DPW-III DPW-Wing Alone CASE-2 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
    Basic Algorithm:  		Finite Volume
   Turbulence Model:  		Spalart-Allmaras
      Miscellaneous:  		


GRID INFORMATION		
--------------------		
Grid-Generator Name:  		ICEM
          Grid Type:  		"Structured Block, Point-to-Point Matched"



FINE GRID SIZE 		W1	W2
----------------------------------------			
              Zones:  		11	17
        Field Nodes:		14750771	14811489
        Field Cells:  		14346240	14346240
     Boundary Nodes:  		48339	48339
     Boundary Faces:  		46848	46848
   BL 1st-Cell Size:  		y+~0.55	0.55
 BL Max-Growth Rate:  		<1.2	<1.2
           BL Cells:  		72	72
      Miscellaneous:  			



CASE 2.A:  SINGLE-POINT GRID CONVERGENCE STUDY - FINE GRID CP AND CF DISTRIBUTIONS			
----------------------------------------------------------------------------------			

DPW-W1			

GRID_SIZE	MACH	ALPHA	CL_TOT
14811489	0.76000	0.500000	0.46358

WING SECTION 1   Y/BO2 0.026 (Y =  20. mm) UPPER SURFACE			
XOC	CP	CFprime	
0.00000	1.06690	-0.000420	
0.00001	1.06836	0.000110	
0.00006	1.06547	0.000400	
0.00014	1.05904	0.000700	
0.00026	1.04882	0.001010	
0.00041	1.03476	0.001310
0.00061	1.01671	0.001620
0.00084	0.99491	0.001910
0.00111	0.96956	0.002200
0.00142	0.94066	0.002470
0.00177	0.90894	0.002730
0.00216	0.87473	0.002970
0.00259	0.83817	0.003180
0.00305	0.80036	0.003370
0.00355	0.76199	0.003530
0.00408	0.72343	0.003680
0.00464	0.68545	0.003790
0.00523	0.64867	0.003860
0.00584	0.61379	0.003910
0.00647	0.58125	0.003950
0.00711	0.55103	0.003970
0.00777	0.52308	0.003980
0.00843	0.49726	0.003990
0.00910	0.47366	0.003990
0.00977	0.45168	0.003990
0.00977	0.45168	0.004000
0.01045	0.43083	0.004010
0.01119	0.40994	0.004040
0.01199	0.38833	0.004070
0.01285	0.36644	0.004100
0.01379	0.34372	0.004150
0.01480	0.32009	0.004200
0.01589	0.29598	0.004240
0.01706	0.27200	0.004270
0.01832	0.24836	0.004300
0.01967	0.22556	0.004300
0.02113	0.20478	0.004280
0.02268	0.18603	0.004260
0.02434	0.16894	0.004240
0.02611	0.15383	0.004210
0.02799	0.14035	0.004180
0.02999	0.12737	0.004170
0.03210	0.11428	0.004160
0.03433	0.10231	0.004140
0.03669	0.09122	0.004120
0.03916	0.08101	0.004090
0.04176	0.07176	0.004070
0.04448	0.06275	0.004040
0.04732	0.05427	0.004020
0.05027	0.04608	0.004000
0.05334	0.03807	0.003980
0.05652	0.03084	0.003950
0.05981	0.02455	0.003920
0.06320	0.01906	0.003890
0.06668	0.01389	0.003860
0.07024	0.00815	0.003850
0.07389	0.00215	0.003830
0.07760	-0.00389	0.003820
0.08137	-0.01004	0.003810
0.08518	-0.01611	0.003800
0.08904	-0.02207	0.003780
0.09292	-0.02796	0.003770
0.09681	-0.03381	0.003760
0.10071	-0.03963	0.003760
0.10459	-0.04530	0.003750
0.10846	-0.05123	0.003740
0.11233	-0.05716	0.003740
0.11644	-0.06312	0.003740
0.12081	-0.06978	0.003740
0.12545	-0.07684	0.003730
0.13038	-0.08420	0.003730
0.13560	-0.09187	0.003730
0.14114	-0.09995	0.003730
0.14700	-0.10836	0.003730
0.15320	-0.11703	0.003730
0.15976	-0.12595	0.003720
