560	0.001800
0.9577	0.2515	0.001840
0.9610	0.2468	0.001880
0.9642	0.2419	0.001920
0.9673	0.2368	0.001960
0.9704	0.2314	0.002000
0.9733	0.2257	0.002040
0.9761	0.2197	0.002090
0.9789	0.2132	0.002140
0.9815	0.2064	0.002200
0.9841	0.1990	0.002260
0.9866	0.1909	0.002330
0.9890	0.1819	0.002400
0.9914	0.1717	0.002510
0.9936	0.1596	0.002670
0.9958	0.1447	0.003070
0.9980	0.1250	0.005160
1.0000	0.1030	0.005160
						
WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7800	0.004120				
0.0001	0.7541	0.003750				
0.0002	0.6958	0.003380				
0.0005	0.6440	0.003650				
0.0008	0.5840	0.004150				
0.0012	0.5212	0.004570				
0.0017	0.4583	0.004930				
0.0023	0.3935	0.005240				
0.0029	0.3291	0.005440				
0.0036	0.2689	0.005580				
0.0043	0.2099	0.005730				
0.0051	0.1512	0.005890				
0.0059	0.0927	0.006060				
0.0067	0.0342	0.006210
0.0076	-0.0241	0.006340
0.0086	-0.0820	0.006460
0.0096	-0.1394	0.006570
0.0106	-0.1969	0.006680
0.0118	-0.2542	0.006780
0.0129	-0.3108	0.006860
0.0142	-0.3671	0.006940
0.0155	-0.4236	0.007040
0.0168	-0.4812	0.007150
0.0183	-0.5413	0.007300
0.0198	-0.6055	0.007500
0.0213	-0.6758	0.007760
0.0229	-0.7537	0.008080
0.0245	-0.8390	0.008380
0.0260	-0.9247	0.008350
0.0277	-0.9958	0.007990
0.0296	-1.0465	0.007550
0.0316	-1.0820	0.007160
0.0337	-1.1054	0.006840
0.0360	-1.1199	0.006590
0.0384	-1.1284	0.006400
0.0410	-1.1338	0.006270
0.0437	-1.1385	0.006190
0.0465	-1.1436	0.006120
0.0494	-1.1485	0.006030
0.0524	-1.1504	0.005900
0.0557	-1.1464	0.005780
0.0591	-1.1427	0.005740
0.0625	-1.1433	0.005720
0.0661	-1.1441	0.005670
0.0699	-1.1442	0.005610
0.0738	-1.1432	0.005550
0.0778	-1.1410	0.005480
0.0820	-1.1377	0.005410
0.0863	-1.1333	0.005350
0.0908	-1.1283	0.005290
0.0954	-1.1234	0.005250
0.1001	-1.1187	0.005210
0.1050	-1.1145	0.005170
0.1100	-1.1106	0.005130
0.1151	-1.1064	0.005090
0.1205	-1.1019	0.005060
0.1259	-1.0985	0.005030
0.1315	-1.0959	0.005010
0.1373	-1.0921	0.004960
0.1432	-1.0872	0.004920
0.1492	-1.0815	0.004870
0.1554	-1.0754	0.004830
0.1618	-1.0693	0.004790
0.1683	-1.0630	0.004750
0.1750	-1.0552	0.004700
0.1818	-1.0456	0.004620
0.1887	-1.0316	0.004460
0.1958	-1.0010	0.004000
0.2031	-0.9206	0.002990
0.2105	-0.7987	0.001980
0.2180	-0.6732	0.001950
0.2257	-0.6059	0.002510
0.2336	-0.6058	0.002930
0.2415	-0.6171	0.003240
0.2497	-0.6320	0.003490
0.2579	-0.6487	0.003680
0.2663	-0.6650	0.003820
0.2748	-0.6802	0.003920
0.2835	-0.6943	0.004000
0.2923	-0.7070	0.004060
0.3012	-0.7182	0.004100
0.3102	-0.7279	0.004130
0.3194	-0.7364	0.004140
0.3286	-0.7437	0.004150
0.3380	-0.7496	0.004150
0.3474	-0.7538	0.004140
0.3570	-0.7564	0.004120
0.3667	-0.7579	0.004100
0.3764	-0.7589	0.004090
0.3862	-0.7595	0.004070
0.3961	-0.7596	0.004050
0.4061	-0.7593	0.004030
0.4162	-0.7587	0.004010
0.4262	-0.7578	0.003990
0.4364	-0.7568	0.003980
0.4466	-0.7557	0.003960
0.4568	-0.7545	0.003940
0.4671	-0.7534	0.003930
0.4773	-0.7525	0.003920
0.4876	-0.7517	0.003910
0.4980	-0.7512	0.003900
0.5083	-0.7509	0.003890
0.5186	-0.7510	0.003880
0.5289	-0.7516	0.003880
0.5392	-0.7527	0.003880
0.5494	-0.7544	0.003890
0.5596	-0.7566	0.003890
0.5698	-0.7594	0.003900
0.5799	-0.7626	0.003900
0.5900	-0.7658	0.003910
0.6000	-0.7687	0.003910
0.6100	-0.7707	0.003900
0.6198	-0.7708	0.003870
0.6296	-0.7675	0.003830
0.6394	-0.7608	0.003760
0.6490	-0.7499	0.003660
0.6585	-0.7327	0.003520
0.6679	-0.7095	0.003340
0.6772	-0.6830	0.003200
0.6864	-0.6592	0.003120
0.6955	-0.6390	0.003050
0.7045	-0.6179	0.002960
0.7134	-0.5959	0.002860
0.7221	-0.5743	0.002780
0.7307	-0.5530	0.002700
0.7392	-0.5325	0.002620
0.7475	-0.5130	0.002560
0.7558	-0.4939	0.002490
0.7638	-0.4749	0.002420
0.7718	-0.4563	0.002350
0.7796	-0.4381	0.002290
0.7872	-0.4203	0.002230
0.7947	-0.4030	0.002170
0.8021	-0.3862	0.002110
0.8093	-0.3697	0.002060
0.8164	-0.3535	0.002000
0.8233	-0.3377	0.001950
0.8301	-0.3222	0.001890
0.8367	-0.3068	0.001840
0.8432	-0.2917	0.001780
0.8495	-0.2768	0.001730
0.8557	-0.2620	0.001670
0.8617	-0.2473	0.001620
0.8676	-0.2327	0.001560
0.8734	-0.2182	0.001500
0.8790	-0.2039	0.001450
0.8844	-0.1900	0.001390
0.8897	-0.1763	0.001340
0.8949	-0.1628	0.001280
0.8999	-0.1494	0.001230
0.9048	-0.1362	0.001170
0.9096	-0.1232	0.001110
0.9142	-0.1104	0.001060
0.9187	-0.0978	0.001000
0.9231	-0.0855	0.000950
0.9273	-0.0735	0.000890
0.9314	-0.0617	0.000840
0.9354	-0.0503	0.000780
0.9393	-0.0391	0.000730
0.9431	-0.0283	0.000680
0.9467	-0.0179	0.000630
0.9503	-0.0078	0.000590
0.9537	0.0020	0.000540
0.9570	0.0113	0.000500
0.9603	0.0204	0.000450
0.9634	0.0290	0.000410
0.9664	0.0373	0.000370
0.9694	0.0453	0.000340
0.9722	0.0529	0.000300
0.9750	0.0601	0.000270
0.9776	0.0670	0.000240
0.9802	0.0736	0.000210
0.9827	0.0798	0.000180
0.9851	0.0856	0.000150				
0.9875	0.0912	0.000130				
0.9897	0.0963	0.000110				
0.9919	0.1012	0.000110				
0.9940	0.1059	0.000140				
0.9961	0.1099	0.000240				
0.9981	0.1150	0.000700				
1.0000	0.1101	0.000700				
						
WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.7946	-0.002120				
0.0000	0.8206	-0.001110				
0.0002	0.8264	0.000420				
0.0005	0.8125	0.001290				
0.0009	0.7879	0.001990				
0.0014	0.7539	0.002600
0.0020	0.7136	0.003110
0.0027	0.6692	0.003510
0.0035	0.6230	0.003800
0.0043	0.5764	0.004020
0.0052	0.5306	0.004180
0.0062	0.4864	0.004280
0.0072	0.4442	0.004340
0.0083	0.4043	0.004380
0.0094	0.3668	0.004390
0.0106	0.3316	0.004390
0.0119	0.2987	0.004390
0.0133	0.2680	0.004380
0.0147	0.2394	0.004370
0.0162	0.2129	0.004350
0.0178	0.1891	0.004290
0.0194	0.1684	0.004250
0.0212	0.1490	0.004240
0.0230	0.1301	0.004230
0.0249	0.1126	0.004210
0.0269	0.0965	0.004190
0.0290	0.0821	0.004160
0.0312	0.0690	0.004130
0.0335	0.0573	0.004100
0.0358	0.0467	0.004070
0.0383	0.0371	0.004040
0.0409	0.0283	0.004020
0.0436	0.0201	0.003990
0.0464	0.0124	0.003970
0.0493	0.0050	0.003960
0.0523	-0.0023	0.003940
0.0555	-0.0095	0.003930
0.0587	-0.0166	0.003920
0.0621	-0.0238	0.003910
0.0656	-0.0309	0.003910
0.0692	-0.0380	0.003900
0.0729	-0.0448	0.003890
0.0767	-0.0514	0.003870
0.0807	-0.0578	0.003860
0.0847	-0.0640	0.003850
0.0890	-0.0705	0.003850
0.0933	-0.0776	0.003850
0.0978	-0.0853	0.003860
0.1024	-0.0933	0.003860
0.1071	-0.1015	0.003870
0.1120	-0.1099	0.003870
0.1170	-0.1184	0.003870
0.1221	-0.1270	0.003880
0.1273	-0.1357	0.003880
0.1327	-0.1444	0.003890
0.1382	-0.1532	0.003890
0.1439	-0.1621	0.003900
0.1497	-0.1709	0.003900
0.1556	-0.1796	0.003910
0.1616	-0.1884	0.003910
0.1678	-0.1970	0.003910
0.1742	-0.2054	0.003910
0.1806	-0.2134	0.003900
0.1872	-0.2203	0.003930
0.1943	-0.2337	0.003970
0.2012	-0.2478	0.003970
0.2082	-0.2566	0.003970
0.2154	-0.2666	0.003970
0.2227	-0.2765	0.003980
0.2301	-0.2864	0.003980
0.2377	-0.2962	0.003990
0.2454	-0.3056	0.003980
0.2532	-0.3145	0.003980
0.2612	-0.3228	0.003970
0.2692	-0.3304	0.003960
0.2774	-0.3372	0.003940
0.2857	-0.3433	0.003930
0.2941	-0.3485	0.003910
0.3027	-0.3528	0.003880
0.3113	-0.3565	0.003860
0.3201	-0.3593	0.003830
0.3290	-0.3615	0.003800
0.3379	-0.3628	0.003770
0.3470	-0.3633	0.003740
0.3561	-0.3628	0.003700
0.3653	-0.3616	0.003660
0.3746	-0.3597	0.003620
0.3840	-0.3571	0.003590
0.3934	-0.3539	0.003550
0.4029	-0.3500	0.003510
0.4124	-0.3455	0.003460
0.4220	-0.3403	0.003420
0.4316	-0.3344	0.003370
0.4413	-0.3277	0.003330
0.4510	-0.3203	0.003270
0.4607	-0.3117	0.003220
0.4704	-0.3021	0.003160
0.4802	-0.2915	0.003100
0.4900	-0.2800	0.003030
0.4998	-0.2676	0.002970
0.5095	-0.2545	0.002900
0.5193	-0.2404	0.002830
0.5290	-0.2254	0.002760
0.5387	-0.2099	0.002680
0.5483	-0.1943	0.002580
0.5572	-0.1737	0.002480
0.5667	-0.1561	0.002440
0.5762	-0.1438	0.002390
0.5856	-0.1288	0.002330
0.5950	-0.1135	0.002260
0.6042	-0.0976	0.002190
0.6135	-0.0813	0.002130
0.6226	-0.0647	0.002050
0.6317	-0.0479	0.001980
0.6408	-0.0309	0.001920
0.6497	-0.0138	0.001850
0.6586	0.0034	0.001770
0.6673	0.0208	0.001700
0.6760	0.0381	0.001630
0.6846	0.0554	0.001560
0.6931	0.0726	0.001490
0.7015	0.0898	0.001410
0.7098	0.1068	0.001340
0.7180	0.1238	0.001280
0.7261	0.1408	0.001200
0.7341	0.1577	0.001130
0.7421	0.1744	0.001060
0.7499	0.1904	0.001000
0.7577	0.2057	0.000950
0.7654	0.2201	0.000900
0.7730	0.2335	0.000870
0.7805	0.2459	0.000840
0.7880	0.2572	0.000820
0.7953	0.2674	0.000800
0.8025	0.2766	0.000790
0.8095	0.2847	0.000790
0.8165	0.2917	0.000800
0.8233	0.2976	0.000820
0.8300	0.3024	0.000840
0.8366	0.3063	0.000860
0.8430	0.3091	0.000890
0.8492	0.3111	0.000930
0.8554	0.3123	0.000970
0.8614	0.3127	0.001010
0.8672	0.3124	0.001050
0.8729	0.3115	0.001090
0.8785	0.3101	0.001140
0.8840	0.3082	0.001180
0.8893	0.3058	0.001230
0.8944	0.3031	0.001270
0.8995	0.3002	0.001320
0.9043	0.2970	0.001360
0.9091	0.2936	0.001400
0.9138	0.2901	0.001440
0.9183	0.2866	0.001480
0.9227	0.2830	0.001520
0.9270	0.2792	0.001560
0.9312	0.2754	0.001590
0.9352	0.2715	0.001630
0.9392	0.2675	0.001670
0.9430	0.2634	0.001700
0.9467	0.2590	0.001740
0.9503	0.2545	0.001780
0.9539	0.2498	0.001820
0.9573	0.2448	0.001860
0.9606	0.2396	0.001910
0.9638	0.2341	0.001950
0.9669	0.2283	0.002000
0.9700	0.2222	0.002050
0.9729	0.2157	0.002100
0.9757	0.2089	0.002160
0.9785	0.2016	0.002220
0.9812	0.1939	0.002280
0.9838	0.1855	0.002350
0.9863	0.1765	0.002420
0.9887	0.1665	0.002510
0.9911	0.1552	0.002610
0.9934	0.1420	0.002790
0.9956	0.1259	0.003230
0.9978	0.1058	0.005370
0.9999	0.0829	0.005370
						
WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7933	0.004490				
0.0001	0.7622	0.004240				
0.0003	0.6881	0.004020				
0.0007	0.6258	0.004220				
0.0011	0.5624	0.004580				
0.0016	0.5008	0.004950				
0.0022	0.4376	0.005280				
0.0028	0.3748	0.005500				
0.0034	0.3140	0.005660				
0.0041	0.2559	0.005800				
0.0049	0.1992	0.005930				
0.0057	0.1437	0.006060				
0.0065	0.0888	0.006190				
0.0074	0.0338	0.006320
0.0083	-0.0220	0.006460
0.0092	-0.0787	0.006590
0.0103	-0.1357	0.006730
0.0113	-0.1925	0.006840
0.0124	-0.2488	0.006940
0.0136	-0.3042	0.007010
0.0148	-0.3586	0.007050
0.0161	-0.4121	0.007060
0.0174	-0.4654	0.007120
0.0189	-0.5227	0.007400
0.0204	-0.5974	0.007990
0.0219	-0.6855	0.008470
0.0233	-0.7739	0.008630
0.0248	-0.8602	0.008630
0.0264	-0.9389	0.008440
0.0280	-1.0022	0.008110
0.0298	-1.0479	0.007680
0.0317	-1.0789	0.007200
0.0338	-1.0965	0.006800
0.0360	-1.1054	0.006550
0.0384	-1.1101	0.006370
0.0409	-1.1118	0.006220
0.0435	-1.1113	0.006100
0.0463	-1.1094	0.005990
0.0492	-1.1065	0.005890
0.0523	-1.1024	0.005810
0.0554	-1.0969	0.005730
0.0587	-1.0916	0.005660
0.0622	-1.0877	0.005600
0.0658	-1.0841	0.005550
0.0695	-1.0804	0.005500
0.0733	-1.0762	0.005440
0.0773	-1.0707	0.005360
0.0814	-1.0632	0.005270
0.0857	-1.0536	0.005190
0.0902	-1.0446	0.005150
0.0948	-1.0384	0.005130
0.0995	-1.0338	0.005110
0.1043	-1.0299	0.005080
0.1093	-1.0265	0.005050
0.1144	-1.0230	0.005020
0.1197	-1.0191	0.004980
0.1251	-1.0152	0.004940
0.1306	-1.0113	0.004900
0.1363	-1.0070	0.004860
0.1422	-1.0021	0.004820
0.1482	-0.9969	0.004780
0.1544	-0.9914	0.004740
0.1607	-0.9853	0.004700
0.1671	-0.9775	0.004610
0.1737	-0.9651	0.004390
0.1804	-0.9368	0.003890
0.1873	-0.8828	0.003230
0.1944	-0.8035	0.002820
0.2016	-0.7194	0.002850
0.2089	-0.6580	0.003140
0.2164	-0.6386	0.003500
0.2241	-0.6497	0.003740
0.2318	-0.6645	0.003890
0.2398	-0.6790	0.004010
0.2478	-0.6930	0.004090
0.2560	-0.7059	0.004150
0.2643	-0.7174	0.004190
0.2728	-0.7278	0.004210
0.2814	-0.7369	0.004230
0.2901	-0.7450	0.004240
0.2989	-0.7521	0.004240
0.3079	-0.7583	0.004240
0.3169	-0.7636	0.004230
0.3261	-0.7683	0.004220
0.3354	-0.7722	0.004210
0.3448	-0.7753	0.004200
0.3542	-0.7775	0.004180
0.3638	-0.7788	0.004160
0.3735	-0.7794	0.004140
0.3832	-0.7793	0.004110
0.3930	-0.7789	0.004090
0.4029	-0.7782	0.004070
0.4128	-0.7774	0.004050
0.4228	-0.7765	0.004030
0.4329	-0.7756	0.004010
0.4430	-0.7745	0.004000
0.4531	-0.7735	0.003980
0.4632	-0.7726	0.003970
0.4734	-0.7720	0.003960
0.4836	-0.7718	0.003950
0.4938	-0.7721	0.003950
0.5041	-0.7730	0.003950
0.5143	-0.7744	0.003960
0.5245	-0.7764	0.003960
0.5347	-0.7791	0.003960
0.5448	-0.7824	0.003970
0.5549	-0.7864	0.003990
0.5650	-0.7909	0.004000
0.5751	-0.7958	0.004010
0.5850	-0.8006	0.004010
0.5950	-0.8047	0.004010
0.6048	-0.8077	0.004000
0.6146	-0.8102	0.003980
0.6244	-0.8120	0.003960
0.6340	-0.8104	0.003890
0.6435	-0.8019	0.003760
0.6530	-0.7832	0.003560
0.6623	-0.7552	0.003360
0.6716	-0.7241	0.003230
0.6807	-0.6991	0.003170
0.6898	-0.6792	0.003100
0.6987	-0.6582	0.003010
0.7075	-0.6366	0.002920
0.7162	-0.6152	0.002830
0.7248	-0.5938	0.002750
0.7332	-0.5727	0.002660
0.7416	-0.5518	0.002580
0.7498	-0.5312	0.002500
0.7578	-0.5109	0.002430
0.7658	-0.4910	0.002350
0.7736	-0.4716	0.002280
0.7812	-0.4525	0.002210
0.7888	-0.4339	0.002150
0.7961	-0.4157	0.002080
0.8034	-0.3979	0.002020
0.8105	-0.3804	0.001950
0.8174	-0.3632	0.001890
0.8243	-0.3463	0.001830
0.8309	-0.3297	0.001770
0.8375	-0.3135	0.001710
0.8439	-0.2977	0.001650
0.8501	-0.2821	0.001600
0.8563	-0.2668	0.001540
0.8622	-0.2519	0.001490
0.8681	-0.2371	0.001430
0.8738	-0.2227	0.001370
0.8793	-0.2085	0.001310
0.8848	-0.1946	0.001260
0.8901	-0.1809	0.001200
0.8952	-0.1675	0.001150
0.9003	-0.1543	0.001100
0.9052	-0.1414	0.001040
0.9099	-0.1286	0.000990
0.9146	-0.1162	0.000930
0.9191	-0.1041	0.000880
0.9235	-0.0923	0.000830
0.9278	-0.0807	0.000780
0.9319	-0.0694	0.000730
0.9360	-0.0584	0.000680
0.9399	-0.0477	0.000630
0.9437	-0.0374	0.000580
0.9474	-0.0273	0.000530
0.9510	-0.0176	0.000480
0.9545	-0.0082	0.000440
0.9579	0.0009	0.000400
0.9612	0.0096	0.000350
0.9644	0.0180	0.000310
0.9675	0.0260	0.000280
0.9705	0.0336	0.000240
0.9734	0.0409	0.000210
0.9762	0.0479	0.000180
0.9790	0.0545	0.000150
0.9816	0.0607	0.000130
0.9842	0.0666	0.000100				
0.9867	0.0721	0.000070				
0.9891	0.0773	0.000050				
0.9914	0.0822	0.000040				
0.9937	0.0868	0.000060				
0.9958	0.0908	0.000100				
0.9980	0.0960	0.000390				
1.0000	0.0917	0.000390				
						
WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.8289	-0.001970				
0.0001	0.8528	-0.000960				
0.0003	0.8538	0.000590				
0.0006	0.8363	0.001490				
0.0010	0.8091	0.002190				
0.0016	0.7732	0.002800
0.0022	0.7314	0.003300
0.0029	0.6859	0.003700
0.0037	0.6389	0.003990
0.0045	0.5918	0.004200
0.0054	0.5456	0.004350
0.0064	0.5010	0.004440
0.0074	0.4585	0.004500
0.0085	0.4183	0.004520
0.0097	0.3807	0.004520
0.0109	0.3456	0.004500
0.0122	0.3129	0.004490
0.0136	0.2824	0.004470
0.0150	0.2540	0.004450
0.0165	0.2278	0.004410
0.0181	0.2046	0.004340
0.0198	0.1844	0.004300
0.0216	0.1651	0.004290
0.0234	0.1464	0.004270
0.0253	0.1293	0.004250
0.0274	0.1137	0.004220
0.0295	0.0997	0.004190
0.0317	0.0870	0.004160
0.0340	0.0757	0.004120
0.0363	0.0656	0.004090
0.0388	0.0563	0.004060
0.0414	0.0479	0.004030
0.0441	0.0401	0.004010
0.0470	0.0326	0.003990
0.0499	0.0254	0.003970
0.0529	0.0184	0.003960
0.0561	0.0113	0.003950
0.0593	0.0043	0.003940
0.0627	-0.0028	0.003930
0.0662	-0.0099	0.003920
0.0698	-0.0169	0.003910
0.0735	-0.0236	0.003900
0.0774	-0.0300	0.003880
0.0813	-0.0361	0.003870
0.0854	-0.0421	0.003860
0.0897	-0.0485	0.003860
0.0940	-0.0558	0.003870
0.0985	-0.0635	0.003870
0.1031	-0.0716	0.003880
0.1078	-0.0798	0.003880
0.1127	-0.0882	0.003890
0.1177	-0.0967	0.003890
0.1228	-0.1053	0.003900
0.1281	-0.1139	0.003900
0.1334	-0.1226	0.003900
0.1390	-0.1313	0.003910
0.1446	-0.1401	0.003910
0.1504	-0.1489	0.003920
0.1564	-0.1577	0.003920
0.1624	-0.1666	0.003920
0.1686	-0.1754	0.003930
0.1750	-0.1843	0.003930
0.1815	-0.1931	0.003930
0.1881	-0.2020	0.003940
0.1949	-0.2109	0.003940
0.2018	-0.2198	0.003940
0.2088	-0.2287	0.003950
0.2160	-0.2376	0.003950
0.2233	-0.2464	0.003950
0.2308	-0.2550	0.003950
0.2384	-0.2632	0.003950
0.2461	-0.2709	0.003940
0.2540	-0.2781	0.003930
0.2619	-0.2846	0.003920
0.2700	-0.2905	0.003900
0.2782	-0.2956	0.003880
0.2866	-0.2999	0.003860
0.2950	-0.3035	0.003840
0.3036	-0.3062	0.003810
0.3122	-0.3080	0.003780
0.3210	-0.3091	0.003750
0.3299	-0.3094	0.003710
0.3389	-0.3088	0.003680
0.3479	-0.3076	0.003640
0.3570	-0.3056	0.003600
0.3662	-0.3030	0.003560
0.3755	-0.2998	0.003520
0.3848	-0.2960	0.003480
0.3942	-0.2917	0.003440
0.4037	-0.2869	0.003400
0.4132	-0.2816	0.003360
0.4227	-0.2757	0.003310
0.4323	-0.2694	0.003270
0.4419	-0.2624	0.003220
0.4515	-0.2547	0.003170
0.4612	-0.2461	0.003120
0.4709	-0.2365	0.003060
0.4806	-0.2261	0.002990
0.4903	-0.2149	0.002930
0.5001	-0.2033	0.002870
0.5098	-0.1911	0.002800
0.5195	-0.1785	0.002740
0.5291	-0.1655	0.002670
0.5388	-0.1522	0.002610
0.5483	-0.1385	0.002540
0.5579	-0.1246	0.002480
0.5674	-0.1104	0.002410
0.5768	-0.0960	0.002340
0.5862	-0.0814	0.002280
0.5955	-0.0665	0.002210
0.6048	-0.0516	0.002140
0.6140	-0.0365	0.002070
0.6232	-0.0213	0.002000
0.6323	-0.0060	0.001930
0.6413	0.0094	0.001870
0.6502	0.0248	0.001800
0.6591	0.0402	0.001730
0.6679	0.0556	0.001660
0.6765	0.0710	0.001590
0.6851	0.0862	0.001520
0.6936	0.1014	0.001450
0.7020	0.1164	0.001380
0.7103	0.1314	0.001320
0.7185	0.1461	0.001250
0.7266	0.1608	0.001180
0.7347	0.1752	0.001120
0.7426	0.1895	0.001050
0.7505	0.2032	0.000990
0.7582	0.2163	0.000940
0.7659	0.2286	0.000900
0.7736	0.2400	0.000860
0.7811	0.2503	0.000830
0.7885	0.2597	0.000810
0.7958	0.2681	0.000800
0.8029	0.2756	0.000800
0.8100	0.2822	0.000800
0.8170	0.2877	0.000810
0.8238	0.2923	0.000820
0.8304	0.2959	0.000840
0.8370	0.2986	0.000870
0.8434	0.3004	0.000900
0.8496	0.3015	0.000940
0.8557	0.3018	0.000980
0.8617	0.3015	0.001020
0.8675	0.3006	0.001060
0.8732	0.2992	0.001100
0.8788	0.2973	0.001140
0.8842	0.2949	0.001190
0.8894	0.2923	0.001230
0.8946	0.2893	0.001280
0.8996	0.2861	0.001320
0.9045	0.2828	0.001360
0.9092	0.2793	0.001400
0.9138	0.2758	0.001440
0.9183	0.2722	0.001470
0.9227	0.2686	0.001510
0.9270	0.2650	0.001540
0.9312	0.2613	0.001580
0.9352	0.2576	0.001610
0.9392	0.2537	0.001640
0.9430	0.2498	0.001680
0.9467	0.2458	0.001710
0.9503	0.2416	0.001750
0.9538	0.2373	0.001790
0.9572	0.2327	0.001830
0.9605	0.2280	0.001870
0.9638	0.2230	0.001910
0.9669	0.2178	0.001950
0.9699	0.2124	0.002000
0.9728	0.2067	0.002040
0.9757	0.2007	0.002090
0.9785	0.1943	0.002150
0.9811	0.1876	0.002200
0.9837	0.1805	0.002260
0.9863	0.1728	0.002330
0.9887	0.1644	0.002410
0.9911	0.1549	0.002500
0.9934	0.1441	0.002660
0.9956	0.1311	0.003070
0.9978	0.1157	0.005110
0.9999	0.0974	0.005980
						
WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8282	0.004380				
0.0001	0.8015	0.004170				
0.0003	0.7320	0.004010				
0.0005	0.6716	0.004310				
0.0009	0.6067	0.004740				
0.0014	0.5440	0.005110				
0.0019	0.4800	0.005450				
0.0025	0.4159	0.005700				
0.0032	0.3542	0.005870				
0.0039	0.2941	0.006020				
0.0046	0.2354	0.006150				
0.0054	0.1778	0.006270				
0.0063	0.1208	0.006400				
0.0072	0.0639	0.006530
0.0081	0.0063	0.006660
0.0091	-0.0520	0.006800
0.0101	-0.1108	0.006930
0.0112	-0.1699	0.007050
0.0124	-0.2286	0.007140
0.0136	-0.2863	0.007200
0.0148	-0.3426	0.007230
0.0161	-0.3972	0.007240
0.0175	-0.4507	0.007320
0.0191	-0.5113	0.007690
0.0206	-0.5934	0.008320
0.0221	-0.6881	0.008760
0.0236	-0.7788	0.008870
0.0252	-0.8629	0.008790
0.0268	-0.9364	0.008530
0.0285	-0.9964	0.008110
0.0304	-1.0405	0.007610
0.0324	-1.0679	0.007110
0.0346	-1.0811	0.006740
0.0369	-1.0862	0.006500
0.0394	-1.0874	0.006320
0.0419	-1.0856	0.006170
0.0446	-1.0817	0.006050
0.0475	-1.0764	0.005940
0.0505	-1.0700	0.005850
0.0536	-1.0628	0.005760
0.0568	-1.0551	0.005680
0.0602	-1.0471	0.005600
0.0637	-1.0391	0.005540
0.0673	-1.0312	0.005470
0.0710	-1.0231	0.005410
0.0749	-1.0144	0.005320
0.0790	-1.0035	0.005210
0.0832	-0.9894	0.005090
0.0875	-0.9728	0.005000
0.0920	-0.9582	0.004950
0.0966	-0.9455	0.004880
0.1013	-0.9302	0.004760
0.1062	-0.9110	0.004610
0.1112	-0.8891	0.004500
0.1163	-0.8681	0.004430
0.1216	-0.8501	0.004410
0.1270	-0.8341	0.004380
0.1326	-0.8173	0.004310
0.1383	-0.7983	0.004240
0.1442	-0.7794	0.004200
0.1503	-0.7655	0.004240
0.1564	-0.7598	0.004330
0.1627	-0.7638	0.004450
0.1692	-0.7745	0.004550
0.1758	-0.7871	0.004600
0.1826	-0.7985	0.004620
0.1895	-0.8068	0.004600
0.1966	-0.8118	0.004560
0.2038	-0.8146	0.004530
0.2111	-0.8162	0.004500
0.2186	-0.8174	0.004480
0.2263	-0.8188	0.004460
0.2340	-0.8201	0.004440
0.2419	-0.8212	0.004410
0.2500	-0.8217	0.004390
0.2582	-0.8215	0.004360
0.2665	-0.8205	0.004320
0.2749	-0.8187	0.004290
0.2835	-0.8164	0.004250
0.2922	-0.8137	0.004220
0.3010	-0.8107	0.004190
0.3099	-0.8075	0.004160
0.3189	-0.8042	0.004130
0.3281	-0.8008	0.004100
0.3373	-0.7975	0.004080
0.3467	-0.7941	0.004050
0.3561	-0.7909	0.004030
0.3656	-0.7878	0.004020
0.3752	-0.7849	0.004000
0.3849	-0.7825	0.003980
0.3947	-0.7804	0.003970
0.4045	-0.7788	0.003960
0.4144	-0.7776	0.003960
0.4243	-0.7766	0.003950
0.4343	-0.7759	0.003950
0.4443	-0.7757	0.003940
0.4544	-0.7761	0.003940
0.4645	-0.7773	0.003950
0.4746	-0.7793	0.003950
0.4847	-0.7819	0.003960
0.4949	-0.7851	0.003970
0.5050	-0.7887	0.003970
0.5151	-0.7925	0.003980
0.5253	-0.7960	0.003990
0.5354	-0.7989	0.003970
0.5454	-0.8003	0.003950
0.5555	-0.7987	0.003900
0.5655	-0.7921	0.003800
0.5754	-0.7771	0.003650
0.5854	-0.7529	0.003480
0.5952	-0.7253	0.003350
0.6050	-0.7030	0.003310
0.6147	-0.6899	0.003340
0.6244	-0.6841	0.003370
0.6339	-0.6797	0.003360
0.6434	-0.6728	0.003330
0.6528	-0.6624	0.003270
0.6621	-0.6494	0.003200
0.6713	-0.6346	0.003130
0.6803	-0.6182	0.003040
0.6893	-0.6006	0.002950
0.6982	-0.5820	0.002860
0.7070	-0.5626	0.002770
0.7156	-0.5429	0.002680
0.7241	-0.5229	0.002600
0.7325	-0.5029	0.002510
0.7408	-0.4830	0.002430
0.7490	-0.4634	0.002350
0.7570	-0.4440	0.002270
0.7649	-0.4250	0.002200
0.7726	-0.4064	0.002130
0.7803	-0.3883	0.002060
0.7878	-0.3705	0.002000
0.7951	-0.3532	0.001930
0.8023	-0.3363	0.001870
0.8094	-0.3198	0.001810
0.8164	-0.3037	0.001750
0.8232	-0.2878	0.001690
0.8298	-0.2724	0.001630
0.8364	-0.2573	0.001580
0.8428	-0.2427	0.001520
0.8490	-0.2283	0.001470
0.8551	-0.2144	0.001420
0.8611	-0.2007	0.001360
0.8670	-0.1874	0.001310
0.8727	-0.1743	0.001260
0.8782	-0.1616	0.001210
0.8837	-0.1491	0.001160
0.8890	-0.1370	0.001110
0.8942	-0.1251	0.001060
0.8992	-0.1135	0.001010
0.9042	-0.1021	0.000960
0.9089	-0.0910	0.000920
0.9136	-0.0802	0.000870
0.9182	-0.0697	0.000820
0.9226	-0.0594	0.000780
0.9269	-0.0494	0.000730
0.9311	-0.0397	0.000690
0.9352	-0.0303	0.000640
0.9391	-0.0212	0.000600
0.9430	-0.0123	0.000560
0.9467	-0.0038	0.000520
0.9504	0.0045	0.000480
0.9539	0.0124	0.000440
0.9573	0.0201	0.000400
0.9607	0.0274	0.000370
0.9639	0.0345	0.000330
0.9670	0.0412	0.000300
0.9701	0.0476	0.000270
0.9730	0.0538	0.000240
0.9759	0.0596	0.000210
0.9786	0.0652	0.000180
0.9813	0.0704	0.000160
0.9839	0.0754	0.000140				
0.9865	0.0800	0.000120				
0.9889	0.0844	0.000100				
0.9913	0.0884	0.000090				
0.9936	0.0923	0.000100				
0.9958	0.0957	0.000150				
0.9979	0.1004	0.000510				
1.0000	0.0981	0.000660				
						
WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.8346	-0.002410				
0.0001	0.8586	-0.001260				
0.0003	0.8623	0.000450				
0.0006	0.8475	0.001400				
0.0010	0.8226	0.002150				
0.0015	0.7886	0.002820
0.0022	0.7481	0.003360
0.0029	0.7035	0.003790
0.0037	0.6568	0.004120
0.0045	0.6097	0.004350
0.0054	0.5634	0.004500
0.0064	0.5185	0.004600
0.0075	0.4756	0.004650
0.0086	0.4351	0.004660
0.0098	0.3972	0.004650
0.0111	0.3618	0.004630
0.0124	0.3288	0.004600
0.0138	0.2982	0.004570
0.0153	0.2697	0.004530
0.0168	0.2435	0.004470
0.0184	0.2206	0.004390
0.0202	0.2005	0.004350
0.0220	0.1810	0.004330
0.0238	0.1626	0.004310
0.0258	0.1457	0.004280
0.0279	0.1303	0.004240
0.0300	0.1166	0.004210
0.0322	0.1042	0.004170
0.0346	0.0931	0.004140
0.0370	0.0832	0.004100
0.0395	0.0741	0.004070
0.0421	0.0658	0.004050
0.0449	0.0581	0.004020
0.0477	0.0507	0.004000
0.0507	0.0435	0.003990
0.0537	0.0365	0.003970
0.0569	0.0294	0.003960
0.0602	0.0224	0.003960
0.0636	0.0153	0.003950
0.0671	0.0083	0.003940
0.0707	0.0015	0.003930
0.0744	-0.0051	0.003920
0.0783	-0.0114	0.003900
0.0823	-0.0174	0.003890
0.0864	-0.0233	0.003880
0.0906	-0.0298	0.003880
0.0950	-0.0371	0.003890
0.0995	-0.0448	0.003900
0.1041	-0.0527	0.003900
0.1088	-0.0609	0.003910
0.1137	-0.0691	0.003920
0.1187	-0.0775	0.003920
0.1238	-0.0859	0.003920
0.1291	-0.0944	0.003930
0.1345	-0.1029	0.003930
0.1400	-0.1115	0.003940
0.1457	-0.1201	0.003940
0.1515	-0.1287	0.003940
0.1575	-0.1373	0.003950
0.1636	-0.1459	0.003950
0.1698	-0.1546	0.003950
0.1762	-0.1633	0.003960
0.1827	-0.1720	0.003960
0.1894	-0.1807	0.003960
0.1961	-0.1895	0.003970
0.2031	-0.1983	0.003970
0.2102	-0.2070	0.003970
0.2174	-0.2158	0.003980
0.2247	-0.2244	0.003980
0.2322	-0.2328	0.003980
0.2398	-0.2408	0.003970
0.2476	-0.2483	0.003960
0.2555	-0.2553	0.003950
0.2635	-0.2616	0.003940
0.2716	-0.2673	0.003930
0.2799	-0.2723	0.003910
0.2882	-0.2765	0.003890
0.2967	-0.2800	0.003870
0.3053	-0.2827	0.003840
0.3140	-0.2846	0.003810
0.3228	-0.2857	0.003770
0.3317	-0.2861	0.003740
0.3406	-0.2857	0.003710
0.3497	-0.2846	0.003670
0.3588	-0.2829	0.003630
0.3680	-0.2806	0.003590
0.3772	-0.2777	0.003550
0.3865	-0.2742	0.003510
0.3959	-0.2703	0.003470
0.4053	-0.2658	0.003430
0.4147	-0.2609	0.003390
0.4242	-0.2555	0.003340
0.4338	-0.2497	0.003300
0.4433	-0.2433	0.003250
0.4529	-0.2363	0.003200
0.4625	-0.2284	0.003150
0.4722	-0.2192	0.003090
0.4818	-0.2093	0.003020
0.4915	-0.1986	0.002960
0.5011	-0.1874	0.002900
0.5108	-0.1758	0.002820
0.5204	-0.1637	0.002760
0.5300	-0.1513	0.002700
0.5396	-0.1385	0.002630
0.5492	-0.1254	0.002560
0.5587	-0.1121	0.002500
0.5681	-0.0985	0.002430
0.5775	-0.0846	0.002360
0.5869	-0.0706	0.002300
0.5962	-0.0563	0.002230
0.6055	-0.0419	0.002160
0.6147	-0.0272	0.002090
0.6238	-0.0124	0.002020
0.6329	0.0025	0.001950
0.6419	0.0175	0.001880
0.6508	0.0325	0.001810
0.6597	0.0476	0.001740
0.6685	0.0628	0.001670
0.6771	0.0779	0.001600
0.6857	0.0929	0.001530
0.6942	0.1079	0.001460
0.7026	0.1227	0.001390
0.7109	0.1375	0.001320
0.7192	0.1519	0.001260
0.7273	0.1659	0.001190
0.7353	0.1800	0.001120
0.7432	0.1940	0.001050
0.7511	0.2077	0.000990
0.7588	0.2207	0.000940
0.7665	0.2328	0.000900
0.7741	0.2439	0.000860
0.7816	0.2540	0.000840
0.7890	0.2630	0.000820
0.7963	0.2711	0.000810
0.8034	0.2784	0.000800
0.8105	0.2848	0.000800
0.8174	0.2902	0.000810
0.8242	0.2947	0.000830
0.8308	0.2982	0.000850
0.8373	0.3009	0.000880
0.8437	0.3027	0.000910
0.8499	0.3037	0.000950
0.8560	0.3040	0.000990
0.8620	0.3037	0.001030
0.8678	0.3028	0.001070
0.8735	0.3013	0.001120
0.8790	0.2995	0.001160
0.8844	0.2972	0.001210
0.8896	0.2946	0.001250
0.8948	0.2918	0.001290
0.8998	0.2887	0.001340
0.9046	0.2854	0.001380
0.9094	0.2821	0.001420
0.9140	0.2786	0.001450
0.9185	0.2752	0.001490
0.9229	0.2717	0.001530
0.9272	0.2682	0.001560
0.9313	0.2646	0.001600
0.9354	0.2610	0.001630
0.9393	0.2573	0.001660
0.9431	0.2535	0.001700
0.9468	0.2497	0.001730
0.9504	0.2456	0.001770
0.9539	0.2414	0.001810
0.9573	0.2371	0.001850
0.9606	0.2325	0.001890
0.9639	0.2278	0.001930
0.9670	0.2228	0.001970
0.9700	0.2176	0.002020
0.9729	0.2121	0.002070
0.9758	0.2064	0.002120
0.9785	0.2003	0.002170
0.9812	0.1940	0.002220
0.9838	0.1872	0.002280
0.9863	0.1800	0.002350
0.9888	0.1721	0.002420
0.9911	0.1634	0.002510
0.9934	0.1536	0.002660
0.9956	0.1420	0.003020
0.9978	0.1300	0.004910
0.9999	0.1112	0.006430
						
WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8351	0.005050				
0.0001	0.8073	0.004740				
0.0002	0.7358	0.004430				
0.0005	0.6753	0.004650				
0.0009	0.6105	0.005090				
0.0014	0.5466	0.005470				
0.0019	0.4819	0.005800				
0.0025	0.4170	0.006050				
0.0031	0.3540	0.006230				
0.0039	0.2925	0.006370				
0.0046	0.2324	0.006500				
0.0054	0.1731	0.006620				
0.0063	0.1143	0.006750				
0.0072	0.0554	0.006870
0.0082	-0.0041	0.007010
0.0092	-0.0645	0.007140
0.0103	-0.1253	0.007270
0.0114	-0.1862	0.007370
0.0126	-0.2467	0.007450
0.0139	-0.3060	0.007500
0.0152	-0.3637	0.007510
0.0166	-0.4197	0.007520
0.0180	-0.4755	0.007700
0.0196	-0.5472	0.008250
0.0212	-0.6392	0.008860
0.0228	-0.7351	0.009160
0.0243	-0.8264	0.009170
0.0260	-0.9015	0.008940
0.0277	-0.9709	0.008560
0.0296	-1.0243	0.008050
0.0316	-1.0602	0.007480
0.0338	-1.0795	0.007000
0.0361	-1.0877	0.006690
0.0386	-1.0905	0.006470
0.0411	-1.0896	0.006290
0.0438	-1.0860	0.006150
0.0467	-1.0805	0.006030
0.0496	-1.0736	0.005930
0.0527	-1.0657	0.005830
0.0559	-1.0570	0.005750
0.0592	-1.0479	0.005670
0.0627	-1.0386	0.005590
0.0662	-1.0293	0.005530
0.0700	-1.0198	0.005450
0.0738	-1.0095	0.005370
0.0778	-0.9972	0.005260
0.0819	-0.9809	0.005100
0.0862	-0.9589	0.004920
0.0906	-0.9332	0.004720
0.0951	-0.9021	0.004440
0.0998	-0.8630	0.004190
0.1045	-0.8276	0.004310
0.1095	-0.8186	0.004670
0.1145	-0.8325	0.004920
0.1197	-0.8483	0.005020
0.1251	-0.8605	0.005030
0.1306	-0.8687	0.005010
0.1362	-0.8734	0.004970
0.1420	-0.8755	0.004930
0.1479	-0.8754	0.004870
0.1540	-0.8739	0.004820
0.1602	-0.8713	0.004770
0.1666	-0.8681	0.004720
0.1731	-0.8640	0.004670
0.1798	-0.8590	0.004620
0.1866	-0.8526	0.004550
0.1935	-0.8446	0.004480
0.2006	-0.8352	0.004410
0.2079	-0.8249	0.004350
0.2153	-0.8149	0.004300
0.2228	-0.8068	0.004280
0.2305	-0.8013	0.004290
0.2383	-0.7982	0.004290
0.2462	-0.7962	0.004290
0.2543	-0.7942	0.004280
0.2625	-0.7912	0.004250
0.2708	-0.7869	0.004210
0.2793	-0.7815	0.004170
0.2879	-0.7759	0.004140
0.2966	-0.7710	0.004120
0.3054	-0.7674	0.004120
0.3143	-0.7654	0.004120
0.3233	-0.7645	0.004120
0.3325	-0.7646	0.004120
0.3417	-0.7654	0.004130
0.3511	-0.7667	0.004130
0.3605	-0.7681	0.004130
0.3700	-0.7696	0.004130
0.3796	-0.7708	0.004120
0.3892	-0.7717	0.004110
0.3990	-0.7720	0.004100
0.4088	-0.7717	0.004080
0.4186	-0.7706	0.004050
0.4285	-0.7686	0.004030
0.4384	-0.7655	0.003990
0.4484	-0.7612	0.003950
0.4584	-0.7553	0.003910
0.4685	-0.7478	0.003850
0.4785	-0.7391	0.003800
0.4886	-0.7302	0.003760
0.4987	-0.7226	0.003730
0.5088	-0.7172	0.003730
0.5188	-0.7141	0.003740
0.5289	-0.7132	0.003760
0.5389	-0.7135	0.003770
0.5489	-0.7141	0.003780
0.5589	-0.7134	0.003770
0.5688	-0.7106	0.003730
0.5787	-0.7054	0.003690
0.5885	-0.6985	0.003640
0.5983	-0.6907	0.003590
0.6080	-0.6826	0.003560
0.6177	-0.6754	0.003530
0.6272	-0.6684	0.003500
0.6367	-0.6604	0.003460
0.6461	-0.6508	0.003400
0.6554	-0.6395	0.003330
0.6646	-0.6265	0.003250
0.6737	-0.6116	0.003170
0.6827	-0.5953	0.003090
0.6917	-0.5780	0.003000
0.7004	-0.5600	0.002910
0.7091	-0.5413	0.002820
0.7177	-0.5222	0.002730
0.7262	-0.5030	0.002640
0.7345	-0.4837	0.002560
0.7427	-0.4646	0.002470
0.7508	-0.4456	0.002390
0.7587	-0.4270	0.002320
0.7666	-0.4087	0.002240
0.7743	-0.3907	0.002170
0.7818	-0.3732	0.002100
0.7893	-0.3561	0.002040
0.7965	-0.3393	0.001970
0.8037	-0.3230	0.001910
0.8107	-0.3071	0.001850
0.8176	-0.2915	0.001790
0.8244	-0.2763	0.001730
0.8310	-0.2614	0.001670
0.8375	-0.2468	0.001620
0.8438	-0.2326	0.001560
0.8500	-0.2188	0.001510
0.8561	-0.2053	0.001460
0.8620	-0.1921	0.001410
0.8678	-0.1792	0.001350
0.8735	-0.1665	0.001300
0.8790	-0.1542	0.001250
0.8844	-0.1421	0.001200
0.8897	-0.1303	0.001150
0.8948	-0.1188	0.001100
0.8999	-0.1075	0.001050
0.9047	-0.0965	0.001010
0.9095	-0.0857	0.000960
0.9141	-0.0752	0.000910
0.9187	-0.0649	0.000860
0.9231	-0.0549	0.000820
0.9273	-0.0452	0.000770
0.9315	-0.0357	0.000730
0.9356	-0.0265	0.000680
0.9395	-0.0175	0.000640
0.9433	-0.0088	0.000600
0.9470	-0.0005	0.000560
0.9506	0.0076	0.000520
0.9542	0.0154	0.000480
0.9576	0.0230	0.000440
0.9609	0.0302	0.000400
0.9641	0.0380	0.000360
0.9672	0.0447	0.000330
0.9702	0.0510	0.000300
0.9732	0.0571	0.000270
0.9760	0.0629	0.000240
0.9787	0.0684	0.000210
0.9814	0.0737	0.000190
0.9840	0.0786	0.000160				
0.9865	0.0832	0.000140				
0.9890	0.0876	0.000120				
0.9913	0.0916	0.000110				
0.9936	0.0955	0.000130				
0.9958	0.0990	0.000200				
0.9979	0.1037	0.000630				
1.0000	0.1032	0.000990				
						
WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m) LOWER SURFACE						
XOC	CP	CFprime				
0.0000	0.8376	-0.002960				
0.0001	0.8592	-0.001630				
0.0002	0.8641	0.000300				
0.0005	0.8518	0.001380				
0.0009	0.8287	0.002270				
0.0015	0.7953	0.003060
0.0021	0.7542	0.003720
0.0028	0.7080	0.004230
0.0036	0.6592	0.004610
0.0045	0.6095	0.004870
0.0055	0.5606	0.005040
0.0065	0.5133	0.005120
0.0076	0.4683	0.005150
0.0088	0.4261	0.005140
0.0101	0.3867	0.005100
0.0115	0.3500	0.005050
0.0129	0.3158	0.005010
0.0144	0.2838	0.004960
0.0160	0.2540	0.004890
0.0176	0.2272	0.004770
0.0193	0.2052	0.004630
0.0211	0.1860	0.004570
0.0230	0.1668	0.004540
0.0250	0.1490	0.004500
0.0271	0.1327	0.004450
0.0292	0.1181	0.004400
0.0315	0.1050	0.004350
0.0338	0.0933	0.004310
0.0362	0.0828	0.004270
0.0387	0.0733	0.004230
0.0413	0.0647	0.004200
0.0440	0.0567	0.004170
0.0468	0.0492	0.004150
0.0497	0.0420	0.004130
0.0527	0.0350	0.004110
0.0559	0.0280	0.004100
0.0591	0.0211	0.004090
0.0624	0.0141	0.004090
0.0658	0.0072	0.004080
0.0694	0.0004	0.004070
0.0730	-0.0062	0.004060
0.0768	-0.0125	0.004040
0.0807	-0.0186	0.004030
0.0847	-0.0244	0.004020
0.0888	-0.0304	0.004020
0.0931	-0.0373	0.004030
0.0975	-0.0480	0.004050
0.1020	-0.0557	0.004060
0.1066	-0.0637	0.004060
0.1114	-0.0718	0.004070
0.1163	-0.0800	0.004070
0.1213	-0.0883	0.004080
0.1265	-0.0967	0.004080
0.1318	-0.1052	0.004090
0.1373	-0.1137	0.004090
0.1428	-0.1222	0.004100
0.1486	-0.1307	0.004100
0.1544	-0.1393	0.004100
0.1604	-0.1479	0.004110
0.1666	-0.1566	0.004110
0.1728	-0.1653	0.004110
0.1793	-0.1740	0.004120
0.1858	-0.1827	0.004120
0.1926	-0.1915	0.004120
0.1994	-0.2003	0.004130
0.2064	-0.2091	0.004130
0.2136	-0.2178	0.004130
0.2209	-0.2266	0.004140
0.2283	-0.2351	0.004140
0.2359	-0.2433	0.004130
0.2436	-0.2511	0.004120
0.2514	-0.2584	0.004110
0.2594	-0.2651	0.004100
0.2675	-0.2712	0.004090
0.2757	-0.2766	0.004070
0.2840	-0.2813	0.004040
0.2925	-0.2852	0.004020
0.3010	-0.2883	0.003990
0.3097	-0.2906	0.003960
0.3184	-0.2922	0.003920
0.3273	-0.2930	0.003890
0.3362	-0.2930	0.003850
0.3451	-0.2923	0.003810
0.3542	-0.2909	0.003770
0.3633	-0.2889	0.003730
0.3724	-0.2862	0.003690
0.3816	-0.2830	0.003650
0.3908	-0.2793	0.003600
0.4001	-0.2751	0.003560
0.4094	-0.2704	0.003520
0.4187	-0.2652	0.003470
0.4281	-0.2596	0.003430
0.4375	-0.2535	0.003380
0.4470	-0.2468	0.003330
0.4564	-0.2396	0.003280
0.4659	-0.2313	0.003210
0.4753	-0.2219	0.003150
0.4848	-0.2118	0.003080
0.4943	-0.2011	0.003020
0.5039	-0.1898	0.002950
0.5134	-0.1781	0.002880
0.5229	-0.1659	0.002810
0.5324	-0.1534	0.002750
0.5418	-0.1406	0.002680
0.5513	-0.1275	0.002610
0.5607	-0.1141	0.002540
0.5701	-0.1004	0.002470
0.5794	-0.0865	0.002400
0.5887	-0.0723	0.002320
0.5980	-0.0579	0.002250
0.6072	-0.0434	0.002180
0.6164	-0.0286	0.002110
0.6255	-0.0138	0.002030
0.6345	0.0012	0.001960
0.6435	0.0163	0.001880
0.6524	0.0314	0.001810
0.6613	0.0466	0.001730
0.6700	0.0617	0.001660
0.6787	0.0768	0.001580
0.6873	0.0918	0.001510
0.6958	0.1067	0.001440
0.7042	0.1215	0.001360
0.7125	0.1361	0.001290
0.7207	0.1503	0.001230
0.7288	0.1643	0.001160
0.7369	0.1782	0.001080
0.7448	0.1919	0.001020
0.7526	0.2052	0.000950
0.7603	0.2178	0.000900
0.7680	0.2294	0.000860
0.7755	0.2401	0.000830
0.7830	0.2498	0.000810
0.7903	0.2585	0.000790
0.7975	0.2663	0.000780
0.8046	0.2734	0.000780
0.8115	0.2796	0.000780
0.8184	0.2848	0.000790
0.8251	0.2892	0.000810
0.8317	0.2927	0.000840
0.8382	0.2962	0.000870
0.8445	0.2982	0.000910
0.8507	0.2994	0.000940
0.8567	0.2999	0.000980
0.8626	0.2999	0.001030
0.8684	0.2993	0.001070
0.8741	0.2982	0.001110
0.8796	0.2966	0.001160
0.8849	0.2947	0.001200
0.8902	0.2925	0.001250
0.8953	0.2900	0.001290
0.9003	0.2874	0.001340
0.9051	0.2845	0.001380
0.9099	0.2816	0.001420
0.9145	0.2786	0.001450
0.9189	0.2755	0.001490
0.9233	0.2725	0.001530
0.9276	0.2694	0.001560
0.9317	0.2663	0.001590
0.9357	0.2631	0.001630
0.9396	0.2599	0.001660
0.9434	0.2566	0.001690
0.9471	0.2532	0.001720
0.9507	0.2497	0.001760
0.9542	0.2461	0.001800
0.9576	0.2423	0.001830
0.9609	0.2384	0.001870
0.9641	0.2343	0.001910
0.9672	0.2300	0.001950
0.9702	0.2255	0.002000
0.9731	0.2208	0.002040
0.9759	0.2159	0.002090
0.9787	0.2108	0.002140
0.9813	0.2054	0.002190
0.9839	0.1998	0.002240
0.9864	0.1938	0.002300
0.9888	0.1874	0.002360
0.9912	0.1804	0.002440
0.9935	0.1727	0.002560
0.9957	0.1646	0.002830
0.9978	0.1583	0.004420
0.9999	0.1363	0.005770
						
WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8390	0.005690				
0.0001	0.8130	0.005290				
0.0002	0.7468	0.004810				
0.0005	0.6910	0.004990				
0.0008	0.6295	0.005520				
0.0013	0.5655	0.005980				
0.0018	0.5000	0.006340				
0.0024	0.4342	0.006610				
0.0030	0.3691	0.006820				
0.0038	0.3048	0.006980				
0.0046	0.2413	0.007110				
0.0055	0.1784	0.007240				
0.0064	0.1157	0.007370				
0.0074	0.0527	0.007490
0.0084	-0.0110	0.007630
0.0096	-0.0755	0.007760
0.0108	-0.1406	0.007870
0.0120	-0.2060	0.007970
0.0134	-0.2710	0.008050
0.0148	-0.3352	0.008080
0.0163	-0.3984	0.008100
0.0178	-0.4608	0.008250
0.0195	-0.5333	0.008730
0.0212	-0.6254	0.009360
0.0229	-0.7265	0.009720
0.0247	-0.8238	0.009720
0.0266	-0.9110	0.009450
0.0286	-0.9829	0.008950
0.0307	-1.0352	0.008260
0.0329	-1.0659	0.007510
0.0353	-1.0769	0.006920
0.0378	-1.0759	0.006560
0.0404	-1.0708	0.006350
0.0432	-1.0636	0.006200
0.0460	-1.0556	0.006110
0.0490	-1.0478	0.006040
0.0520	-1.0402	0.005980
0.0552	-1.0325	0.005910
0.0585	-1.0243	0.005830
0.0619	-1.0149	0.005730
0.0655	-1.0035	0.005620
0.0691	-0.9898	0.005490
0.0729	-0.9730	0.005330
0.0768	-0.9519	0.005130
0.0809	-0.9251	0.004850
0.0850	-0.8909	0.004490
0.0893	-0.8490	0.004350
0.0937	-0.8152	0.004590
0.0982	-0.8061	0.004930
0.1029	-0.8143	0.005170
0.1077	-0.8264	0.005260
0.1126	-0.8362	0.005260
0.1177	-0.8420	0.005220
0.1229	-0.8439	0.005150
0.1282	-0.8420	0.005060
0.1337	-0.8361	0.004950
0.1394	-0.8257	0.004810
0.1451	-0.8112	0.004670
0.1510	-0.7954	0.004610
0.1571	-0.7840	0.004650
0.1633	-0.7805	0.004710
0.1696	-0.7817	0.004730
0.1761	-0.7825	0.004700
0.1827	-0.7797	0.004630
0.1894	-0.7736	0.004550
0.1964	-0.7659	0.004500
0.2034	-0.7585	0.004480
0.2106	-0.7523	0.004470
0.2179	-0.7467	0.004450
0.2254	-0.7412	0.004430
0.2330	-0.7359	0.004400
0.2407	-0.7313	0.004380
0.2486	-0.7280	0.004360
0.2566	-0.7264	0.004350
0.2647	-0.7262	0.004360
0.2730	-0.7267	0.004360
0.2814	-0.7267	0.004360
0.2899	-0.7254	0.004350
0.2985	-0.7229	0.004330
0.3072	-0.7195	0.004290
0.3161	-0.7159	0.004250
0.3250	-0.7126	0.004210
0.3340	-0.7093	0.004180
0.3432	-0.7056	0.004140
0.3524	-0.7016	0.004120
0.3617	-0.6981	0.004100
0.3711	-0.6916	0.004110
0.3806	-0.6899	0.004100
0.3901	-0.6879	0.004080
0.3997	-0.6854	0.004070
0.4094	-0.6821	0.004050
0.4191	-0.6783	0.004030
0.4289	-0.6743	0.004010
0.4387	-0.6706	0.004000
0.4485	-0.6678	0.003980
0.4584	-0.6660	0.003970
0.4683	-0.6650	0.003960
0.4782	-0.6642	0.003950
0.4881	-0.6682	0.003930
0.4980	-0.6673	0.003920
0.5080	-0.6659	0.003920
0.5179	-0.6641	0.003910
0.5278	-0.6619	0.003900
0.5377	-0.6592	0.003890
0.5475	-0.6563	0.003870
0.5574	-0.6531	0.003850
0.5672	-0.6497	0.003820
0.5769	-0.6460	0.003790
0.5866	-0.6415	0.003760
0.5963	-0.6362	0.003720
0.6058	-0.6302	0.003690
0.6154	-0.6242	0.003660
0.6248	-0.6183	0.003630
0.6342	-0.6115	0.003590
0.6435	-0.6036	0.003540
0.6527	-0.5943	0.003480
0.6618	-0.5835	0.003410
0.6708	-0.5710	0.003330
0.6797	-0.5573	0.003250
0.6886	-0.5426	0.003170
0.6973	-0.5270	0.003080
0.7059	-0.5106	0.002990
0.7144	-0.4936	0.002900
0.7228	-0.4763	0.002820
0.7311	-0.4588	0.002730
0.7392	-0.4412	0.002650
0.7472	-0.4236	0.002560
0.7552	-0.4062	0.002490
0.7629	-0.3889	0.002410
0.7706	-0.3720	0.002330
0.7782	-0.3553	0.002260
0.7856	-0.3391	0.002200
0.7928	-0.3233	0.002130
0.8000	-0.3079	0.002070
0.8070	-0.2930	0.002010
0.8139	-0.2785	0.001960
0.8207	-0.2646	0.001900
0.8273	-0.2508	0.001840
0.8338	-0.2370	0.001780
0.8401	-0.2233	0.001720
0.8463	-0.2098	0.001660
0.8524	-0.1967	0.001610
0.8584	-0.1838	0.001550
0.8642	-0.1712	0.001500
0.8699	-0.1590	0.001450
0.8755	-0.1470	0.001390
0.8809	-0.1354	0.001340
0.8862	-0.1240	0.001290
0.8914	-0.1129	0.001250
0.8964	-0.1021	0.001200
0.9014	-0.0915	0.001150
0.9062	-0.0811	0.001100
0.9108	-0.0710	0.001050
0.9154	-0.0611	0.001000
0.9198	-0.0514	0.000960
0.9242	-0.0419	0.000910
0.9284	-0.0327	0.000860
0.9325	-0.0236	0.000820
0.9365	-0.0148	0.000770
0.9403	-0.0062	0.000730
0.9441	0.0021	0.000680
0.9478	0.0102	0.000640
0.9513	0.0181	0.000600
0.9548	0.0258	0.000560
0.9581	0.0331	0.000520
0.9614	0.0402	0.000480
0.9645	0.0471	0.000440
0.9676	0.0538	0.000400
0.9706	0.0601	0.000370
0.9735	0.0662	0.000330
0.9763	0.0720	0.000300
0.9790	0.0776	0.000270
0.9817	0.0829	0.000240
0.9842	0.0879	0.000220				
0.9867	0.0941	0.000200				
0.9891	0.0985	0.000180				
0.9914	0.1027	0.000170				
0.9937	0.1067	0.000200				
0.9958	0.1105	0.000320				
0.9980	0.1144	0.000950				
1.0000	0.1159	0.001470				