0.16668	-0.13494	0.003720
0.17398	-0.14394	0.003710
0.18167	-0.15301	0.003700
0.18977	-0.16246	0.003700
0.19828	-0.17277	0.003700
0.20722	-0.18447	0.003710
0.21659	-0.19831	0.003740
0.22640	-0.21391	0.003760
0.23665	-0.23047	0.003780
0.24736	-0.24749	0.003800
0.25852	-0.26418	0.003810
0.27013	-0.28012	0.003810
0.28220	-0.29475	0.003800
0.29471	-0.30744	0.003780
0.30766	-0.31928	0.003770
0.32103	-0.33272	0.003770
0.33481	-0.34678	0.003770
0.34900	-0.35883	0.003750
0.36356	-0.36759	0.003720
0.37847	-0.37266	0.003670
0.39371	-0.37491	0.003620
0.40925	-0.37529	0.003560
0.42506	-0.37478	0.003520
0.44111	-0.37355	0.003470
0.45735	-0.37108	0.003430
0.47376	-0.36760	0.003380
0.49028	-0.36348	0.003340
0.50689	-0.35657	0.003270
0.52353	-0.34208	0.003160
0.54017	-0.31802	0.003010
0.55676	-0.28668	0.002840
0.57326	-0.25139	0.002670
0.58963	-0.21490	0.002520
0.60584	-0.17804	0.002360
0.62184	-0.14084	0.002210
0.63762	-0.10363	0.002070
0.65312	-0.06672	0.001930
0.66833	-0.03014	0.001790
0.68322	0.00623	0.001650
0.69776	0.04216	0.001510
0.71193	0.07782	0.001370
0.72572	0.11265	0.001240
0.73911	0.14504	0.001130
0.75210	0.17398	0.001040
0.76468	0.19889	0.000980
0.77684	0.21955	0.000950
0.78856	0.23644	0.000940
0.79986	0.25025	0.000940
0.81072	0.26168	0.000940
0.82114	0.27121	0.000950
0.83113	0.27916	0.000970
0.84068	0.28574	0.000980
0.84981	0.29114	0.001000
0.85851	0.29552	0.001030
0.86680	0.29900	0.001050
0.87469	0.30166	0.001070
0.88218	0.30359	0.001100
0.88930	0.30489	0.001120
0.89604	0.30562	0.001150
0.90243	0.30587	0.001180
0.90847	0.30570	0.001210
0.91418	0.30517	0.001230
0.91958	0.30429	0.001260
0.92467	0.30316	0.001290
0.92948	0.30176	0.001310
0.93400	0.30015	0.001340
0.93826	0.29838	0.001370
0.94227	0.29640	0.001390
0.94604	0.29434	0.001420
0.94959	0.29209	0.001440
0.95314	0.28959	0.001470
0.95667	0.28692	0.001500
0.96016	0.28396	0.001530
0.96356	0.28078	0.001560
0.96687	0.27741	0.001590
0.97005	0.27383	0.001620
0.97308	0.27009	0.001650
0.97595	0.26621	0.001680
0.97864	0.26225	0.001720
0.98115	0.25817	0.001750
0.98348	0.25404	0.001790
0.98563	0.24991	0.001820
0.98759	0.24576	0.001860
0.98939	0.24161	0.001890
0.99101	0.23748	0.001930
0.99248	0.23335	0.001960
0.99380	0.22931	0.002000
0.99499	0.22519	0.002040
0.99605	0.22114	0.002080
0.99699	0.21700	0.002110
0.99784	0.21314	0.002170
0.99858	0.20905	0.002330
0.99925	0.20590	0.002970

WING SECTION 1   Y/BO2 0.026 (Y =  20. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.06897	0.000620
0.00001	1.06486	0.000430
0.00004	1.05913	0.000690
0.00010	1.05043	0.000940
0.00018	1.03897	0.001190
0.00029	1.02480	0.001430
0.00042	1.00803	0.001660
0.00058	0.98845	0.001890
0.00077	0.96661	0.002110
0.00099	0.94232	0.002320
0.00123	0.91589	0.002530
0.00151	0.88758	0.002720
0.00182	0.85726	0.002900
0.00215	0.82567	0.003070
0.00252	0.79278	0.003230
0.00291	0.75871	0.003370
0.00333	0.72422	0.003500
0.00378	0.68949	0.003620
0.00426	0.65453	0.003730
0.00476	0.61970	0.003830
0.00529	0.58518	0.003920
0.00585	0.55109	0.004010
0.00642	0.51744	0.004100
0.00702	0.48431	0.004190
0.00763	0.45101	0.004320
0.00826	0.41821	0.004360
0.00895	0.38406	0.004460
0.00970	0.34705	0.004590
0.01051	0.30746	0.004720
0.01140	0.26461	0.004870
0.01236	0.21894	0.005020
0.01341	0.16983	0.005190
0.01454	0.11608	0.005360
0.01576	0.05925	0.005540
0.01709	-0.00172	0.005730
0.01852	-0.06646	0.005890
0.02007	-0.13262	0.006040
0.02173	-0.20075	0.006170
0.02353	-0.26765	0.006250
0.02545	-0.33136	0.006290
0.02751	-0.39103	0.006300
0.02971	-0.44499	0.006270
0.03204	-0.49194	0.006200
0.03452	-0.53185	0.006120
0.03713	-0.56594	0.006040
0.03987	-0.59634	0.005970
0.04275	-0.62347	0.005890
0.04575	-0.64780	0.005840
0.04888	-0.67138	0.005800
0.05212	-0.69432	0.005740
0.05548	-0.71320	0.005660
0.05895	-0.72911	0.005600
0.06251	-0.74445	0.005540
0.06616	-0.75706	0.005460
0.06989	-0.76682	0.005380
0.07369	-0.77402	0.005300
0.07755	-0.77785	0.005190
0.08146	-0.77791	0.005090
0.08541	-0.77576	0.005000
0.08937	-0.77285	0.004900
0.09335	-0.76638	0.004790
0.09733	-0.75712	0.004680
0.10130	-0.74812	0.004600
0.10524	-0.73965	0.004540
0.10914	-0.73379	0.004510
0.11305	-0.73026	0.004490
0.11721	-0.72777	0.004480
0.12163	-0.72515	0.004440
0.12632	-0.72088	0.004400
0.13131	-0.71757	0.004380
0.13659	-0.71555	0.004350
0.14219	-0.71365	0.004330
0.14812	-0.71343	0.004330
0.15439	-0.71511	0.004320
0.16102	-0.71697	0.004300
0.16801	-0.71913	0.004280
0.17540	-0.72143	0.004270
0.18317	-0.72406	0.004250
0.19136	-0.72838	0.004240
0.19996	-0.73261	0.004230
0.20899	-0.73668	0.004210
0.21846	-0.74074	0.004180
0.22837	-0.74381	0.004160
0.23872	-0.74763	0.004140
0.24953	-0.75119	0.004110
0.26079	-0.75325	0.004080
0.27251	-0.75601	0.004060
0.28468	-0.75967	0.004040
0.29728	-0.76407	0.004020
0.31033	-0.76799	0.004000
0.32380	-0.77081	0.003970
0.33769	-0.77376	0.003950
0.35197	-0.77728	0.003930
0.36662	-0.78137	0.003920
0.38163	-0.78560	0.003900
0.39696	-0.78978	0.003890
0.41260	-0.79409	0.003870
0.42849	-0.79847	0.003860
0.44463	-0.80276	0.003840
0.46096	-0.80681	0.003830
0.47746	-0.81060	0.003810
0.49407	-0.81457	0.003800
0.51077	-0.81833	0.003790
0.52751	-0.82119	0.003770
0.54425	-0.82310	0.003740
0.56094	-0.82125	0.003670
0.57756	-0.80616	0.003490
0.59404	-0.76061	0.003120
0.61036	-0.68684	0.002760
0.62648	-0.62188	0.002650
0.64236	-0.58681	0.002700
0.65797	-0.57177	0.002760
0.67327	-0.56155	0.002750
0.68823	-0.54311	0.002680
0.70284	-0.51565	0.002570
0.71706	-0.48533	0.002460
0.73087	-0.45515	0.002360
0.74427	-0.42469	0.002250
0.75724	-0.39437	0.002150
0.76977	-0.36446	0.002040
0.78186	-0.33510	0.001940
0.79349	-0.30697	0.001850
0.80467	-0.27997	0.001760
0.81540	-0.25389	0.001680
0.82567	-0.22903	0.001600
0.83550	-0.20540	0.001520
0.84490	-0.18279	0.001450
0.85386	-0.16156	0.001380
0.86239	-0.14126	0.001310
0.87052	-0.12197	0.001250
0.87824	-0.10370	0.001190
0.88557	-0.08636	0.001130
0.89252	-0.06995	0.001080
0.89910	-0.05437	0.001030