WING/BODY/FX2B-FAIRING						

GRID_SIZE	MACH	ALPHA				
30751522	0.75	-0.044				

WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m) - LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.9216	-0.001660
0.0000	0.9289	-0.001130
0.0001	0.9349	-0.000420
0.0002	0.9379	-0.000130
0.0004	0.9382	0.000110
0.0006	0.9350	0.000360
0.0008	0.9278	0.000620
0.0012	0.9167	0.000860
0.0016	0.9023	0.001100
0.0021	0.8846	0.001330
0.0027	0.8633	0.001550
0.0033	0.8389	0.001770
0.0040	0.8119	0.001970
0.0048	0.7826	0.002160
0.0057	0.7515	0.002340
0.0066	0.7189	0.002510
0.0077	0.6853	0.002660
0.0088	0.6509	0.002810
0.0100	0.6159	0.002950
0.0113	0.5806	0.003080
0.0127	0.5451	0.003200
0.0142	0.5103	0.003300
0.0158	0.4762	0.003400
0.0174	0.4426	0.003490
0.0192	0.4097	0.003580
0.0210	0.3777	0.003650
0.0230	0.3467	0.003710
0.0250	0.3167	0.003770
0.0271	0.2878	0.003820
0.0293	0.2600	0.003860
0.0317	0.2333	0.003900
0.0341	0.2078	0.003930
0.0366	0.1833	0.003960
0.0392	0.1599	0.003980
0.0420	0.1377	0.003990
0.0448	0.1166	0.004010
0.0478	0.0967	0.004010
0.0508	0.0778	0.004010
0.0540	0.0599	0.004010
0.0573	0.0428	0.004010
0.0607	0.0263	0.004010
0.0642	0.0106	0.004000
0.0679	-0.0044	0.004000
0.0716	-0.0185	0.003990
0.0755	-0.0320	0.003980
0.0795	-0.0447	0.003970
0.0837	-0.0568	0.003950
0.0879	-0.0683	0.003940
0.0923	-0.0792	0.003930
0.0968	-0.0897	0.003910
0.1015	-0.0998	0.003900
0.1063	-0.1096	0.003880
0.1112	-0.1190	0.003870
0.1163	-0.1280	0.003850
0.1215	-0.1368	0.003830
0.1269	-0.1451	0.003820
0.1324	-0.1530	0.003800
0.1380	-0.1605	0.003780
0.1438	-0.1673	0.003760
0.1497	-0.1734	0.003740
0.1558	-0.1787	0.003710
0.1620	-0.1830	0.003680
0.1684	-0.1864	0.003650
0.1749	-0.1888	0.003610
0.1815	-0.1904	0.003580
0.1883	-0.1918	0.003550
0.1953	-0.1935	0.003530
0.2024	-0.1961	0.003510
0.2096	-0.2002	0.003510
0.2170	-0.2063	0.003530
0.2245	-0.2144	0.003550
0.2322	-0.2237	0.003560
0.2400	-0.2321	0.003560
0.2479	-0.2392	0.003560
0.2560	-0.2461	0.003560
0.2642	-0.2524	0.003550
0.2726	-0.2574	0.003530
0.2810	-0.2612	0.003510
0.2896	-0.2643	0.003480
0.2984	-0.2670	0.003470
0.3072	-0.2703	0.003460
0.3162	-0.2748	0.003460
0.3252	-0.2813	0.003470
0.3344	-0.2905	0.003510
0.3437	-0.3011	0.003530
0.3531	-0.3095	0.003520
0.3626	-0.3129	0.003480
0.3721	-0.3125	0.003430
0.3818	-0.3108	0.003390
0.3915	-0.3103	0.003370
0.4013	-0.3123	0.003370
0.4112	-0.3161	0.003370
0.4211	-0.3193	0.003360
0.4311	-0.3213	0.003350
0.4411	-0.3232	0.003340
0.4512	-0.3262	0.003340
0.4613	-0.3316	0.003360
0.4714	-0.3404	0.003400
0.4816	-0.3522	0.003450
0.4918	-0.3646	0.003480
0.5019	-0.3749	0.003490
0.5121	-0.3822	0.003480
0.5223	-0.3844	0.003430
0.5324	-0.3793	0.003350
0.5426	-0.3674	0.003240
0.5527	-0.3502	0.003120
0.5627	-0.3292	0.002990
0.5728	-0.3058	0.002860
0.5828	-0.2812	0.002740
0.5927	-0.2561	0.002620
0.6026	-0.2310	0.002510
0.6123	-0.2056	0.002390
0.6220	-0.1800	0.002290
0.6316	-0.1551	0.002200
0.6411	-0.1310	0.002100
0.6505	-0.1076	0.002010
0.6598	-0.0845	0.001920
0.6689	-0.0616	0.001830
0.6778	-0.0386	0.001730
0.6866	-0.0156	0.001630
0.6952	0.0071	0.001540
0.7036	0.0291	0.001440
0.7119	0.0501	0.001350
0.7200	0.0693	0.001280
0.7279	0.0866	0.001210
0.7357	0.1021	0.001160
0.7433	0.1159	0.001110
0.7509	0.1302	0.001070
0.7583	0.1397	0.001060
0.7656	0.1474	0.001060
0.7728	0.1534	0.001070
0.7800	0.1577	0.001080
0.7871	0.1605	0.001100
0.7941	0.1621	0.001120
0.8011	0.1628	0.001150
0.8079	0.1627	0.001170
0.8147	0.1621	0.001190
0.8213	0.1610	0.001220
0.8278	0.1597	0.001230
0.8343	0.1581	0.001250
0.8406	0.1563	0.001270
0.8468	0.1540	0.001290
0.8528	0.1513	0.001310
0.8588	0.1481	0.001330
0.8646	0.1447	0.001350
0.8703	0.1410	0.001370
0.8759	0.1372	0.001390
0.8813	0.1331	0.001410
0.8867	0.1288	0.001440
0.8919	0.1242	0.001470
0.8970	0.1194	0.001510
0.9019	0.1143	0.001540
0.9068	0.1089	0.001570
0.9115	0.1033	0.001600
0.9161	0.0976	0.001640
0.9206	0.0915	0.001680
0.9250	0.0851	0.001740
0.9293	0.0786	0.001800
0.9334	0.0721	0.001840
0.9375	0.0658	0.001880
0.9414	0.0597	0.001920
0.9452	0.0539	0.001940
0.9490	0.0486	0.001960
0.9526	0.0437	0.001970
0.9561	0.0393	0.001980
0.9595	0.0354	0.001980
0.9628	0.0318	0.001980
0.9661	0.0286	0.001980
0.9692	0.0257	0.001980
0.9722	0.0232	0.001970
0.9752	0.0210	0.001970
0.9780	0.0190	0.001960
0.9808	0.0170	0.001960
0.9835	0.0150	0.001970
0.9861	0.0128	0.001960
0.9886	0.0104	0.001960				
0.9910	0.0077	0.001940				
0.9934	0.0046	0.001890				
0.9957	0.0025	0.001860				
0.9979	-0.0481	0.002220				
1.0000	-0.0923	0.002240				
						
WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m) - UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.9204	0.002210				
0.0000	0.9107	0.001810				
0.0000	0.8918	0.001380				
0.0001	0.8748	0.001420				
0.0002	0.8537	0.001640				
0.0004	0.8289	0.001910				
0.0006	0.7994	0.002230				
0.0008	0.7630	0.002630
0.0011	0.7160	0.003090
0.0015	0.6583	0.003480
0.0019	0.5982	0.003770
0.0025	0.5366	0.004070
0.0031	0.4699	0.004390
0.0038	0.3993	0.004700
0.0046	0.3247	0.005000
0.0055	0.2467	0.005290
0.0065	0.1660	0.005570
0.0076	0.0841	0.005790
0.0088	0.0028	0.005980
0.0101	-0.0777	0.006150
0.0115	-0.1570	0.006300
0.0130	-0.2347	0.006430
0.0146	-0.3103	0.006520
0.0163	-0.3834	0.006600
0.0182	-0.4537	0.006650
0.0201	-0.5209	0.006690
0.0221	-0.5844	0.006690
0.0243	-0.6427	0.006650
0.0265	-0.6954	0.006590
0.0289	-0.7427	0.006520
0.0313	-0.7843	0.006420
0.0339	-0.8202	0.006320
0.0366	-0.8502	0.006200
0.0394	-0.8747	0.006080
0.0423	-0.8942	0.005950
0.0453	-0.9095	0.005830
0.0484	-0.9216	0.005720
0.0516	-0.9312	0.005600
0.0550	-0.9369	0.005460
0.0584	-0.9385	0.005330
0.0620	-0.9382	0.005230
0.0657	-0.9372	0.005130
0.0695	-0.9352	0.005030
0.0735	-0.9323	0.004940
0.0775	-0.9286	0.004850
0.0817	-0.9244	0.004770
0.0860	-0.9202	0.004700
0.0904	-0.9161	0.004640
0.0950	-0.9124	0.004590
0.0997	-0.9092	0.004540
0.1045	-0.9065	0.004500
0.1094	-0.9042	0.004460
0.1145	-0.9020	0.004420
0.1197	-0.9000	0.004370
0.1251	-0.8931	0.004240
0.1305	-0.8764	0.004070
0.1362	-0.8580	0.004000
0.1419	-0.8496	0.004050
0.1479	-0.8524	0.004130
0.1539	-0.8595	0.004160
0.1601	-0.8607	0.004090
0.1664	-0.8529	0.004020
0.1729	-0.8471	0.004010
0.1795	-0.8467	0.004010
0.1862	-0.8443	0.003970
0.1931	-0.8386	0.003920
0.2002	-0.8317	0.003880
0.2074	-0.8275	0.003880
0.2147	-0.8270	0.003880
0.2222	-0.8240	0.003840
0.2298	-0.8162	0.003770
0.2375	-0.8069	0.003740
0.2454	-0.8008	0.003720
0.2534	-0.7926	0.003650
0.2615	-0.7773	0.003560
0.2698	-0.7603	0.003490
0.2782	-0.7445	0.003440
0.2868	-0.7289	0.003380
0.2954	-0.7114	0.003310
0.3042	-0.6921	0.003250
0.3131	-0.6741	0.003220
0.3221	-0.6613	0.003230
0.3312	-0.6537	0.003250
0.3404	-0.6474	0.003260
0.3497	-0.6410	0.003260
0.3591	-0.6348	0.003260
0.3686	-0.6293	0.003260
0.3782	-0.6247	0.003260
0.3878	-0.6200	0.003260
0.3976	-0.6144	0.003250
0.4074	-0.6090	0.003240
0.4172	-0.6038	0.003230
0.4272	-0.5988	0.003230
0.4371	-0.5940	0.003220
0.4472	-0.5895	0.003210
0.4572	-0.5851	0.003210
0.4673	-0.5810	0.003200
0.4774	-0.5770	0.003200
0.4876	-0.5731	0.003190
0.4977	-0.5693	0.003190
0.5079	-0.5656	0.003180
0.5180	-0.5619	0.003170
0.5281	-0.5582	0.003170
0.5383	-0.5544	0.003160
0.5484	-0.5505	0.003150
0.5585	-0.5463	0.003140
0.5685	-0.5419	0.003130
0.5785	-0.5371	0.003110
0.5885	-0.5320	0.003100
0.5984	-0.5264	0.003080
0.6082	-0.5203	0.003060
0.6180	-0.5137	0.003030
0.6277	-0.5065	0.003010
0.6373	-0.4989	0.002980
0.6468	-0.4908	0.002950
0.6562	-0.4818	0.002910
0.6656	-0.4719	0.002870
0.6748	-0.4609	0.002830
0.6839	-0.4490	0.002780
0.6929	-0.4363	0.002730
0.7018	-0.4230	0.002670
0.7105	-0.4093	0.002620
0.7191	-0.3955	0.002570
0.7276	-0.3817	0.002520
0.7359	-0.3681	0.002470
0.7442	-0.3551	0.002430
0.7523	-0.3427	0.002390
0.7602	-0.3310	0.002360
0.7681	-0.3205	0.002330
0.7758	-0.3111	0.002300
0.7833	-0.3028	0.002290
0.7908	-0.2954	0.002270
0.7980	-0.2887	0.002260
0.8052	-0.2827	0.002240
0.8122	-0.2770	0.002230
0.8190	-0.2642	0.002180
0.8257	-0.2586	0.002160
0.8322	-0.2529	0.002140
0.8386	-0.2473	0.002120
0.8448	-0.2417	0.002100
0.8509	-0.2356	0.002070
0.8568	-0.2288	0.002030
0.8625	-0.2221	0.002000
0.8681	-0.2154	0.001960
0.8736	-0.2088	0.001920
0.8789	-0.2026	0.001880
0.8841	-0.1971	0.001850
0.8892	-0.1919	0.001820
0.8942	-0.1868	0.001780
0.8990	-0.1819	0.001750
0.9037	-0.1771	0.001700
0.9083	-0.1726	0.001670
0.9127	-0.1683	0.001630
0.9171	-0.1644	0.001600
0.9214	-0.1609	0.001570
0.9255	-0.1576	0.001540
0.9295	-0.1545	0.001510
0.9335	-0.1516	0.001490
0.9373	-0.1489	0.001470
0.9411	-0.1465	0.001460
0.9447	-0.1443	0.001460
0.9483	-0.1423	0.001460
0.9518	-0.1405	0.001460
0.9551	-0.1387	0.001470
0.9584	-0.1364	0.001510
0.9616	-0.1341	0.001560
0.9647	-0.1318	0.001610
0.9678	-0.1291	0.001650				
0.9707	-0.1262	0.001680				
0.9736	-0.1231	0.001710				
0.9764	-0.1198	0.001720				
0.9791	-0.1157	0.001730				
0.9817	-0.1107	0.001720				
0.9843	-0.1051	0.001700				
0.9868	-0.0991	0.001670				
0.9891	-0.0927	0.001630				
0.9915	-0.0858	0.001570				
0.9937	-0.0784	0.001460				
0.9959	-0.0707	0.001410				
0.9980	-0.0931	0.001800				
1.0000	-0.1056	0.001770				
						
WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.7974	-0.002380
0.0000	0.8094	-0.001630
0.0001	0.8194	-0.000660
0.0002	0.8251	-0.000260
0.0004	0.8267	0.000090
0.0007	0.8232	0.000430
0.0010	0.8144	0.000760
0.0014	0.8007	0.001080
0.0019	0.7828	0.001380
0.0025	0.7609	0.001660
0.0031	0.7353	0.001920
0.0039	0.7067	0.002150
0.0047	0.6757	0.002360
0.0055	0.6430	0.002550
0.0065	0.6091	0.002720
0.0076	0.5745	0.002870
0.0087	0.5396	0.003000
0.0099	0.5046	0.003130
0.0112	0.4697	0.003250
0.0125	0.4350	0.003360
0.0140	0.4006	0.003450
0.0155	0.3675	0.003520
0.0171	0.3364	0.003580
0.0188	0.3061	0.003650
0.0206	0.2763	0.003710
0.0225	0.2475	0.003760
0.0245	0.2200	0.003810
0.0265	0.1937	0.003850
0.0287	0.1687	0.003880
0.0309	0.1450	0.003900
0.0333	0.1224	0.003920
0.0357	0.1011	0.003940
0.0382	0.0809	0.003950
0.0409	0.0617	0.003960
0.0436	0.0436	0.003970
0.0464	0.0263	0.003970
0.0494	0.0100	0.003980
0.0524	-0.0056	0.003980
0.0556	-0.0204	0.003980
0.0589	-0.0346	0.003970
0.0623	-0.0483	0.003970
0.0658	-0.0613	0.003970
0.0694	-0.0738	0.003960
0.0731	-0.0857	0.003960
0.0770	-0.0971	0.003950
0.0810	-0.1079	0.003940
0.0851	-0.1184	0.003930
0.0893	-0.1285	0.003920
0.0937	-0.1383	0.003910
0.0982	-0.1478	0.003910
0.1028	-0.1571	0.003900
0.1076	-0.1662	0.003890
0.1125	-0.1752	0.003890
0.1175	-0.1840	0.003880
0.1227	-0.1926	0.003870
0.1280	-0.2009	0.003870
0.1334	-0.2089	0.003860
0.1390	-0.2166	0.003850
0.1448	-0.2237	0.003840
0.1506	-0.2303	0.003820
0.1567	-0.2362	0.003800
0.1628	-0.2413	0.003780
0.1691	-0.2458	0.003760
0.1756	-0.2498	0.003740
0.1822	-0.2536	0.003720
0.1890	-0.2575	0.003700
0.1959	-0.2618	0.003700
0.2029	-0.2666	0.003690
0.2101	-0.2724	0.003690
0.2175	-0.2790	0.003700
0.2249	-0.2867	0.003710
0.2326	-0.2954	0.003730
0.2403	-0.3048	0.003750
0.2482	-0.3141	0.003750
0.2562	-0.3217	0.003740
0.2644	-0.3276	0.003730
0.2727	-0.3328	0.003710
0.2811	-0.3373	0.003700
0.2896	-0.3414	0.003680
0.2983	-0.3452	0.003670
0.3071	-0.3488	0.003650
0.3160	-0.3526	0.003650
0.3250	-0.3575	0.003650
0.3342	-0.3647	0.003680
0.3434	-0.3738	0.003690
0.3527	-0.3806	0.003680
0.3620	-0.3826	0.003630
0.3715	-0.3814	0.003590
0.3811	-0.3789	0.003540
0.3908	-0.3770	0.003520
0.4005	-0.3769	0.003510
0.4103	-0.3783	0.003500
0.4202	-0.3785	0.003480
0.4301	-0.3768	0.003450
0.4401	-0.3754	0.003430
0.4501	-0.3752	0.003420
0.4602	-0.3762	0.003420
0.4703	-0.3779	0.003420
0.4804	-0.3800	0.003420
0.4905	-0.3827	0.003430
0.5006	-0.3863	0.003430
0.5107	-0.3860	0.003390
0.5208	-0.3786	0.003310
0.5308	-0.3664	0.003220
0.5409	-0.3503	0.003110
0.5509	-0.3310	0.003000
0.5609	-0.3094	0.002880
0.5709	-0.2863	0.002770
0.5809	-0.2622	0.002650
0.5908	-0.2377	0.002550
0.6006	-0.2133	0.002440
0.6104	-0.1892	0.002350
0.6201	-0.1658	0.002260
0.6297	-0.1434	0.002180
0.6391	-0.1213	0.002100
0.6485	-0.0992	0.002010
0.6578	-0.0769	0.001920
0.6669	-0.0546	0.001840
0.6758	-0.0324	0.001750
0.6846	-0.0103	0.001660
0.6932	0.0115	0.001570
0.7017	0.0329	0.001490
0.7100	0.0539	0.001410
0.7181	0.0743	0.001320
0.7260	0.0946	0.001240
0.7339	0.1141	0.001170
0.7415	0.1319	0.001120
0.7491	0.1480	0.001080
0.7566	0.1625	0.001050
0.7639	0.1754	0.001020
0.7712	0.1869	0.001000
0.7784	0.1973	0.000990
0.7856	0.2066	0.000990
0.7926	0.2147	0.000990
0.7996	0.2219	0.000990
0.8065	0.2282	0.001000
0.8133	0.2340	0.001010
0.8200	0.2391	0.001020
0.8266	0.2437	0.001040
0.8331	0.2477	0.001050
0.8394	0.2511	0.001070
0.8457	0.2541	0.001090
0.8518	0.2566	0.001110
0.8578	0.2587	0.001120
0.8636	0.2604	0.001140
0.8694	0.2616	0.001160
0.8750	0.2625	0.001190
0.8805	0.2583	0.001220
0.8859	0.2585	0.001240
0.8911	0.2585	0.001260
0.8963	0.2583	0.001290
0.9013	0.2578	0.001310
0.9061	0.2570	0.001330
0.9109	0.2560	0.001360
0.9155	0.2549	0.001380
0.9201	0.2535	0.001400
0.9245	0.2519	0.001430
0.9288	0.2501	0.001450
0.9330	0.2482	0.001480
0.9370	0.2462	0.001500
0.9410	0.2441	0.001530
0.9449	0.2420	0.001550
0.9486	0.2398	0.001570
0.9523	0.2377	0.001590
0.9558	0.2354	0.001610
0.9592	0.2331	0.001630
0.9626	0.2307	0.001660
0.9658	0.2281	0.001680
0.9690	0.2254	0.001710
0.9720	0.2224	0.001730
0.9750	0.2191	0.001760
0.9779	0.2155	0.001800
0.9807	0.2115	0.001830
0.9834	0.2069	0.001870
0.9860	0.2017	0.001920
0.9885	0.1955	0.001980				
0.9910	0.1881	0.002060				
0.9933	0.1789	0.002190				
0.9956	0.1670	0.002510				
0.9979	0.1505	0.004220				
1.0000	0.1280	0.004220				
						
WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7952	0.003340				
0.0000	0.7792	0.002760				
0.0001	0.7487	0.002110				
0.0002	0.7218	0.002140				
0.0004	0.6883	0.002450				
0.0007	0.6483	0.002870				
0.0009	0.5990	0.003390				
0.0013	0.5391	0.003900
0.0017	0.4710	0.004250
0.0022	0.4038	0.004480
0.0029	0.3383	0.004730
0.0036	0.2688	0.005040
0.0043	0.1948	0.005360
0.0052	0.1175	0.005630
0.0061	0.0398	0.005840
0.0071	-0.0358	0.006010
0.0082	-0.1103	0.006190
0.0094	-0.1860	0.006380
0.0107	-0.2616	0.006530
0.0120	-0.3353	0.006640
0.0134	-0.4068	0.006730
0.0149	-0.4761	0.006800
0.0165	-0.5439	0.006880
0.0182	-0.6116	0.006980
0.0200	-0.6811	0.007100
0.0219	-0.7541	0.007240
0.0238	-0.8288	0.007300
0.0258	-0.8977	0.007220
0.0280	-0.9560	0.007080
0.0302	-1.0058	0.006940
0.0326	-1.0485	0.006800
0.0350	-1.0851	0.006670
0.0376	-1.1160	0.006530
0.0402	-1.1422	0.006410
0.0430	-1.1642	0.006290
0.0459	-1.1832	0.006190
0.0490	-1.2004	0.006120
0.0521	-1.2172	0.006050
0.0553	-1.2328	0.005960
0.0587	-1.2447	0.005860
0.0621	-1.2538	0.005770
0.0657	-1.2613	0.005690
0.0695	-1.2673	0.005620
0.0733	-1.2719	0.005540
0.0773	-1.2753	0.005470
0.0814	-1.2777	0.005400
0.0856	-1.2791	0.005340
0.0899	-1.2797	0.005280
0.0944	-1.2795	0.005220
0.0990	-1.2785	0.005170
0.1037	-1.2767	0.005110
0.1086	-1.2740	0.005040
0.1136	-1.2700	0.004980
0.1187	-1.2642	0.004910
0.1240	-1.2555	0.004830
0.1295	-1.2431	0.004740
0.1350	-1.2267	0.004640
0.1407	-1.2067	0.004530
0.1466	-1.1829	0.004410
0.1526	-1.1551	0.004260
0.1587	-1.1233	0.004070
0.1650	-1.0866	0.003840
0.1714	-1.0459	0.003600
0.1780	-1.0069	0.003450
0.1847	-0.9770	0.003430
0.1915	-0.9576	0.003490
0.1985	-0.9449	0.003580
0.2057	-0.9364	0.003650
0.2129	-0.9246	0.003650
0.2204	-0.9079	0.003610
0.2279	-0.8905	0.003550
0.2356	-0.8678	0.003410
0.2435	-0.8322	0.003160
0.2515	-0.7836	0.002840
0.2596	-0.7289	0.002710
0.2678	-0.6869	0.002810
0.2762	-0.6709	0.002970
0.2847	-0.6684	0.003090
0.2933	-0.6665	0.003170
0.3021	-0.6631	0.003210
0.3109	-0.6585	0.003240
0.3199	-0.6546	0.003280
0.3290	-0.6533	0.003330
0.3382	-0.6530	0.003360
0.3475	-0.6521	0.003380
0.3569	-0.6505	0.003400
0.3664	-0.6485	0.003410
0.3760	-0.6463	0.003410
0.3856	-0.6442	0.003410
0.3954	-0.6419	0.003410
0.4051	-0.6394	0.003410
0.4150	-0.6368	0.003400
0.4249	-0.6340	0.003400
0.4349	-0.6312	0.003390
0.4449	-0.6284	0.003380
0.4550	-0.6255	0.003380
0.4651	-0.6227	0.003360
0.4752	-0.6198	0.003350
0.4854	-0.6169	0.003340
0.4955	-0.6141	0.003330
0.5057	-0.6112	0.003330
0.5159	-0.6084	0.003320
0.5260	-0.6055	0.003310
0.5362	-0.6026	0.003300
0.5463	-0.5997	0.003290
0.5564	-0.5966	0.003270
0.5665	-0.5933	0.003260
0.5765	-0.5898	0.003250
0.5865	-0.5860	0.003230
0.5964	-0.5820	0.003210
0.6063	-0.5775	0.003200
0.6160	-0.5727	0.003180
0.6258	-0.5674	0.003150
0.6354	-0.5612	0.003120
0.6449	-0.5537	0.003080
0.6544	-0.5452	0.003050
0.6637	-0.5360	0.003000
0.6730	-0.5261	0.002950
0.6821	-0.5153	0.002900
0.6912	-0.5037	0.002850
0.7000	-0.4912	0.002800
0.7088	-0.4781	0.002740
0.7175	-0.4644	0.002680
0.7260	-0.4506	0.002630
0.7343	-0.4371	0.002580
0.7426	-0.4242	0.002540
0.7507	-0.4123	0.002500
0.7587	-0.4008	0.002460
0.7666	-0.3896	0.002430
0.7743	-0.3793	0.002400
0.7819	-0.3698	0.002380
0.7893	-0.3612	0.002360
0.7966	-0.3530	0.002340
0.8038	-0.3452	0.002330
0.8108	-0.3376	0.002310
0.8177	-0.3298	0.002280
0.8244	-0.3218	0.002260
0.8310	-0.3134	0.002230
0.8374	-0.3045	0.002190
0.8436	-0.2950	0.002160
0.8497	-0.2849	0.002110
0.8556	-0.2743	0.002060
0.8614	-0.2631	0.002010
0.8670	-0.2514	0.001950
0.8725	-0.2394	0.001900
0.8778	-0.2270	0.001850
0.8831	-0.2144	0.001790
0.8882	-0.2014	0.001720
0.8932	-0.1880	0.001660
0.8980	-0.1743	0.001590
0.9027	-0.1603	0.001520
0.9073	-0.1462	0.001450
0.9118	-0.1319	0.001380
0.9162	-0.1176	0.001310
0.9205	-0.1033	0.001230
0.9247	-0.0892	0.001160
0.9288	-0.0790	0.001120
0.9327	-0.0652	0.001050
0.9366	-0.0517	0.000980
0.9404	-0.0386	0.000920
0.9441	-0.0258	0.000850
0.9477	-0.0134	0.000790
0.9512	-0.0015	0.000740
0.9546	0.0099	0.000680
0.9580	0.0209	0.000630
0.9612	0.0314	0.000580
0.9643	0.0413	0.000530
0.9674	0.0509	0.000490				
0.9704	0.0600	0.000450				
0.9733	0.0686	0.000410				
0.9761	0.0769	0.000370				
0.9789	0.0847	0.000340				
0.9815	0.0922	0.000310				
0.9841	0.0992	0.000270				
0.9866	0.1059	0.000240				
0.9890	0.1122	0.000220				
0.9914	0.1181	0.000200				
0.9936	0.1237	0.000220				
0.9958	0.1285	0.000300				
0.9980	0.1342	0.000770				
1.0000	0.1300	0.000770				
						
WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.7736	-0.002440
0.0000	0.7899	-0.001570
0.0002	0.7994	-0.000370
0.0004	0.8003	0.000230
0.0007	0.7939	0.000750
0.0011	0.7796	0.001250
0.0015	0.7588	0.001700
0.0021	0.7325	0.002090
0.0027	0.7021	0.002430
0.0034	0.6685	0.002720
0.0042	0.6328	0.002960
0.0050	0.5958	0.003160
0.0059	0.5582	0.003330
0.0069	0.5205	0.003470
0.0080	0.4831	0.003590
0.0091	0.4464	0.003690
0.0103	0.4107	0.003770
0.0115	0.3763	0.003840
0.0128	0.3433	0.003890
0.0142	0.3119	0.003920
0.0157	0.2821	0.003950
0.0173	0.2538	0.003970
0.0189	0.2267	0.004010
0.0206	0.2003	0.004050
0.0224	0.1754	0.004070
0.0243	0.1525	0.004070
0.0262	0.1311	0.004070
0.0283	0.1112	0.004070
0.0304	0.0927	0.004060
0.0326	0.0753	0.004060
0.0349	0.0591	0.004060
0.0374	0.0437	0.004050
0.0399	0.0292	0.004050
0.0425	0.0154	0.004040
0.0452	0.0022	0.004030
0.0480	-0.0103	0.004030
0.0510	-0.0221	0.004020
0.0540	-0.0333	0.004010
0.0571	-0.0438	0.003990
0.0604	-0.0535	0.003980
0.0637	-0.0628	0.003960
0.0672	-0.0719	0.003960
0.0708	-0.0811	0.003950
0.0746	-0.0902	0.003950
0.0784	-0.0991	0.003940
0.0824	-0.1078	0.003930
0.0865	-0.1164	0.003930
0.0907	-0.1248	0.003920
0.0950	-0.1330	0.003920
0.0995	-0.1413	0.003920
0.1041	-0.1494	0.003910
0.1088	-0.1576	0.003910
0.1137	-0.1658	0.003910
0.1187	-0.1739	0.003910
0.1238	-0.1821	0.003910
0.1291	-0.1903	0.003910
0.1345	-0.1985	0.003910
0.1401	-0.2066	0.003910
0.1457	-0.2146	0.003900
0.1516	-0.2224	0.003900
0.1575	-0.2299	0.003900
0.1636	-0.2371	0.003890
0.1699	-0.2439	0.003880
0.1763	-0.2504	0.003880
0.1828	-0.2568	0.003870
0.1895	-0.2632	0.003870
0.1964	-0.2700	0.003870
0.2034	-0.2772	0.003870
0.2105	-0.2849	0.003880
0.2178	-0.2932	0.003890
0.2252	-0.3021	0.003900
0.2327	-0.3114	0.003910
0.2404	-0.3208	0.003920
0.2482	-0.3295	0.003920
0.2561	-0.3374	0.003920
0.2642	-0.3450	0.003910
0.2724	-0.3518	0.003900
0.2807	-0.3572	0.003880
0.2892	-0.3616	0.003860
0.2977	-0.3652	0.003840
0.3064	-0.3688	0.003830
0.3153	-0.3728	0.003820
0.3242	-0.3774	0.003820
0.3332	-0.3822	0.003810
0.3423	-0.3859	0.003790
0.3516	-0.3877	0.003760
0.3609	-0.3884	0.003730
0.3702	-0.3879	0.003700
0.3797	-0.3863	0.003660
0.3893	-0.3840	0.003630
0.3989	-0.3810	0.003600
0.4086	-0.3778	0.003560
0.4184	-0.3741	0.003520
0.4282	-0.3703	0.003490
0.4381	-0.3662	0.003460
0.4480	-0.3616	0.003430
0.4580	-0.3564	0.003390
0.4680	-0.3511	0.003360
0.4780	-0.3456	0.003320
0.4881	-0.3399	0.003290
0.4981	-0.3333	0.003260
0.5081	-0.3250	0.003200
0.5181	-0.3142	0.003140
0.5281	-0.3005	0.003060
0.5381	-0.2843	0.002970
0.5481	-0.2661	0.002870
0.5580	-0.2464	0.002770
0.5680	-0.2258	0.002670
0.5779	-0.2048	0.002580
0.5878	-0.1836	0.002490
0.5976	-0.1625	0.002410
0.6074	-0.1414	0.002320
0.6170	-0.1201	0.002240
0.6266	-0.0987	0.002150
0.6361	-0.0777	0.002060
0.6455	-0.0568	0.001980
0.6548	-0.0361	0.001900
0.6639	-0.0155	0.001820
0.6729	0.0049	0.001740
0.6817	0.0250	0.001660
0.6904	0.0450	0.001580
0.6988	0.0647	0.001500
0.7071	0.0842	0.001420
0.7153	0.1035	0.001340
0.7232	0.1226	0.001260
0.7311	0.1410	0.001190
0.7388	0.1584	0.001130
0.7465	0.1748	0.001070
0.7540	0.1900	0.001030
0.7614	0.2040	0.000990
0.7687	0.2170	0.000950
0.7760	0.2289	0.000930
0.7832	0.2398	0.000910
0.7903	0.2497	0.000890
0.7974	0.2586	0.000890
0.8044	0.2664	0.000890
0.8113	0.2733	0.000890
0.8181	0.2792	0.000900
0.8247	0.2843	0.000920
0.8313	0.2886	0.000940
0.8377	0.2920	0.000960
0.8441	0.2947	0.000980
0.8503	0.2966	0.001010
0.8563	0.2980	0.001040
0.8623	0.2987	0.001070
0.8681	0.2989	0.001100
0.8738	0.2985	0.001140
0.8793	0.2977	0.001170
0.8848	0.2966	0.001210
0.8901	0.2950	0.001240
0.8952	0.2932	0.001280
0.9003	0.2912	0.001310
0.9052	0.2889	0.001350
0.9100	0.2864	0.001380
0.9147	0.2838	0.001420
0.9193	0.2810	0.001450
0.9238	0.2781	0.001480
0.9281	0.2751	0.001510
0.9323	0.2720	0.001540
0.9364	0.2687	0.001570
0.9404	0.2654	0.001610
0.9443	0.2620	0.001640
0.9481	0.2585	0.001670
0.9518	0.2549	0.001700
0.9554	0.2511	0.001730
0.9588	0.2472	0.001770
0.9622	0.2431	0.001800
0.9655	0.2389	0.001840
0.9687	0.2344	0.001880
0.9718	0.2297	0.001910
0.9748	0.2246	0.001950
0.9777	0.2192	0.002000
0.9805	0.2134	0.002050
0.9832	0.2070	0.002100
0.9858	0.2000	0.002160
0.9884	0.1921	0.002230				
0.9909	0.1829	0.002320				
0.9933	0.1719	0.002470				
0.9956	0.1582	0.002830				
0.9978	0.1401	0.004700				
1.0000	0.1177	0.004700				
						
WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7723	0.003910				
0.0000	0.7491	0.003460				
0.0002	0.7000	0.002990				
0.0004	0.6552	0.003200				
0.0007	0.5995	0.003740				
0.0010	0.5360	0.004260				
0.0015	0.4666	0.004690				
0.0020	0.3953	0.005010
0.0026	0.3249	0.005240
0.0033	0.2558	0.005460
0.0041	0.1865	0.005680
0.0049	0.1168	0.005890
0.0058	0.0471	0.006080
0.0068	-0.0219	0.006230
0.0079	-0.0895	0.006370
0.0090	-0.1566	0.006510
0.0101	-0.2238	0.006650
0.0114	-0.2905	0.006770
0.0126	-0.3557	0.006860
0.0140	-0.4194	0.006940
0.0154	-0.4820	0.007020
0.0170	-0.5444	0.007120
0.0185	-0.6081	0.007250
0.0202	-0.6754	0.007420
0.0219	-0.7486	0.007660
0.0237	-0.8298	0.007940
0.0255	-0.9168	0.008060
0.0273	-0.9956	0.007860
0.0293	-1.0548	0.007490
0.0314	-1.0965	0.007130
0.0336	-1.1253	0.006830
0.0360	-1.1453	0.006610
0.0385	-1.1601	0.006450
0.0411	-1.1725	0.006340
0.0438	-1.1846	0.006270
0.0465	-1.1970	0.006210
0.0494	-1.2085	0.006110
0.0525	-1.2162	0.005970
0.0556	-1.2183	0.005850
0.0589	-1.2205	0.005810
0.0623	-1.2254	0.005780
0.0658	-1.2295	0.005720
0.0694	-1.2327	0.005660
0.0732	-1.2350	0.005600
0.0771	-1.2365	0.005540
0.0811	-1.2372	0.005480
0.0852	-1.2371	0.005430
0.0895	-1.2365	0.005370
0.0939	-1.2354	0.005320
0.0984	-1.2341	0.005270
0.1031	-1.2326	0.005230
0.1079	-1.2308	0.005180
0.1129	-1.2287	0.005140
0.1179	-1.2258	0.005090
0.1231	-1.2225	0.005060
0.1285	-1.2194	0.005020
0.1340	-1.2161	0.004980
0.1396	-1.2120	0.004940
0.1454	-1.2073	0.004890
0.1514	-1.2023	0.004850
0.1574	-1.1970	0.004810
0.1637	-1.1914	0.004780
0.1700	-1.1856	0.004740
0.1765	-1.1794	0.004700
0.1832	-1.1729	0.004670
0.1900	-1.1659	0.004620
0.1969	-1.1574	0.004560
0.2040	-1.1437	0.004410
0.2112	-1.1140	0.004000
0.2186	-1.0224	0.002850
0.2261	-0.8785	0.001490
0.2338	-0.7311	0.001070
0.2416	-0.6295	0.001430
0.2495	-0.5969	0.001890
0.2576	-0.5921	0.002270
0.2658	-0.5961	0.002600
0.2741	-0.6047	0.002870
0.2826	-0.6158	0.003090
0.2912	-0.6279	0.003280
0.2999	-0.6401	0.003420
0.3087	-0.6518	0.003540
0.3177	-0.6628	0.003630
0.3267	-0.6728	0.003700
0.3359	-0.6818	0.003750
0.3451	-0.6896	0.003780
0.3545	-0.6961	0.003800
0.3640	-0.7014	0.003820
0.3735	-0.7056	0.003830
0.3832	-0.7089	0.003820
0.3929	-0.7114	0.003820
0.4026	-0.7133	0.003820
0.4125	-0.7146	0.003810
0.4224	-0.7152	0.003810
0.4324	-0.7154	0.003800
0.4424	-0.7153	0.003780
0.4524	-0.7150	0.003770
0.4625	-0.7145	0.003760
0.4726	-0.7138	0.003750
0.4828	-0.7130	0.003740
0.4929	-0.7122	0.003720
0.5031	-0.7113	0.003710
0.5133	-0.7104	0.003700
0.5234	-0.7096	0.003690
0.5336	-0.7089	0.003680
0.5437	-0.7084	0.003680
0.5538	-0.7080	0.003670
0.5639	-0.7078	0.003670
0.5740	-0.7075	0.003660
0.5840	-0.7071	0.003650
0.5939	-0.7062	0.003640
0.6038	-0.7043	0.003620
0.6136	-0.7008	0.003580
0.6233	-0.6950	0.003530
0.6330	-0.6868	0.003480
0.6425	-0.6771	0.003410
0.6520	-0.6659	0.003340
0.6614	-0.6522	0.003260
0.6707	-0.6366	0.003170
0.6798	-0.6197	0.003090
0.6889	-0.6019	0.003000
0.6978	-0.5833	0.002920
0.7066	-0.5642	0.002830
0.7152	-0.5450	0.002750
0.7238	-0.5260	0.002670
0.7322	-0.5073	0.002600
0.7405	-0.4893	0.002540
0.7486	-0.4722	0.002480
0.7567	-0.4556	0.002430
0.7646	-0.4394	0.002370
0.7723	-0.4238	0.002320
0.7799	-0.4086	0.002270
0.7874	-0.3939	0.002220
0.7947	-0.3796	0.002170
0.8019	-0.3656	0.002130
0.8090	-0.3519	0.002080
0.8159	-0.3384	0.002040
0.8226	-0.3251	0.002000
0.8292	-0.3119	0.001950
0.8356	-0.2988	0.001900
0.8419	-0.2857	0.001850
0.8480	-0.2726	0.001800
0.8540	-0.2594	0.001750
0.8598	-0.2462	0.001700
0.8654	-0.2329	0.001640
0.8710	-0.2193	0.001580
0.8764	-0.2057	0.001520
0.8816	-0.1924	0.001470
0.8868	-0.1792	0.001420
0.8918	-0.1661	0.001360
0.8967	-0.1530	0.001300
0.9014	-0.1400	0.001250
0.9061	-0.1270	0.001190
0.9106	-0.1140	0.001130
0.9151	-0.1012	0.001070
0.9194	-0.0886	0.001010
0.9236	-0.0761	0.000950
0.9278	-0.0639	0.000890
0.9318	-0.0520	0.000830
0.9357	-0.0403	0.000780
0.9395	-0.0289	0.000730
0.9433	-0.0178	0.000680
0.9469	-0.0071	0.000630
0.9505	0.0033	0.000580
0.9539	0.0133	0.000530
0.9573	0.0229	0.000490
0.9606	0.0321	0.000450
0.9638	0.0410	0.000410
0.9669	0.0494	0.000370				
0.9700	0.0575	0.000330				
0.9729	0.0652	0.000300				
0.9758	0.0726	0.000260				
0.9785	0.0795	0.000230				
0.9812	0.0862	0.000200				
0.9839	0.0924	0.000180				
0.9864	0.0983	0.000150				
0.9889	0.1038	0.000130				
0.9912	0.1090	0.000130				
0.9935	0.1140	0.000150				
0.9958	0.1182	0.000240				
0.9979	0.1235	0.000690				
1.0000	0.1197	0.000690				
						
WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.7740	-0.002380
0.0001	0.7952	-0.001390
0.0002	0.8024	0.000010
0.0005	0.7955	0.000770
0.0009	0.7796	0.001400
0.0014	0.7551	0.001950
0.0020	0.7248	0.002410
0.0026	0.6898	0.002820
0.0033	0.6517	0.003150
0.0040	0.6116	0.003410
0.0049	0.5710	0.003610
0.0057	0.5310	0.003750
0.0067	0.4918	0.003860
0.0077	0.4536	0.003950
0.0087	0.4166	0.004020
0.0099	0.3810	0.004080
0.0111	0.3468	0.004120
0.0123	0.3143	0.004150
0.0136	0.2836	0.004170
0.0150	0.2549	0.004170
0.0165	0.2283	0.004160
0.0180	0.2039	0.004150
0.0196	0.1814	0.004140
0.0214	0.1597	0.004160
0.0231	0.1381	0.004180
0.0250	0.1181	0.004170
0.0269	0.1004	0.004150
0.0290	0.0843	0.004120
0.0311	0.0695	0.004100
0.0333	0.0560	0.004080
0.0356	0.0435	0.004060
0.0380	0.0319	0.004050
0.0406	0.0209	0.004030
0.0432	0.0106	0.004020
0.0459	0.0007	0.004000
0.0488	-0.0088	0.003990
0.0517	-0.0179	0.003980
0.0548	-0.0266	0.003970
0.0579	-0.0349	0.003950
0.0612	-0.0427	0.003940
0.0646	-0.0501	0.003920
0.0681	-0.0572	0.003910
0.0718	-0.0645	0.003910
0.0755	-0.0719	0.003900
0.0794	-0.0793	0.003900
0.0834	-0.0866	0.003890
0.0875	-0.0941	0.003890
0.0918	-0.1015	0.003890
0.0962	-0.1090	0.003890
0.1007	-0.1167	0.003890
0.1054	-0.1244	0.003890
0.1101	-0.1323	0.003890
0.1151	-0.1404	0.003900
0.1201	-0.1486	0.003900
0.1253	-0.1569	0.003910
0.1306	-0.1654	0.003910
0.1360	-0.1740	0.003920
0.1416	-0.1826	0.003920
0.1473	-0.1911	0.003920
0.1532	-0.1996	0.003930
0.1592	-0.2079	0.003930
0.1653	-0.2161	0.003930
0.1716	-0.2243	0.003930
0.1780	-0.2327	0.003940
0.1846	-0.2414	0.003940
0.1913	-0.2503	0.003950
0.1982	-0.2590	0.003950
0.2052	-0.2677	0.003960
0.2123	-0.2765	0.003960
0.2196	-0.2854	0.003970
0.2270	-0.2946	0.003980
0.2345	-0.3042	0.003990
0.2422	-0.3140	0.004000
0.2500	-0.3237	0.004000
0.2580	-0.3326	0.004000
0.2660	-0.3406	0.003990
0.2742	-0.3477	0.003980
0.2825	-0.3536	0.003960
0.2909	-0.3586	0.003940
0.2995	-0.3630	0.003920
0.3082	-0.3670	0.003910
0.3170	-0.3711	0.003900
0.3259	-0.3751	0.003880
0.3349	-0.3787	0.003860
0.3439	-0.3806	0.003830
0.3531	-0.3806	0.003790
0.3624	-0.3801	0.003760
0.3717	-0.3792	0.003730
0.3811	-0.3776	0.003700
0.3906	-0.3756	0.003670
0.4002	-0.3728	0.003640
0.4098	-0.3694	0.003600
0.4195	-0.3646	0.003550
0.4293	-0.3589	0.003510
0.4390	-0.3534	0.003470
0.4489	-0.3477	0.003430
0.4587	-0.3411	0.003390
0.4686	-0.3334	0.003340
0.4785	-0.3246	0.003280
0.4884	-0.3148	0.003230
0.4984	-0.3043	0.003170
0.5083	-0.2930	0.003110
0.5182	-0.2804	0.003040
0.5281	-0.2659	0.002960
0.5380	-0.2501	0.002880
0.5479	-0.2333	0.002800
0.5577	-0.2155	0.002720
0.5675	-0.1972	0.002640
0.5773	-0.1784	0.002560
0.5870	-0.1594	0.002480
0.5967	-0.1401	0.002390
0.6063	-0.1207	0.002310
0.6158	-0.1011	0.002230
0.6252	-0.0815	0.002150
0.6344	-0.0621	0.002070
0.6435	-0.0426	0.001990
0.6528	-0.0229	0.001900
0.6619	-0.0030	0.001810
0.6709	0.0167	0.001730
0.6798	0.0361	0.001660
0.6884	0.0551	0.001570
0.6969	0.0737	0.001490
0.7052	0.0919	0.001420
0.7134	0.1098	0.001340
0.7214	0.1277	0.001250
0.7292	0.1454	0.001180
0.7370	0.1625	0.001110
0.7446	0.1778	0.001040
0.7522	0.1933	0.001000
0.7596	0.2070	0.000990
0.7670	0.2186	0.000960
0.7743	0.2306	0.000930
0.7815	0.2419	0.000900
0.7887	0.2525	0.000870
0.7959	0.2623	0.000860
0.8029	0.2711	0.000850
0.8099	0.2790	0.000840
0.8167	0.2860	0.000840
0.8235	0.2920	0.000860
0.8301	0.2970	0.000870
0.8366	0.3010	0.000900
0.8430	0.3040	0.000930
0.8493	0.3062	0.000960
0.8554	0.3076	0.000990
0.8614	0.3082	0.001030
0.8672	0.3082	0.001080
0.8730	0.3076	0.001120
0.8786	0.3064	0.001160
0.8841	0.3047	0.001200
0.8894	0.3027	0.001240
0.8946	0.3003	0.001280
0.8997	0.2976	0.001320
0.9047	0.2947	0.001370
0.9095	0.2916	0.001410
0.9142	0.2884	0.001440
0.9188	0.2850	0.001480
0.9233	0.2816	0.001520
0.9277	0.2780	0.001560
0.9319	0.2743	0.001600
0.9360	0.2705	0.001630
0.9401	0.2666	0.001670
0.9440	0.2625	0.001700
0.9478	0.2583	0.001740
0.9515	0.2540	0.001780
0.9551	0.2494	0.001820
0.9586	0.2446	0.001860
0.9620	0.2396	0.001910
0.9653	0.2343	0.001950
0.9685	0.2287	0.002000
0.9716	0.2228	0.002040
0.9746	0.2165	0.002100
0.9775	0.2098	0.002160
0.9804	0.2026	0.002210
0.9831	0.1948	0.002280
0.9857	0.1863	0.002350
0.9883	0.1769	0.002430				
0.9908	0.1663	0.002540				
0.9932	0.1538	0.002700				
0.9956	0.1386	0.003090				
0.9978	0.1190	0.005100				
1.0000	0.0962	0.005100				
						
WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.7734	0.004370				
0.0001	0.7434	0.004060				
0.0002	0.6748	0.003740				
0.0005	0.6149	0.003980				
0.0009	0.5467	0.004450				
0.0014	0.4769	0.004850				
0.0020	0.4064	0.005210				
0.0026	0.3346	0.005480
0.0034	0.2658	0.005640
0.0041	0.2005	0.005790
0.0050	0.1356	0.005960
0.0059	0.0705	0.006130
0.0069	0.0053	0.006290
0.0079	-0.0594	0.006440
0.0090	-0.1231	0.006570
0.0101	-0.1862	0.006690
0.0113	-0.2487	0.006790
0.0126	-0.3102	0.006880
0.0139	-0.3708	0.006970
0.0153	-0.4310	0.007060
0.0167	-0.4919	0.007180
0.0182	-0.5550	0.007340
0.0198	-0.6225	0.007550
0.0214	-0.6965	0.007840
0.0231	-0.7790	0.008190
0.0248	-0.8691	0.008450
0.0264	-0.9565	0.008330
0.0282	-1.0261	0.007900
0.0302	-1.0748	0.007460
0.0322	-1.1084	0.007090
0.0344	-1.1302	0.006790
0.0368	-1.1438	0.006550
0.0392	-1.1522	0.006390
0.0418	-1.1581	0.006270
0.0444	-1.1635	0.006190
0.0472	-1.1692	0.006120
0.0501	-1.1741	0.006020
0.0531	-1.1753	0.005880
0.0563	-1.1711	0.005780
0.0596	-1.1679	0.005740
0.0629	-1.1684	0.005720
0.0664	-1.1685	0.005660
0.0701	-1.1680	0.005610
0.0738	-1.1667	0.005550
0.0777	-1.1648	0.005490
0.0817	-1.1622	0.005430
0.0859	-1.1588	0.005380
0.0901	-1.1549	0.005320
0.0945	-1.1508	0.005270
0.0991	-1.1466	0.005230
0.1037	-1.1426	0.005200
0.1085	-1.1387	0.005160
0.1134	-1.1347	0.005120
0.1185	-1.1303	0.005080
0.1237	-1.1264	0.005060
0.1291	-1.1238	0.005040
0.1346	-1.1213	0.005000
0.1402	-1.1176	0.004960
0.1460	-1.1133	0.004920
0.1519	-1.1085	0.004890
0.1580	-1.1038	0.004850
0.1642	-1.0992	0.004820
0.1706	-1.0943	0.004790
0.1771	-1.0885	0.004750
0.1837	-1.0826	0.004710
0.1905	-1.0765	0.004670
0.1974	-1.0676	0.004570
0.2045	-1.0509	0.004310
0.2117	-1.0059	0.003570
0.2191	-0.9005	0.002420
0.2266	-0.7656	0.001790
0.2342	-0.6562	0.002010
0.2420	-0.6078	0.002500
0.2499	-0.6087	0.002880
0.2580	-0.6180	0.003160
0.2662	-0.6308	0.003380
0.2745	-0.6448	0.003560
0.2829	-0.6591	0.003700
0.2915	-0.6728	0.003810
0.3002	-0.6856	0.003890
0.3090	-0.6971	0.003950
0.3179	-0.7075	0.004000
0.3269	-0.7169	0.004040
0.3361	-0.7250	0.004060
0.3453	-0.7316	0.004070
0.3546	-0.7368	0.004070
0.3640	-0.7410	0.004070
0.3735	-0.7448	0.004070
0.3831	-0.7485	0.004070
0.3928	-0.7519	0.004070
0.4025	-0.7549	0.004060
0.4123	-0.7575	0.004060
0.4221	-0.7597	0.004050
0.4320	-0.7615	0.004040
0.4420	-0.7629	0.004030
0.4519	-0.7639	0.004010
0.4620	-0.7645	0.004000
0.4720	-0.7649	0.003990
0.4820	-0.7651	0.003970
0.4921	-0.7652	0.003960
0.5022	-0.7653	0.003950
0.5122	-0.7655	0.003940
0.5223	-0.7659	0.003930
0.5324	-0.7667	0.003930
0.5424	-0.7681	0.003930
0.5524	-0.7699	0.003930
0.5625	-0.7722	0.003940
0.5725	-0.7750	0.003940
0.5825	-0.7782	0.003950
0.5925	-0.7815	0.003950
0.6024	-0.7843	0.003950
0.6122	-0.7860	0.003930
0.6219	-0.7855	0.003890
0.6316	-0.7812	0.003820
0.6411	-0.7719	0.003710
0.6506	-0.7559	0.003560
0.6600	-0.7333	0.003400
0.6693	-0.7088	0.003290
0.6784	-0.6877	0.003210
0.6875	-0.6680	0.003110
0.6964	-0.6469	0.003020
0.7052	-0.6254	0.002930
0.7139	-0.6040	0.002840
0.7224	-0.5828	0.002760
0.7309	-0.5621	0.002680
0.7392	-0.5420	0.002610
0.7473	-0.5228	0.002540
0.7554	-0.5041	0.002470
0.7633	-0.4855	0.002410
0.7710	-0.4672	0.002340
0.7787	-0.4494	0.002280
0.7862	-0.4320	0.002220
0.7935	-0.4151	0.002160
0.8007	-0.3986	0.002100
0.8078	-0.3824	0.002040
0.8147	-0.3666	0.001990
0.8215	-0.3513	0.001930
0.8281	-0.3362	0.001890
0.8346	-0.3215	0.001830
0.8409	-0.3070	0.001780
0.8470	-0.2928	0.001720
0.8530	-0.2789	0.001670
0.8588	-0.2651	0.001620
0.8645	-0.2515	0.001570
0.8700	-0.2380	0.001510
0.8754	-0.2245	0.001460
0.8807	-0.2111	0.001410
0.8859	-0.1978	0.001350
0.8909	-0.1848	0.001300
0.8959	-0.1719	0.001240
0.9007	-0.1592	0.001200
0.9053	-0.1466	0.001140
0.9099	-0.1342	0.001090
0.9144	-0.1219	0.001030
0.9187	-0.1098	0.000980
0.9230	-0.0979	0.000930
0.9271	-0.0862	0.000870
0.9312	-0.0748	0.000820
0.9351	-0.0636	0.000770
0.9390	-0.0526	0.000720
0.9428	-0.0419	0.000670
0.9464	-0.0316	0.000620
0.9500	-0.0214	0.000580
0.9535	-0.0116	0.000530
0.9569	-0.0022	0.000490
0.9602	0.0070	0.000440
0.9635	0.0158	0.000400
0.9666	0.0244	0.000360				
0.9697	0.0325	0.000320				
0.9726	0.0404	0.000290				
0.9755	0.0479	0.000250				
0.9783	0.0551	0.000230				
0.9811	0.0619	0.000200				
0.9837	0.0684	0.000170				
0.9863	0.0745	0.000140				
0.9888	0.0802	0.000120				
0.9912	0.0856	0.000110				
0.9935	0.0908	0.000140				
0.9957	0.0952	0.000230				
0.9979	0.1009	0.000690				
1.0000	0.0977	0.000690				
						
WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.8050	-0.001750
0.0001	0.8220	-0.000790
0.0004	0.8153	0.000660
0.0007	0.7953	0.001480
0.0012	0.7676	0.002120
0.0018	0.7332	0.002680
0.0024	0.6944	0.003140
0.0031	0.6528	0.003500
0.0038	0.6100	0.003770
0.0046	0.5671	0.003980
0.0055	0.5252	0.004130
0.0064	0.4846	0.004230
0.0073	0.4458	0.004280
0.0084	0.4088	0.004320
0.0095	0.3738	0.004350
0.0106	0.3406	0.004350
0.0118	0.3094	0.004350
0.0131	0.2801	0.004340
0.0145	0.2524	0.004330
0.0159	0.2267	0.004320
0.0174	0.2031	0.004280
0.0189	0.1822	0.004240
0.0206	0.1632	0.004220
0.0224	0.1447	0.004220
0.0242	0.1272	0.004200
0.0261	0.1108	0.004180
0.0281	0.0959	0.004160
0.0302	0.0824	0.004130
0.0323	0.0701	0.004100
0.0346	0.0589	0.004070
0.0370	0.0487	0.004050
0.0395	0.0394	0.004020
0.0421	0.0307	0.003990
0.0448	0.0226	0.003970
0.0476	0.0148	0.003950
0.0505	0.0073	0.003940
0.0536	-0.0002	0.003920
0.0567	-0.0076	0.003910
0.0600	-0.0150	0.003910
0.0634	-0.0224	0.003900
0.0669	-0.0298	0.003890
0.0706	-0.0371	0.003880
0.0743	-0.0442	0.003870
0.0782	-0.0512	0.003860
0.0822	-0.0580	0.003850
0.0863	-0.0647	0.003840
0.0906	-0.0719	0.003840
0.0950	-0.0797	0.003850
0.0996	-0.0878	0.003860
0.1043	-0.0963	0.003860
0.1091	-0.1050	0.003870
0.1140	-0.1139	0.003880
0.1191	-0.1230	0.003880
0.1243	-0.1322	0.003890
0.1296	-0.1416	0.003890
0.1351	-0.1510	0.003900
0.1407	-0.1605	0.003910
0.1465	-0.1701	0.003910
0.1524	-0.1797	0.003920
0.1584	-0.1893	0.003920
0.1646	-0.1989	0.003930
0.1710	-0.2085	0.003930
0.1774	-0.2183	0.003940
0.1841	-0.2283	0.003950
0.1908	-0.2385	0.003950
0.1977	-0.2486	0.003960
0.2048	-0.2588	0.003970
0.2120	-0.2689	0.003970
0.2193	-0.2790	0.003980
0.2268	-0.2891	0.003980
0.2344	-0.2991	0.003990
0.2422	-0.3089	0.003990
0.2501	-0.3183	0.003980
0.2581	-0.3271	0.003980
0.2663	-0.3353	0.003970
0.2746	-0.3428	0.003950
0.2830	-0.3494	0.003940
0.2915	-0.3552	0.003920
0.3002	-0.3602	0.003890
0.3090	-0.3643	0.003870
0.3179	-0.3675	0.003840
0.3269	-0.3700	0.003810
0.3360	-0.3716	0.003780
0.3453	-0.3722	0.003740
0.3546	-0.3719	0.003710
0.3640	-0.3707	0.003670
0.3735	-0.3687	0.003630
0.3831	-0.3660	0.003590
0.3928	-0.3625	0.003550
0.4025	-0.3584	0.003510
0.4124	-0.3541	0.003440
0.4217	-0.3444	0.003370
0.4316	-0.3366	0.003340
0.4415	-0.3332	0.003310
0.4515	-0.3266	0.003260
0.4615	-0.3188	0.003210
0.4716	-0.3094	0.003150
0.4817	-0.2988	0.003080
0.4918	-0.2871	0.003010
0.5020	-0.2745	0.002950
0.5122	-0.2611	0.002880
0.5223	-0.2469	0.002810
0.5325	-0.2320	0.002740
0.5427	-0.2164	0.002670
0.5529	-0.2002	0.002590
0.5630	-0.1835	0.002520
0.5732	-0.1663	0.002440
0.5833	-0.1488	0.002370
0.5933	-0.1308	0.002290
0.6034	-0.1126	0.002220
0.6134	-0.0941	0.002140
0.6233	-0.0756	0.002060
0.6331	-0.0570	0.001980
0.6427	-0.0385	0.001900
0.6523	-0.0200	0.001830
0.6617	-0.0016	0.001750
0.6710	0.0167	0.001680
0.6800	0.0347	0.001600
0.6889	0.0524	0.001520
0.6975	0.0698	0.001450
0.7059	0.0868	0.001380
0.7140	0.1037	0.001310
0.7220	0.1205	0.001230
0.7297	0.1374	0.001150
0.7373	0.1543	0.001080
0.7447	0.1710	0.001020
0.7519	0.1874	0.000950
0.7590	0.2028	0.000890
0.7660	0.2164	0.000830
0.7726	0.2319	0.000780
0.7794	0.2447	0.000770
0.7861	0.2527	0.000760
0.7928	0.2620	0.000750
0.7995	0.2704	0.000740
0.8061	0.2782	0.000730
0.8127	0.2851	0.000740
0.8192	0.2911	0.000750
0.8256	0.2961	0.000770
0.8319	0.3002	0.000790
0.8381	0.3034	0.000820
0.8442	0.3058	0.000850
0.8502	0.3073	0.000880
0.8561	0.3081	0.000910
0.8618	0.3082	0.000950
0.8674	0.3077	0.001000
0.8729	0.3066	0.001040
0.8782	0.3050	0.001080
0.8835	0.3029	0.001130
0.8886	0.3004	0.001170
0.8936	0.2976	0.001220
0.8984	0.2946	0.001260
0.9032	0.2960	0.001400
0.9079	0.2931	0.001440
0.9124	0.2901	0.001480
0.9169	0.2870	0.001520
0.9212	0.2838	0.001550
0.9254	0.2805	0.001590
0.9295	0.2771	0.001620
0.9336	0.2736	0.001660
0.9375	0.2700	0.001690
0.9413	0.2662	0.001730
0.9451	0.2623	0.001770
0.9487	0.2581	0.001810
0.9523	0.2537	0.001850
0.9557	0.2490	0.001890
0.9591	0.2441	0.001930
0.9624	0.2388	0.001980
0.9656	0.2332	0.002020
0.9687	0.2272	0.002070
0.9717	0.2208	0.002130
0.9747	0.2139	0.002180
0.9775	0.2065	0.002240
0.9803	0.1986	0.002310
0.9830	0.1901	0.002380
0.9856	0.1808	0.002450
0.9882	0.1705	0.002540				
0.9907	0.1588	0.002650				
0.9931	0.1453	0.002830				
0.9954	0.1288	0.003240				
0.9977	0.1086	0.005220				
0.9999	0.0846	0.005220				
						
WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8054	0.003970				
0.0000	0.7784	0.003920				
0.0002	0.7062	0.003950				
0.0005	0.6392	0.004260				
0.0010	0.5660	0.004690				
0.0015	0.4930	0.005080				
0.0021	0.4197	0.005410				
0.0028	0.3479	0.005640
0.0036	0.2778	0.005810
0.0044	0.2109	0.005960
0.0053	0.1461	0.006100
0.0063	0.0821	0.006240
0.0073	0.0181	0.006390
0.0084	-0.0465	0.006560
0.0095	-0.1119	0.006710
0.0107	-0.1773	0.006850
0.0119	-0.2414	0.006950
0.0132	-0.3040	0.007030
0.0146	-0.3648	0.007080
0.0160	-0.4241	0.007100
0.0175	-0.4829	0.007200
0.0191	-0.5482	0.007560
0.0207	-0.6310	0.008140
0.0223	-0.7259	0.008560
0.0239	-0.8217	0.008690
0.0256	-0.9150	0.008600
0.0273	-0.9943	0.008280
0.0292	-1.0522	0.007830
0.0312	-1.0904	0.007340
0.0333	-1.1155	0.006920
0.0355	-1.1263	0.006610
0.0380	-1.1298	0.006420
0.0405	-1.1341	0.006280
0.0431	-1.1345	0.006140
0.0459	-1.1325	0.006010
0.0488	-1.1292	0.005910
0.0518	-1.1253	0.005820
0.0549	-1.1209	0.005750
0.0582	-1.1164	0.005680
0.0615	-1.1121	0.005620
0.0650	-1.1085	0.005570
0.0686	-1.1054	0.005530
0.0724	-1.1025	0.005470
0.0763	-1.0992	0.005410
0.0803	-1.0941	0.005320
0.0844	-1.0863	0.005220
0.0887	-1.0774	0.005170
0.0932	-1.0708	0.005150
0.0977	-1.0664	0.005130
0.1024	-1.0623	0.005090
0.1072	-1.0588	0.005060
0.1121	-1.0557	0.005040
0.1172	-1.0528	0.005010
0.1225	-1.0499	0.004980
0.1278	-1.0470	0.004940
0.1333	-1.0440	0.004910
0.1390	-1.0406	0.004870
0.1448	-1.0369	0.004830
0.1508	-1.0329	0.004790
0.1569	-1.0285	0.004750
0.1632	-1.0239	0.004720
0.1696	-1.0190	0.004680
0.1762	-1.0137	0.004640
0.1829	-1.0071	0.004570
0.1897	-0.9973	0.004430
0.1968	-0.9781	0.004080
0.2039	-0.9355	0.003400
0.2112	-0.8574	0.002680
0.2187	-0.7589	0.002410
0.2263	-0.6759	0.002630
0.2340	-0.6337	0.003010
0.2419	-0.6306	0.003340
0.2499	-0.6434	0.003540
0.2581	-0.6570	0.003700
0.2664	-0.6709	0.003820
0.2749	-0.6844	0.003910
0.2835	-0.6970	0.003970
0.2922	-0.7086	0.004020
0.3010	-0.7193	0.004060
0.3100	-0.7290	0.004080
0.3191	-0.7378	0.004100
0.3283	-0.7457	0.004110
0.3376	-0.7528	0.004110
0.3470	-0.7589	0.004110
0.3565	-0.7640	0.004100
0.3662	-0.7683	0.004090
0.3759	-0.7719	0.004080
0.3857	-0.7751	0.004060
0.3956	-0.7780	0.004050
0.4055	-0.7805	0.004030
0.4156	-0.7827	0.004020
0.4257	-0.7845	0.004000
0.4358	-0.7858	0.003990
0.4460	-0.7869	0.003970
0.4563	-0.7877	0.003950
0.4666	-0.7882	0.003940
0.4769	-0.7887	0.003920
0.4873	-0.7892	0.003910
0.4977	-0.7898	0.003900
0.5080	-0.7906	0.003900
0.5184	-0.7917	0.003890
0.5288	-0.7933	0.003890
0.5392	-0.7955	0.003890
0.5496	-0.7982	0.003900
0.5599	-0.8016	0.003900
0.5703	-0.8056	0.003910
0.5805	-0.8099	0.003920
0.5908	-0.8141	0.003920
0.6010	-0.8176	0.003910
0.6111	-0.8206	0.003900
0.6212	-0.8235	0.003880
0.6312	-0.8244	0.003840
0.6411	-0.8197	0.003730
0.6508	-0.8058	0.003550
0.6605	-0.7807	0.003310
0.6701	-0.7484	0.003120
0.6796	-0.7176	0.003020
0.6889	-0.6927	0.002960
0.6981	-0.6705	0.002870
0.7072	-0.6478	0.002790
0.7161	-0.6251	0.002710
0.7248	-0.6030	0.002630
0.7334	-0.5813	0.002550
0.7418	-0.5600	0.002470
0.7501	-0.5392	0.002390
0.7582	-0.5187	0.002320
0.7661	-0.4985	0.002250
0.7740	-0.4787	0.002180
0.7817	-0.4592	0.002120
0.7892	-0.4403	0.002050
0.7965	-0.4218	0.001990
0.8037	-0.4037	0.001920
0.8108	-0.3859	0.001860
0.8176	-0.3686	0.001800
0.8243	-0.3515	0.001750
0.8309	-0.3348	0.001690
0.8372	-0.3187	0.001630
0.8434	-0.3029	0.001580
0.8494	-0.2876	0.001520
0.8552	-0.2727	0.001470
0.8608	-0.2582	0.001420
0.8662	-0.2442	0.001370
0.8714	-0.2305	0.001320
0.8765	-0.2172	0.001270
0.8814	-0.2041	0.001220
0.8863	-0.1913	0.001180
0.8910	-0.1788	0.001130
0.8955	-0.1665	0.001080
0.9000	-0.1545	0.001040
0.9043	-0.1427	0.000990
0.9085	-0.1312	0.000940
0.9126	-0.1200	0.000890
0.9166	-0.1089	0.000850
0.9206	-0.0981	0.000810
0.9244	-0.0876	0.000760
0.9281	-0.0772	0.000720
0.9318	-0.0672	0.000670
0.9354	-0.0573	0.000630
0.9389	-0.0666	0.000770
0.9424	-0.0564	0.000720
0.9458	-0.0465	0.000670
0.9491	-0.0368	0.000630
0.9523	-0.0274	0.000580
0.9555	-0.0181	0.000540
0.9586	-0.0092	0.000490
0.9616	-0.0005	0.000450
0.9646	0.0080	0.000410
0.9675	0.0162	0.000370				
0.9704	0.0241	0.000330				
0.9732	0.0318	0.000290				
0.9760	0.0391	0.000250				
0.9786	0.0462	0.000220				
0.9813	0.0529	0.000180				
0.9838	0.0593	0.000150				
0.9863	0.0653	0.000130				
0.9888	0.0709	0.000100				
0.9911	0.0763	0.000090				
0.9934	0.0814	0.000100				
0.9957	0.0857	0.000140				
0.9979	0.0915	0.000430				
1.0000	0.0889	0.000430				
						
WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.8264	-0.002150
0.0001	0.8501	-0.001070
0.0003	0.8509	0.000530
0.0006	0.8339	0.001440
0.0011	0.8076	0.002130
0.0016	0.7732	0.002730
0.0022	0.7333	0.003220
0.0029	0.6900	0.003620
0.0037	0.6451	0.003920
0.0045	0.6000	0.004130
0.0054	0.5557	0.004290
0.0063	0.5128	0.004390
0.0073	0.4717	0.004450
0.0083	0.4326	0.004470
0.0094	0.3958	0.004480
0.0106	0.3613	0.004470
0.0119	0.3289	0.004450
0.0132	0.2987	0.004440
0.0146	0.2704	0.004420
0.0160	0.2440	0.004390
0.0175	0.2201	0.004330
0.0191	0.1994	0.004280
0.0208	0.1802	0.004260
0.0226	0.1612	0.004260
0.0245	0.1436	0.004240
0.0264	0.1274	0.004210
0.0284	0.1127	0.004190
0.0305	0.0993	0.004160
0.0328	0.0874	0.004120
0.0351	0.0765	0.004090
0.0375	0.0668	0.004060
0.0400	0.0578	0.004040
0.0426	0.0495	0.004010
0.0453	0.0417	0.003990
0.0482	0.0343	0.003970
0.0511	0.0270	0.003950
0.0542	0.0198	0.003940
0.0574	0.0126	0.003930
0.0607	0.0054	0.003920
0.0641	-0.0019	0.003920
0.0676	-0.0091	0.003910
0.0713	-0.0161	0.003900
0.0750	-0.0229	0.003890
0.0789	-0.0294	0.003870
0.0829	-0.0355	0.003860
0.0871	-0.0418	0.003850
0.0914	-0.0488	0.003860
0.0958	-0.0564	0.003860
0.1004	-0.0645	0.003870
0.1051	-0.0728	0.003880
0.1099	-0.0813	0.003880
0.1148	-0.0899	0.003890
0.1199	-0.0986	0.003890
0.1251	-0.1074	0.003900
0.1305	-0.1163	0.003900
0.1360	-0.1252	0.003900
0.1416	-0.1341	0.003910
0.1474	-0.1431	0.003910
0.1533	-0.1521	0.003920
0.1594	-0.1611	0.003920
0.1656	-0.1702	0.003920
0.1719	-0.1793	0.003930
0.1784	-0.1883	0.003930
0.1850	-0.1974	0.003940
0.1918	-0.2066	0.003940
0.1987	-0.2157	0.003940
0.2058	-0.2248	0.003950
0.2130	-0.2340	0.003950
0.2204	-0.2431	0.003950
0.2279	-0.2520	0.003960
0.2355	-0.2606	0.003950
0.2433	-0.2687	0.003950
0.2512	-0.2763	0.003940
0.2592	-0.2833	0.003930
0.2673	-0.2896	0.003910
0.2756	-0.2951	0.003900
0.2841	-0.2999	0.003880
0.2926	-0.3038	0.003850
0.3013	-0.3069	0.003830
0.3100	-0.3091	0.003800
0.3189	-0.3105	0.003760
0.3279	-0.3111	0.003730
0.3370	-0.3108	0.003690
0.3462	-0.3098	0.003660
0.3555	-0.3080	0.003620
0.3649	-0.3055	0.003580
0.3743	-0.3023	0.003540
0.3839	-0.2986	0.003500
0.3935	-0.2943	0.003450
0.4031	-0.2894	0.003410
0.4129	-0.2840	0.003370
0.4227	-0.2781	0.003320
0.4325	-0.2715	0.003280
0.4424	-0.2644	0.003230
0.4523	-0.2565	0.003170
0.4623	-0.2476	0.003120
0.4723	-0.2375	0.003050
0.4823	-0.2266	0.002990
0.4924	-0.2150	0.002920
0.5024	-0.2028	0.002860
0.5125	-0.1900	0.002790
0.5226	-0.1767	0.002720
0.5327	-0.1629	0.002660
0.5428	-0.1488	0.002590
0.5529	-0.1342	0.002520
0.5630	-0.1193	0.002450
0.5731	-0.1041	0.002370
0.5831	-0.0886	0.002300
0.5931	-0.0728	0.002230
0.6031	-0.0568	0.002160
0.6130	-0.0406	0.002080
0.6228	-0.0243	0.002010
0.6325	-0.0079	0.001940
0.6421	0.0085	0.001860
0.6516	0.0249	0.001790
0.6610	0.0413	0.001720
0.6702	0.0575	0.001640
0.6792	0.0736	0.001570
0.6881	0.0882	0.001500
0.6967	0.1037	0.001430
0.7051	0.1189	0.001360
0.7133	0.1337	0.001300
0.7212	0.1481	0.001230
0.7290	0.1624	0.001160
0.7365	0.1762	0.001100
0.7440	0.1896	0.001040
0.7512	0.2023	0.000990
0.7584	0.2144	0.000940
0.7654	0.2257	0.000900
0.7723	0.2361	0.000870
0.7791	0.2458	0.000840
0.7860	0.2548	0.000820
0.7927	0.2629	0.000810
0.7994	0.2703	0.000800
0.8061	0.2770	0.000800
0.8127	0.2828	0.000800
0.8193	0.2878	0.000810
0.8257	0.2918	0.000830
0.8320	0.2951	0.000850
0.8382	0.2975	0.000880
0.8443	0.2992	0.000910
0.8503	0.3001	0.000940
0.8562	0.3004	0.000980
0.8619	0.3001	0.001020
0.8676	0.2992	0.001060
0.8730	0.2979	0.001100
0.8784	0.2960	0.001140
0.8837	0.2938	0.001180
0.8888	0.2912	0.001230
0.8938	0.2884	0.001270
0.8987	0.2853	0.001310
0.9034	0.2821	0.001350
0.9081	0.2788	0.001390
0.9126	0.2753	0.001430
0.9171	0.2718	0.001460
0.9214	0.2684	0.001500
0.9256	0.2648	0.001530
0.9297	0.2612	0.001570
0.9337	0.2576	0.001600
0.9377	0.2539	0.001630
0.9415	0.2500	0.001670
0.9452	0.2461	0.001700
0.9488	0.2420	0.001740
0.9524	0.2377	0.001780
0.9558	0.2332	0.001820
0.9592	0.2286	0.001860
0.9625	0.2237	0.001900
0.9657	0.2185	0.001940
0.9688	0.2131	0.001990
0.9718	0.2074	0.002030
0.9747	0.2014	0.002080
0.9776	0.1950	0.002140
0.9804	0.1882	0.002190
0.9831	0.1810	0.002250
0.9857	0.1733	0.002320
0.9882	0.1648	0.002390				
0.9907	0.1553	0.002490				
0.9931	0.1445	0.002640				
0.9954	0.1314	0.003020				
0.9977	0.1164	0.004940				
0.9999	0.0973	0.004940				
						
WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8273	0.004590				
0.0001	0.7970	0.004430				
0.0003	0.7177	0.004300				
0.0006	0.6486	0.004550				
0.0010	0.5766	0.004960				
0.0016	0.5064	0.005340				
0.0022	0.4345	0.005660				
0.0029	0.3640	0.005880
0.0037	0.2962	0.006050
0.0045	0.2303	0.006190
0.0054	0.1655	0.006330
0.0064	0.1010	0.006470
0.0074	0.0364	0.006620
0.0085	-0.0286	0.006770
0.0096	-0.0939	0.006920
0.0108	-0.1595	0.007050
0.0120	-0.2246	0.007160
0.0133	-0.2886	0.007240
0.0147	-0.3505	0.007270
0.0161	-0.4099	0.007280
0.0176	-0.4676	0.007370
0.0193	-0.5341	0.007790
0.0209	-0.6240	0.008440
0.0225	-0.7259	0.008850
0.0242	-0.8225	0.008900
0.0258	-0.9095	0.008730
0.0276	-0.9825	0.008380
0.0295	-1.0384	0.007900
0.0316	-1.0760	0.007370
0.0338	-1.0965	0.006930
0.0361	-1.1062	0.006650
0.0385	-1.1112	0.006450
0.0411	-1.1125	0.006290
0.0438	-1.1112	0.006150
0.0465	-1.1079	0.006040
0.0495	-1.1033	0.005940
0.0525	-1.0977	0.005850
0.0557	-1.0915	0.005770
0.0589	-1.0849	0.005690
0.0623	-1.0783	0.005630
0.0658	-1.0717	0.005560
0.0695	-1.0652	0.005500
0.0732	-1.0583	0.005430
0.0771	-1.0501	0.005350
0.0812	-1.0394	0.005230
0.0854	-1.0254	0.005130
0.0897	-1.0114	0.005070
0.0941	-1.0003	0.005040
0.0987	-0.9908	0.005000
0.1034	-0.9812	0.004940
0.1082	-0.9707	0.004870
0.1131	-0.9580	0.004770
0.1182	-0.9424	0.004670
0.1235	-0.9255	0.004590
0.1289	-0.9099	0.004550
0.1344	-0.8967	0.004500
0.1401	-0.8833	0.004410
0.1459	-0.8644	0.004230
0.1519	-0.8352	0.003980
0.1580	-0.7960	0.003770
0.1643	-0.7578	0.003740
0.1707	-0.7337	0.003860
0.1772	-0.7269	0.004030
0.1840	-0.7351	0.004220
0.1908	-0.7512	0.004370
0.1978	-0.7670	0.004440
0.2050	-0.7801	0.004470
0.2123	-0.7899	0.004480
0.2197	-0.7970	0.004470
0.2273	-0.8025	0.004460
0.2351	-0.8073	0.004450
0.2430	-0.8117	0.004440
0.2510	-0.8157	0.004430
0.2591	-0.8189	0.004400
0.2674	-0.8213	0.004380
0.2759	-0.8229	0.004350
0.2844	-0.8238	0.004330
0.2931	-0.8241	0.004300
0.3020	-0.8240	0.004280
0.3109	-0.8236	0.004250
0.3200	-0.8230	0.004220
0.3291	-0.8221	0.004200
0.3384	-0.8212	0.004180
0.3478	-0.8201	0.004160
0.3573	-0.8189	0.004140
0.3669	-0.8177	0.004120
0.3766	-0.8165	0.004100
0.3863	-0.8152	0.004080
0.3962	-0.8138	0.004060
0.4061	-0.8124	0.004040
0.4161	-0.8107	0.004020
0.4261	-0.8088	0.004000
0.4363	-0.8066	0.003980
0.4464	-0.8042	0.003960
0.4566	-0.8018	0.003940
0.4669	-0.7995	0.003920
0.4771	-0.7978	0.003910
0.4874	-0.7968	0.003910
0.4978	-0.7964	0.003910
0.5081	-0.7968	0.003910
0.5184	-0.7978	0.003910
0.5287	-0.7990	0.003920
0.5391	-0.7998	0.003900
0.5494	-0.7990	0.003880
0.5597	-0.7951	0.003820
0.5699	-0.7848	0.003710
0.5801	-0.7650	0.003550
0.5903	-0.7378	0.003380
0.6004	-0.7122	0.003300
0.6105	-0.6953	0.003310
0.6205	-0.6874	0.003340
0.6304	-0.6840	0.003360
0.6402	-0.6794	0.003340
0.6499	-0.6705	0.003290
0.6596	-0.6578	0.003210
0.6691	-0.6428	0.003130
0.6785	-0.6261	0.003050
0.6878	-0.6117	0.002950
0.6969	-0.5926	0.002860
0.7059	-0.5726	0.002770
0.7148	-0.5522	0.002680
0.7235	-0.5316	0.002590
0.7321	-0.5111	0.002500
0.7404	-0.4907	0.002420
0.7487	-0.4705	0.002340
0.7568	-0.4507	0.002260
0.7647	-0.4314	0.002190
0.7726	-0.4124	0.002120
0.7803	-0.3939	0.002050
0.7878	-0.3759	0.001980
0.7951	-0.3584	0.001920
0.8023	-0.3414	0.001850
0.8094	-0.3248	0.001790
0.8162	-0.3086	0.001730
0.8230	-0.2928	0.001680
0.8295	-0.2775	0.001620
0.8359	-0.2627	0.001570
0.8421	-0.2483	0.001510
0.8481	-0.2344	0.001460
0.8540	-0.2209	0.001410
0.8596	-0.2079	0.001360
0.8651	-0.1953	0.001320
0.8704	-0.1832	0.001270
0.8755	-0.1714	0.001220
0.8805	-0.1599	0.001180
0.8854	-0.1487	0.001130
0.8902	-0.1377	0.001090
0.8948	-0.1270	0.001050
0.8993	-0.1166	0.001000
0.9037	-0.1065	0.000960
0.9080	-0.0966	0.000920
0.9122	-0.0869	0.000880
0.9162	-0.0775	0.000840
0.9202	-0.0683	0.000800
0.9241	-0.0593	0.000760
0.9279	-0.0505	0.000720
0.9316	-0.0419	0.000680
0.9352	-0.0335	0.000640
0.9388	-0.0254	0.000600
0.9422	-0.0174	0.000560
0.9457	-0.0096	0.000530
0.9490	-0.0021	0.000490
0.9523	0.0053	0.000460
0.9555	0.0124	0.000420
0.9586	0.0193	0.000390
0.9616	0.0260	0.000360
0.9646	0.0325	0.000330
0.9675	0.0387	0.000300				
0.9704	0.0448	0.000270				
0.9732	0.0506	0.000240				
0.9760	0.0562	0.000210				
0.9787	0.0615	0.000190				
0.9813	0.0666	0.000160				
0.9839	0.0715	0.000140				
0.9864	0.0761	0.000120				
0.9888	0.0804	0.000100				
0.9912	0.0844	0.000090				
0.9935	0.0883	0.000100				
0.9957	0.0918	0.000160				
0.9979	0.0965	0.000520				
1.0000	0.0949	0.000520				
						
WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.8309	-0.002550
0.0001	0.8558	-0.001370
0.0003	0.8597	0.000370
0.0006	0.8456	0.001310
0.0010	0.8216	0.002070
0.0016	0.7889	0.002730
0.0022	0.7500	0.003270
0.0029	0.7073	0.003690
0.0036	0.6626	0.004020
0.0045	0.6173	0.004250
0.0054	0.5727	0.004410
0.0063	0.5294	0.004510
0.0073	0.4879	0.004570
0.0084	0.4484	0.004600
0.0096	0.4112	0.004590
0.0108	0.3764	0.004580
0.0121	0.3439	0.004550
0.0134	0.3136	0.004520
0.0149	0.2853	0.004490
0.0164	0.2591	0.004440
0.0179	0.2354	0.004380
0.0196	0.2148	0.004320
0.0213	0.1954	0.004300
0.0231	0.1765	0.004290
0.0250	0.1591	0.004260
0.0270	0.1432	0.004230
0.0291	0.1288	0.004200
0.0313	0.1158	0.004160
0.0335	0.1042	0.004130
0.0359	0.0936	0.004100
0.0383	0.0841	0.004070
0.0409	0.0754	0.004040
0.0436	0.0672	0.004010
0.0463	0.0596	0.003990
0.0492	0.0522	0.003980
0.0522	0.0449	0.003960
0.0553	0.0378	0.003950
0.0585	0.0306	0.003950
0.0619	0.0234	0.003940
0.0653	0.0162	0.003930
0.0689	0.0091	0.003920
0.0725	0.0022	0.003910
0.0763	-0.0044	0.003900
0.0802	-0.0107	0.003880
0.0843	-0.0167	0.003870
0.0885	-0.0213	0.003870
0.0928	-0.0283	0.003880
0.0972	-0.0360	0.003890
0.1018	-0.0440	0.003900
0.1065	-0.0522	0.003900
0.1113	-0.0606	0.003910
0.1163	-0.0691	0.003910
0.1214	-0.0776	0.003920
0.1266	-0.0862	0.003920
0.1320	-0.0949	0.003930
0.1375	-0.1036	0.003930
0.1432	-0.1123	0.003930
0.1490	-0.1211	0.003940
0.1549	-0.1298	0.003940
0.1610	-0.1386	0.003950
0.1672	-0.1475	0.003950
0.1736	-0.1563	0.003950
0.1801	-0.1652	0.003960
0.1868	-0.1741	0.003960
0.1936	-0.1830	0.003960
0.2005	-0.1919	0.003970
0.2076	-0.2009	0.003970
0.2149	-0.2098	0.003980
0.2222	-0.2187	0.003980
0.2297	-0.2273	0.003980
0.2374	-0.2356	0.003970
0.2452	-0.2434	0.003970
0.2531	-0.2507	0.003960
0.2612	-0.2574	0.003950
0.2694	-0.2635	0.003930
0.2777	-0.2688	0.003910
0.2861	-0.2734	0.003890
0.2947	-0.2772	0.003870
0.3033	-0.2801	0.003840
0.3121	-0.2823	0.003810
0.3210	-0.2837	0.003780
0.3300	-0.2843	0.003740
0.3391	-0.2842	0.003710
0.3483	-0.2833	0.003670
0.3575	-0.2817	0.003630
0.3668	-0.2795	0.003590
0.3762	-0.2767	0.003550
0.3857	-0.2733	0.003510
0.3952	-0.2694	0.003470
0.4048	-0.2650	0.003430
0.4145	-0.2600	0.003390
0.4242	-0.2546	0.003340
0.4340	-0.2487	0.003300
0.4438	-0.2422	0.003250
0.4536	-0.2367	0.003200
0.4634	-0.2285	0.003140
0.4733	-0.2190	0.003080
0.4832	-0.2087	0.003010
0.4932	-0.1976	0.002950
0.5031	-0.1860	0.002880
0.5131	-0.1738	0.002820
0.5231	-0.1612	0.002750
0.5331	-0.1482	0.002680
0.5431	-0.1347	0.002610
0.5530	-0.1209	0.002540
0.5630	-0.1068	0.002470
0.5729	-0.0923	0.002400
0.5828	-0.0776	0.002330
0.5927	-0.0626	0.002260
0.6026	-0.0473	0.002190
0.6123	-0.0318	0.002120
0.6220	-0.0161	0.002040
0.6317	-0.0003	0.001970
0.6412	0.0155	0.001900
0.6506	0.0314	0.001820
0.6599	0.0473	0.001750
0.6690	0.0631	0.001670
0.6780	0.0788	0.001600
0.6868	0.0943	0.001530
0.6955	0.1095	0.001460
0.7039	0.1244	0.001390
0.7121	0.1390	0.001320
0.7201	0.1531	0.001260
0.7279	0.1666	0.001190
0.7356	0.1801	0.001130
0.7431	0.1934	0.001060
0.7504	0.2063	0.001000
0.7577	0.2185	0.000950
0.7648	0.2300	0.000910
0.7718	0.2405	0.000880
0.7788	0.2502	0.000850
0.7857	0.2590	0.000830
0.7925	0.2669	0.000820
0.7993	0.2742	0.000810
0.8061	0.2808	0.000810
0.8127	0.2866	0.000810
0.8193	0.2916	0.000820
0.8257	0.2956	0.000840
0.8321	0.2988	0.000860
0.8384	0.3012	0.000890
0.8445	0.3028	0.000920
0.8505	0.3037	0.000960
0.8564	0.3040	0.001000
0.8622	0.3036	0.001040
0.8678	0.3027	0.001080
0.8733	0.3013	0.001120
0.8787	0.2995	0.001160
0.8840	0.2973	0.001210
0.8891	0.2948	0.001250
0.8941	0.2920	0.001290
0.8990	0.2891	0.001330
0.9038	0.2859	0.001370
0.9084	0.2826	0.001410
0.9130	0.2793	0.001450
0.9174	0.2758	0.001490
0.9218	0.2724	0.001520
0.9260	0.2689	0.001560
0.9301	0.2655	0.001590
0.9341	0.2619	0.001620
0.9380	0.2583	0.001660
0.9419	0.2546	0.001690
0.9456	0.2507	0.001730
0.9492	0.2468	0.001760
0.9527	0.2427	0.001800
0.9562	0.2383	0.001840
0.9595	0.2338	0.001880
0.9628	0.2291	0.001920
0.9659	0.2242	0.001960
0.9690	0.2190	0.002010
0.9720	0.2135	0.002060
0.9750	0.2077	0.002110
0.9778	0.2016	0.002160
0.9805	0.1952	0.002210
0.9832	0.1884	0.002270
0.9858	0.1811	0.002340
0.9883	0.1732	0.002410				
0.9908	0.1644	0.002500				
0.9932	0.1545	0.002640				
0.9955	0.1430	0.002970				
0.9977	0.1319	0.004770				
0.9999	0.1118	0.004770				
						
WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8324	0.005140				
0.0001	0.8019	0.004890				
0.0003	0.7225	0.004620				
0.0006	0.6548	0.004810				
0.0010	0.5834	0.005240				
0.0015	0.5131	0.005620				
0.0021	0.4416	0.005940				
0.0028	0.3710	0.006170
0.0036	0.3027	0.006330
0.0044	0.2361	0.006470
0.0053	0.1707	0.006610
0.0062	0.1055	0.006740
0.0073	0.0402	0.006880
0.0083	-0.0255	0.007030
0.0095	-0.0917	0.007170
0.0107	-0.1582	0.007310
0.0119	-0.2244	0.007410
0.0133	-0.2894	0.007480
0.0147	-0.3523	0.007500
0.0161	-0.4128	0.007500
0.0177	-0.4716	0.007610
0.0193	-0.5407	0.008070
0.0210	-0.6331	0.008740
0.0227	-0.7366	0.009140
0.0243	-0.8347	0.009160
0.0261	-0.9222	0.008950
0.0280	-0.9945	0.008530
0.0299	-1.0484	0.007980
0.0320	-1.0832	0.007410
0.0343	-1.1015	0.006970
0.0367	-1.1102	0.006690
0.0392	-1.1144	0.006490
0.0418	-1.1149	0.006320
0.0446	-1.1126	0.006190
0.0474	-1.1084	0.006070
0.0504	-1.1028	0.005970
0.0535	-1.0963	0.005880
0.0567	-1.0891	0.005800
0.0600	-1.0817	0.005730
0.0634	-1.0741	0.005660
0.0670	-1.0666	0.005600
0.0706	-1.0590	0.005530
0.0744	-1.0505	0.005450
0.0784	-1.0401	0.005340
0.0824	-1.0265	0.005210
0.0867	-1.0095	0.005100
0.0910	-0.9933	0.005040
0.0955	-0.9794	0.004990
0.1000	-0.9643	0.004880
0.1047	-0.9443	0.004700
0.1096	-0.9145	0.004400
0.1146	-0.8760	0.004050
0.1197	-0.8319	0.003960
0.1250	-0.8019	0.004190
0.1304	-0.8015	0.004490
0.1359	-0.8145	0.004690
0.1416	-0.8279	0.004780
0.1474	-0.8390	0.004820
0.1534	-0.8477	0.004830
0.1595	-0.8543	0.004820
0.1658	-0.8591	0.004800
0.1722	-0.8624	0.004780
0.1788	-0.8641	0.004740
0.1855	-0.8645	0.004700
0.1924	-0.8636	0.004660
0.1994	-0.8616	0.004610
0.2066	-0.8585	0.004570
0.2139	-0.8548	0.004520
0.2213	-0.8506	0.004480
0.2289	-0.8463	0.004440
0.2366	-0.8424	0.004420
0.2445	-0.8389	0.004390
0.2525	-0.8361	0.004370
0.2607	-0.8334	0.004350
0.2689	-0.8305	0.004320
0.2774	-0.8271	0.004290
0.2859	-0.8227	0.004260
0.2946	-0.8173	0.004210
0.3034	-0.8109	0.004170
0.3123	-0.8038	0.004120
0.3213	-0.7967	0.004090
0.3304	-0.7900	0.004060
0.3397	-0.7840	0.004040
0.3490	-0.7791	0.004030
0.3585	-0.7750	0.004020
0.3680	-0.7715	0.004010
0.3777	-0.7687	0.004000
0.3874	-0.7661	0.003990
0.3972	-0.7635	0.003980
0.4070	-0.7609	0.003960
0.4169	-0.7578	0.003940
0.4269	-0.7547	0.003930
0.4370	-0.7516	0.003920
0.4470	-0.7492	0.003910
0.4572	-0.7473	0.003900
0.4673	-0.7458	0.003890
0.4775	-0.7438	0.003880
0.4877	-0.7409	0.003850
0.4980	-0.7370	0.003820
0.5082	-0.7326	0.003800
0.5184	-0.7289	0.003790
0.5287	-0.7267	0.003790
0.5389	-0.7258	0.003800
0.5491	-0.7254	0.003800
0.5593	-0.7238	0.003770
0.5694	-0.7198	0.003730
0.5796	-0.7129	0.003670
0.5896	-0.7042	0.003610
0.5997	-0.6949	0.003570
0.6096	-0.6861	0.003540
0.6195	-0.6786	0.003510
0.6294	-0.6708	0.003480
0.6391	-0.6616	0.003430
0.6487	-0.6509	0.003370
0.6582	-0.6385	0.003300
0.6677	-0.6244	0.003210
0.6770	-0.6083	0.003130
0.6862	-0.5908	0.003040
0.6953	-0.5725	0.002950
0.7042	-0.5537	0.002850
0.7130	-0.5343	0.002760
0.7217	-0.5146	0.002670
0.7302	-0.4950	0.002590
0.7386	-0.4755	0.002500
0.7468	-0.4561	0.002420
0.7549	-0.4371	0.002340
0.7628	-0.4184	0.002270
0.7706	-0.4001	0.002190
0.7783	-0.3822	0.002120
0.7858	-0.3648	0.002050
0.7931	-0.3479	0.001990
0.8003	-0.3314	0.001930
0.8074	-0.3153	0.001870
0.8143	-0.2997	0.001810
0.8210	-0.2844	0.001750
0.8276	-0.2695	0.001690
0.8340	-0.2551	0.001640
0.8403	-0.2411	0.001580
0.8464	-0.2275	0.001530
0.8523	-0.2143	0.001480
0.8580	-0.2016	0.001430
0.8635	-0.1892	0.001380
0.8689	-0.1772	0.001330
0.8741	-0.1656	0.001280
0.8792	-0.1542	0.001240
0.8842	-0.1432	0.001190
0.8890	-0.1323	0.001150
0.8938	-0.1217	0.001100
0.8984	-0.1114	0.001060
0.9029	-0.1013	0.001010
0.9072	-0.0915	0.000970
0.9115	-0.0819	0.000930
0.9156	-0.0725	0.000880
0.9197	-0.0633	0.000840
0.9236	-0.0543	0.000800
0.9275	-0.0455	0.000760
0.9313	-0.0370	0.000720
0.9350	-0.0286	0.000680
0.9386	-0.0205	0.000640
0.9421	-0.0125	0.000600
0.9456	-0.0048	0.000560
0.9489	0.0028	0.000530
0.9522	0.0101	0.000490
0.9555	0.0172	0.000450
0.9586	0.0241	0.000420
0.9617	0.0308	0.000390
0.9647	0.0372	0.000350
0.9676	0.0435	0.000320				
0.9705	0.0495	0.000290				
0.9733	0.0553	0.000260				
0.9761	0.0608	0.000240				
0.9788	0.0662	0.000210				
0.9814	0.0713	0.000190				
0.9840	0.0761	0.000160				
0.9864	0.0807	0.000140				
0.9889	0.0850	0.000120				
0.9912	0.0890	0.000110				
0.9935	0.0928	0.000130				
0.9957	0.0964	0.000210				
0.9979	0.1010	0.000650				
1.0000	0.1009	0.000650				
						
WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m) LOWER SURFACE						
XOC	CP	CFprime
0.0000	0.8336	-0.003250
0.0001	0.8569	-0.001850
0.0002	0.8636	0.000140
0.0005	0.8532	0.001220
0.0009	0.8319	0.002130
0.0015	0.8002	0.002930
0.0021	0.7610	0.003590
0.0028	0.7167	0.004110
0.0036	0.6697	0.004490
0.0045	0.6217	0.004760
0.0054	0.5742	0.004940
0.0064	0.5282	0.005040
0.0075	0.4842	0.005080
0.0087	0.4428	0.005070
0.0100	0.4039	0.005040
0.0113	0.3676	0.005000
0.0127	0.3337	0.004960
0.0142	0.3018	0.004910
0.0157	0.2721	0.004860
0.0173	0.2449	0.004750
0.0190	0.2223	0.004610
0.0208	0.2028	0.004540
0.0227	0.1836	0.004510
0.0246	0.1654	0.004470
0.0266	0.1488	0.004430
0.0287	0.1337	0.004380
0.0309	0.1201	0.004330
0.0332	0.1079	0.004290
0.0356	0.0970	0.004250
0.0381	0.0871	0.004210
0.0407	0.0781	0.004180
0.0433	0.0698	0.004150
0.0461	0.0620	0.004130
0.0490	0.0545	0.004110
0.0519	0.0472	0.004090
0.0550	0.0400	0.004080
0.0582	0.0329	0.004080
0.0615	0.0258	0.004070
0.0649	0.0187	0.004060
0.0684	0.0116	0.004050
0.0720	0.0047	0.004040
0.0758	-0.0018	0.004030
0.0796	-0.0081	0.004020
0.0836	-0.0141	0.004000
0.0877	-0.0202	0.004000
0.0919	-0.0270	0.004010
0.0963	-0.0344	0.004020
0.1008	-0.0422	0.004030
0.1054	-0.0503	0.004030
0.1101	-0.0585	0.004040
0.1150	-0.0669	0.004050
0.1200	-0.0753	0.004050
0.1252	-0.0838	0.004060
0.1305	-0.0924	0.004060
0.1359	-0.1011	0.004070
0.1415	-0.1129	0.004080
0.1472	-0.1216	0.004090
0.1530	-0.1303	0.004090
0.1590	-0.1390	0.004090
0.1651	-0.1478	0.004100
0.1714	-0.1566	0.004100
0.1779	-0.1655	0.004110
0.1844	-0.1743	0.004110
0.1912	-0.1832	0.004110
0.1980	-0.1921	0.004120
0.2050	-0.2010	0.004120
0.2122	-0.2100	0.004130
0.2195	-0.2188	0.004130
0.2269	-0.2276	0.004130
0.2345	-0.2360	0.004120
0.2423	-0.2440	0.004120
0.2501	-0.2515	0.004110
0.2581	-0.2584	0.004100
0.2662	-0.2648	0.004080
0.2745	-0.2704	0.004060
0.2828	-0.2753	0.004040
0.2913	-0.2795	0.004020
0.2999	-0.2828	0.003990
0.3086	-0.2854	0.003960
0.3174	-0.2872	0.003930
0.3263	-0.2882	0.003890
0.3353	-0.2884	0.003850
0.3443	-0.2879	0.003810
0.3534	-0.2867	0.003780
0.3626	-0.2849	0.003730
0.3718	-0.2824	0.003690
0.3811	-0.2793	0.003650
0.3904	-0.2757	0.003610
0.3998	-0.2716	0.003560
0.4092	-0.2670	0.003520
0.4186	-0.2619	0.003470
0.4281	-0.2564	0.003430
0.4376	-0.2503	0.003380
0.4472	-0.2437	0.003330
0.4568	-0.2365	0.003280
0.4663	-0.2282	0.003210
0.4760	-0.2187	0.003150
0.4856	-0.2085	0.003080
0.4953	-0.1977	0.003010
0.5049	-0.1863	0.002950
0.5146	-0.1744	0.002880
0.5243	-0.1621	0.002810
0.5340	-0.1494	0.002740
0.5437	-0.1364	0.002670
0.5533	-0.1230	0.002600
0.5630	-0.1092	0.002530
0.5726	-0.0952	0.002460
0.5823	-0.0809	0.002380
0.5918	-0.0663	0.002310
0.6014	-0.0515	0.002230
0.6109	-0.0365	0.002160
0.6203	-0.0213	0.002080
0.6297	-0.0060	0.002010
0.6390	0.0094	0.001930
0.6482	0.0249	0.001850
0.6573	0.0404	0.001780
0.6663	0.0558	0.001700
0.6752	0.0711	0.001630
0.6839	0.0874	0.001550
0.6925	0.1025	0.001480
0.7010	0.1173	0.001410
0.7093	0.1318	0.001340
0.7174	0.1460	0.001270
0.7254	0.1597	0.001200
0.7333	0.1733	0.001130
0.7410	0.1868	0.001060
0.7486	0.1998	0.001000
0.7561	0.2123	0.000940
0.7635	0.2241	0.000900
0.7708	0.2349	0.000860
0.7780	0.2448	0.000830
0.7851	0.2538	0.000810
0.7922	0.2619	0.000800
0.7991	0.2693	0.000790
0.8060	0.2760	0.000790
0.8128	0.2818	0.000790
0.8194	0.2868	0.000810
0.8260	0.2909	0.000830
0.8324	0.2943	0.000850
0.8387	0.2968	0.000880
0.8449	0.2986	0.000910
0.8510	0.2997	0.000950
0.8569	0.3002	0.000990
0.8627	0.3001	0.001030
0.8684	0.2995	0.001070
0.8740	0.2984	0.001120
0.8794	0.2969	0.001160
0.8847	0.2950	0.001210
0.8899	0.2928	0.001250
0.8949	0.2904	0.001290
0.8999	0.2878	0.001340
0.9047	0.2849	0.001380
0.9093	0.2820	0.001420
0.9139	0.2791	0.001450
0.9184	0.2761	0.001490
0.9227	0.2730	0.001520
0.9269	0.2700	0.001560
0.9310	0.2669	0.001590
0.9351	0.2637	0.001630
0.9390	0.2605	0.001660
0.9428	0.2573	0.001690
0.9465	0.2539	0.001730
0.9501	0.2504	0.001760
0.9536	0.2467	0.001800
0.9570	0.2430	0.001840
0.9603	0.2390	0.001880
0.9635	0.2349	0.001920
0.9666	0.2306	0.001960
0.9697	0.2260	0.002000
0.9726	0.2213	0.002050
0.9755	0.2163	0.002090
0.9783	0.2111	0.002140
0.9810	0.2057	0.002190
0.9836	0.1999	0.002250
0.9862	0.1938	0.002310
0.9886	0.1873	0.002370				
0.9910	0.1802	0.002450				
0.9933	0.1725	0.002560				
0.9956	0.1643	0.002830				
0.9978	0.1578	0.004390				
0.9999	0.1353	0.004390				
						
WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m) UPPER SURFACE						
XOC	CP	CFprime				
0.0000	0.8355	0.006010				
0.0001	0.8071	0.005590				
0.0002	0.7351	0.005070				
0.0005	0.6749	0.005200				
0.0009	0.6089	0.005710				
0.0013	0.5403	0.006160				
0.0019	0.4705	0.006510				
0.0026	0.4007	0.006770
0.0033	0.3319	0.006960
0.0041	0.2642	0.007110
0.0050	0.1973	0.007240
0.0059	0.1306	0.007370
0.0069	0.0639	0.007500
0.0080	-0.0034	0.007630
0.0092	-0.0712	0.007770
0.0104	-0.1397	0.007890
0.0117	-0.2083	0.008000
0.0131	-0.2766	0.008080
0.0146	-0.3439	0.008120
0.0161	-0.4097	0.008140
0.0177	-0.4743	0.008270
0.0195	-0.5487	0.008750
0.0212	-0.6438	0.009400
0.0230	-0.7492	0.009770
0.0249	-0.8502	0.009750
0.0268	-0.9396	0.009440
0.0289	-1.0120	0.008900
0.0311	-1.0630	0.008180
0.0334	-1.0919	0.007460
0.0358	-1.1026	0.006940
0.0384	-1.1039	0.006640
0.0410	-1.1023	0.006460
0.0438	-1.0986	0.006320
0.0467	-1.0938	0.006220
0.0496	-1.0882	0.006130
0.0527	-1.0823	0.006050
0.0559	-1.0758	0.005980
0.0592	-1.0685	0.005890
0.0626	-1.0599	0.005800
0.0662	-1.0498	0.005700
0.0698	-1.0384	0.005600
0.0736	-1.0257	0.005510
0.0775	-1.0125	0.005430
0.0815	-0.9991	0.005360
0.0856	-0.9854	0.005260
0.0899	-0.9676	0.005080
0.0942	-0.9408	0.004790
0.0988	-0.9043	0.004420
0.1034	-0.8614	0.004010
0.1082	-0.8120	0.004000
0.1131	-0.7810	0.004400
0.1181	-0.7864	0.004810
0.1233	-0.8033	0.005030
0.1286	-0.8164	0.005070
0.1340	-0.8251	0.005070
0.1396	-0.8300	0.005040
0.1453	-0.8317	0.004990
0.1512	-0.8302	0.004920
0.1572	-0.8164	0.004760
0.1633	-0.8035	0.004610
0.1696	-0.7873	0.004490
0.1760	-0.7732	0.004490
0.1826	-0.7671	0.004570
0.1893	-0.7696	0.004660
0.1962	-0.7754	0.004710
0.2032	-0.7796	0.004690
0.2104	-0.7800	0.004640
0.2177	-0.7761	0.004560
0.2251	-0.7690	0.004490
0.2327	-0.7603	0.004420
0.2404	-0.7518	0.004370
0.2482	-0.7447	0.004340
0.2562	-0.7390	0.004330
0.2643	-0.7345	0.004310
0.2726	-0.7302	0.004290
0.2809	-0.7257	0.004270
0.2894	-0.7218	0.004260
0.2980	-0.7192	0.004260
0.3068	-0.7179	0.004260
0.3156	-0.7171	0.004250
0.3245	-0.7159	0.004240
0.3336	-0.7137	0.004220
0.3427	-0.7111	0.004200
0.3520	-0.7082	0.004170
0.3613	-0.7053	0.004140
0.3708	-0.7018	0.004120
0.3803	-0.6978	0.004100
0.3898	-0.6938	0.004080
0.3995	-0.6905	0.004060
0.4092	-0.6881	0.004050
0.4189	-0.6862	0.004030
0.4288	-0.6839	0.004020
0.4386	-0.6810	0.004000
0.4485	-0.6776	0.003980
0.4585	-0.6743	0.003970
0.4684	-0.6715	0.003960
0.4784	-0.6696	0.003950
0.4884	-0.6681	0.003940
0.4984	-0.6668	0.003930
0.5085	-0.6651	0.003920
0.5185	-0.6630	0.003910
0.5285	-0.6606	0.003890
0.5385	-0.6578	0.003880
0.5484	-0.6547	0.003860
0.5584	-0.6515	0.003840
0.5683	-0.6481	0.003810
0.5782	-0.6440	0.003780
0.5880	-0.6392	0.003750
0.5978	-0.6334	0.003710
0.6075	-0.6272	0.003680
0.6172	-0.6213	0.003660
0.6267	-0.6153	0.003620
0.6362	-0.6082	0.003580
0.6456	-0.5997	0.003520
0.6550	-0.5898	0.003460
0.6642	-0.5783	0.003380
0.6733	-0.5653	0.003310
0.6824	-0.5511	0.003220
0.6913	-0.5358	0.003140
0.7001	-0.5197	0.003050
0.7087	-0.5029	0.002960
0.7173	-0.4857	0.002870
0.7257	-0.4682	0.002790
0.7339	-0.4506	0.002700
0.7421	-0.4330	0.002620
0.7501	-0.4175	0.002520
0.7580	-0.3999	0.002440
0.7658	-0.3827	0.002370
0.7734	-0.3657	0.002290
0.7809	-0.3492	0.002220
0.7883	-0.3330	0.002160
0.7955	-0.3173	0.002090
0.8026	-0.3021	0.002030
0.8095	-0.2874	0.001980
0.8163	-0.2732	0.001920
0.8229	-0.2594	0.001870
0.8294	-0.2458	0.001810
0.8358	-0.2321	0.001750
0.8420	-0.2187	0.001690
0.8480	-0.2056	0.001630
0.8539	-0.1928	0.001580
0.8597	-0.1804	0.001520
0.8652	-0.1684	0.001470
0.8707	-0.1567	0.001420
0.8760	-0.1453	0.001370
0.8812	-0.1342	0.001330
0.8863	-0.1233	0.001280
0.8912	-0.1127	0.001230
0.8960	-0.1024	0.001190
0.9007	-0.0923	0.001140
0.9053	-0.0825	0.001090
0.9098	-0.0728	0.001050
0.9141	-0.0634	0.001000
0.9184	-0.0542	0.000960
0.9225	-0.0452	0.000920
0.9265	-0.0364	0.000870
0.9305	-0.0277	0.000830
0.9343	-0.0193	0.000790
0.9381	-0.0110	0.000740
0.9417	-0.0030	0.000700
0.9453	0.0049	0.000660
0.9488	0.0126	0.000620
0.9522	0.0200	0.000580
0.9555	0.0273	0.000540
0.9587	0.0343	0.000500
0.9618	0.0411	0.000460
0.9649	0.0477	0.000430
0.9678	0.0540	0.000390
0.9708	0.0602	0.000360
0.9736	0.0661	0.000330
0.9763	0.0718	0.000300
0.9790	0.0772	0.000270
0.9816	0.0824	0.000240
0.9842	0.0874	0.000210
0.9866	0.0921	0.000190
0.9890	0.0964	0.000170
0.9914	0.1005	0.000160
0.9936	0.1044	0.000190
0.9958	0.1082	0.000310
0.9979	0.1120	0.000930
1.0000	0.1135	0.000930


NOTES:	
------	
* Information lines are 80 characters long.	
* Information blocks allow free-form miscellaneous information.	

* MACH     (F10.2) Mach Number.	
* ALPHA    (F10.3) Angle of Attack in Degrees.	

* GRID_SIZE (F10.0) Number of grid nodes or cells	

"Include as many X/C, CP pairs as necessary for each location"	
* X/C              (F12.4) X location on wing non-dimensionalized by local chord	
* CP               (F12.4) Coefficient of pressure	
* CF               (F12.6) Skin-friction Coefficient at wall = tauw/(freestream dynamic pressure)	
"* CFX, CFY, CFZ    (F12.6) Components of skin-friction Coefficient at wall"	
* Cfprime 	(F12.6) Skin-friction Coefficient perpendicular to the cell trailing edge (downstream)

* BO2              Semispan   (585.647 mm)