0.90534	-0.03979	0.000980
0.91123	-0.02571	0.000930
0.91680	-0.01247	0.000880
0.92206	-0.00002	0.000830
0.92702	0.01199	0.000790
0.93169	0.02305	0.000750
0.93609	0.03356	0.000710
0.94024	0.04355	0.000670
0.94414	0.05291	0.000640
0.94780	0.06171	0.000610
0.95125	0.07008	0.000570
0.95469	0.07823	0.000540
0.95812	0.08634	0.000510
0.96151	0.09446	0.000480
0.96482	0.10235	0.000450
0.96802	0.10998	0.000420
0.97111	0.11728	0.000390
0.97405	0.12417	0.000360
0.97683	0.13064	0.000340
0.97944	0.13680	0.000310
0.98188	0.14241	0.000290
0.98414	0.14752	0.000270
0.98622	0.15229	0.000250
0.98813	0.15653	0.000240
0.98986	0.16034	0.000220
0.99144	0.16388	0.000210
0.99287	0.16688	0.000200
0.99415	0.16957	0.000190
0.99530	0.17211	0.000180
0.99633	0.17419	0.000180
0.99725	0.17597	0.000170
0.99806	0.17767	0.000180
0.99879	0.17880	0.000200
0.99943	0.18046	0.000320
1.00000	0.18183	0.000320

WING SECTION 2   Y/BO2 0.157 (Y = 120. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.02858	-0.000420
0.00001	1.03266	-0.000070
0.00006	1.03190	0.000220
0.00013	1.02777	0.000540
0.00024	1.01996	0.000860
0.00038	1.00833	0.001180
0.00056	0.99293	0.001500
0.00078	0.97358	0.001810
0.00103	0.95069	0.002120
0.00132	0.92425	0.002410
0.00165	0.89460	0.002680
0.00201	0.86229	0.002950
0.00241	0.82733	0.003190
0.00284	0.79074	0.003400
0.00331	0.75296	0.003600
0.00381	0.71437	0.003760
0.00434	0.67602	0.003890
0.00490	0.63856	0.004000
0.00548	0.60224	0.004080
0.00608	0.56761	0.004130
0.00670	0.53515	0.004150
0.00734	0.50496	0.004180
0.00798	0.47681	0.004190
0.00864	0.45085	0.004200
0.00931	0.42634	0.004200
0.00931	0.42634	0.004200
0.00997	0.40354	0.004210
0.01069	0.38109	0.004230
0.01147	0.35767	0.004260
0.01232	0.33405	0.004290
0.01323	0.30948	0.004350
0.01422	0.28379	0.004400
0.01528	0.25748	0.004440
0.01643	0.23107	0.004480
0.01766	0.20488	0.004510
0.01898	0.17914	0.004520
0.02040	0.15501	0.004520
0.02192	0.13285	0.004500
0.02355	0.11275	0.004470
0.02528	0.09506	0.004440
0.02712	0.07891	0.004420
0.02907	0.06413	0.004400
0.03114	0.04956	0.004390
0.03333	0.03533	0.004370
0.03563	0.02254	0.004350
0.03805	0.01076	0.004330
0.04060	-0.00029	0.004310
0.04326	-0.01055	0.004280
0.04606	-0.02009	0.004260
0.04896	-0.02923	0.004230
0.05199	-0.03791	0.004210
0.05512	-0.04618	0.004190
0.05835	-0.05348	0.004160
0.06169	-0.05956	0.004120
0.06512	-0.06480	0.004090
0.06863	-0.07033	0.004070
0.07222	-0.07638	0.004060
0.07588	-0.08241	0.004040
0.07961	-0.08855	0.004030
0.08339	-0.09460	0.004010
0.08721	-0.10046	0.004000
0.09105	-0.10619	0.003990
0.09492	-0.11187	0.003980
0.09878	-0.11751	0.003970
0.10265	-0.12295	0.003960
0.10649	-0.12862	0.003950
0.11034	-0.13426	0.003940
0.11444	-0.13990	0.003940
0.11879	-0.14617	0.003930
0.12341	-0.15289	0.003930
0.12832	-0.15986	0.003920
0.13352	-0.16711	0.003920
0.13903	-0.17481	0.003920
0.14487	-0.18272	0.003910
0.15105	-0.19081	0.003910
0.15758	-0.19917	0.003900
0.16448	-0.20749	0.003890
0.17176	-0.21572	0.003880
0.17942	-0.22398	0.003870
0.18750	-0.23223	0.003860
0.19598	-0.24095	0.003860
0.20491	-0.25135	0.003860
0.21428	-0.26356	0.003880
0.22409	-0.27736	0.003900
0.23434	-0.29274	0.003920
0.24505	-0.30825	0.003930
0.25621	-0.32312	0.003930
0.26782	-0.33697	0.003930
0.27989	-0.34898	0.003910
0.29241	-0.35856	0.003880
0.30536	-0.36652	0.003850
0.31874	-0.37505	0.003840
0.33253	-0.38412	0.003820
0.34673	-0.39127	0.003790
0.36130	-0.39447	0.003740
0.37624	-0.39331	0.003670
0.39150	-0.38887	0.003600
0.40707	-0.38225	0.003530
0.42291	-0.37470	0.003460
0.43898	-0.36656	0.003400
0.45526	-0.35717	0.003340
0.47170	-0.34680	0.003280
0.48827	-0.33593	0.003220
0.50492	-0.32300	0.003140
0.52160	-0.30396	0.003030
0.53829	-0.27700	0.002880
0.55493	-0.24388	0.002710
0.57148	-0.20750	0.002540
0.58791	-0.17035	0.002380
0.60417	-0.13355	0.002230
0.62022	-0.09712	0.002090
0.63604	-0.06095	0.001950
0.65160	-0.02541	0.001810
0.66687	0.00940	0.001680
0.68181	0.04366	0.001550
0.69641	0.07726	0.001420
0.71065	0.11027	0.001290
0.72450	0.14227	0.001170
0.73795	0.17196	0.001060
0.75100	0.19842	0.000980
0.76364	0.22114	0.000930
0.77586	0.23989	0.000900
0.78765	0.25507	0.000890
0.79901	0.26735	0.000890
0.80993	0.27734	0.000900
0.82042	0.28557	0.000910
0.83046	0.29232	0.000930
0.84007	0.29780	0.000940
0.84926	0.30222	0.000970
0.85802	0.30569	0.000990
0.86637	0.30831	0.001010
0.87431	0.31023	0.001040
0.88186	0.31150	0.001070
0.88903	0.31217	0.001090
0.89582	0.31236	0.001120
0.90225	0.31213	0.001150
0.90834	0.31152	0.001170
0.91410	0.31060	0.001200
0.91954	0.30940	0.001230
0.92467	0.30796	0.001260
0.92951	0.30631	0.001280
0.93407	0.30448	0.001310
0.93837	0.30252	0.001340
0.94241	0.30038	0.001360
0.94622	0.29823	0.001390
0.94979	0.29584	0.001410
0.95337	0.29322	0.001440
0.95692	0.29052	0.001470
0.96043	0.28751	0.001500
0.96386	0.28432	0.001530
0.96717	0.28096	0.001560
0.97036	0.27743	0.001590
0.97339	0.27375	0.001620
0.97625	0.26998	0.001650
0.97893	0.26614	0.001680
0.98143	0.26222	0.001720
0.98375	0.25829	0.001750
0.98587	0.25436	0.001780
0.98782	0.25044	0.001820
0.98959	0.24653	0.001850
0.99119	0.24264	0.001890
0.99264	0.23881	0.001920
0.99394	0.23504	0.001960
0.99511	0.23119	0.001990
0.99615	0.22744	0.002030
0.99708	0.22360	0.002070
0.99790	0.22005	0.002130
0.99863	0.21629	0.002290
0.99928	0.21342	0.002940

WING SECTION 2   Y/BO2 0.157 (Y = 120. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.03227	0.000630
0.00001	1.02580	0.000610
0.00004	1.01859	0.000870
0.00009	1.00850	0.001130
0.00017	0.99579	0.001390
0.00027	0.98039	0.001640
0.00039	0.96231	0.001880
0.00054	0.94180	0.002110
0.00071	0.91880	0.002340
0.00092	0.89346	0.002560
0.00115	0.86603	0.002770
0.00140	0.83654	0.002970
0.00169	0.80520	0.003160
0.00200	0.77240	0.003340
0.00235	0.73816	0.003510
0.00272	0.70284	0.003670
0.00312	0.66695	0.003810
0.00354	0.63041	0.003940
0.00400	0.59363	0.004060
0.00448	0.55698	0.004160
0.00499	0.52058	0.004260
0.00552	0.48450	0.004350
0.00607	0.44880	0.004440
0.00665	0.41365	0.004530
0.00725	0.37824	0.004660
0.00786	0.34388	0.004700
0.00853	0.30787	0.004810
0.00925	0.26889	0.004930
0.01005	0.22780	0.005070
0.01091	0.18301	0.005210
0.01184	0.13530	0.005370
0.01286	0.08395	0.005530
0.01396	0.02813	0.005720
0.01515	-0.03187	0.005910
0.01644	-0.09622	0.006090
0.01783	-0.16465	0.006280
0.01933	-0.23641	0.006440
0.02095	-0.31076	0.006590
0.02270	-0.38567	0.006690
0.02457	-0.45925	0.006760
0.02657	-0.52917	0.006770
0.02871	-0.59352	0.006750
0.03099	-0.65143	0.006690
0.03340	-0.70269	0.006600
0.03595	-0.74747	0.006520
0.03862	-0.78683	0.006430
0.04143	-0.82160	0.006350
0.04436	-0.85295	0.006280
0.04741	-0.88230	0.006220
0.05058	-0.91056	0.006170
0.05387	-0.93766	0.006120
0.05726	-0.96243	0.006060
0.06075	-0.98499	0.006000
0.06433	-1.00568	0.005940
0.06799	-1.02422	0.005870
0.07172	-1.04075	0.005810
0.07551	-1.05512	0.005740
0.07936	-1.06672	0.005660
0.08324	-1.07541	0.005590
0.08715	-1.08206	0.005520
0.09108	-1.08734	0.005450
0.09501	-1.09014	0.005370
0.09894	-1.09056	0.005300
0.10284	-1.08943	0.005230
0.10672	-1.08743	0.005160
0.11060	-1.08531	0.005110
0.11474	-1.08293	0.005060
0.11913	-1.07991	0.005010
0.12380	-1.07560	0.004950
0.12876	-1.06992	0.004890
0.13402	-1.06302	0.004820
0.13959	-1.05483	0.004760
0.14549	-1.04480	0.004700
0.15174	-1.03155	0.004620
0.15834	-1.01305	0.004530
0.16531	-0.98712	0.004400
0.17268	-0.95440	0.004200
0.18044	-0.91912	0.003990
0.18861	-0.88801	0.003830
0.19720	-0.86606	0.003790
0.20621	-0.85397	0.003820
0.21566	-0.84991	0.003890
0.22556	-0.85098	0.003970
0.23590	-0.85458	0.004040
0.24670	-0.85798	0.004070
0.25796	-0.85952	0.004080
0.26967	-0.85946	0.004080
0.28183	-0.85876	0.004060
0.29443	-0.85772	0.004030
0.30748	-0.85616	0.004000
0.32096	-0.85359	0.003970
0.33486	-0.85106	0.003950
0.34915	-0.84962	0.003930
0.36382	-0.84874	0.003910
0.37885	-0.84807	0.003890
0.39420	-0.84743	0.003870
0.40986	-0.84694	0.003850
0.42579	-0.84649	0.003830
0.44196	-0.84593	0.003810
0.45833	-0.84485	0.003790
0.47486	-0.84199	0.003740
0.49152	-0.83220	0.003610
0.50827	-0.80322	0.003310
0.52506	-0.73892	0.002860
0.54185	-0.65741	0.002600
0.55861	-0.59823	0.002610
0.57528	-0.57118	0.002720
0.59183	-0.56426	0.002820
0.60822	-0.56248	0.002880
0.62441	-0.55667	0.002880
0.64036	-0.54426	0.002840
0.65604	-0.52728	0.002780
0.67141	-0.50696	0.002700
0.68645	-0.48223	0.002600
0.70113	-0.45423	0.002490
0.71543	-0.42519	0.002380
0.72933	-0.39554	0.002270
0.74281	-0.36593	0.002160
0.75586	-0.33689	0.002060
0.76847	-0.30819	0.001950
0.78063	-0.28040	0.001860
0.79234	-0.25374	0.001770
0.80360	-0.22812	0.001680
0.81440	-0.20355	0.001600
0.82475	-0.18030	0.001520
0.83465	-0.15814	0.001440
0.84412	-0.13702	0.001370
0.85314	-0.11713	0.001310
0.86175	-0.09830	0.001240
0.86993	-0.08047	0.001180
0.87771	-0.06358	0.001130
0.88511	-0.04765	0.001070
0.89211	-0.03262	0.001020
0.89876	-0.01839	0.000970
0.90504	-0.00502	0.000920
0.91098	0.00775	0.000880
0.91660	0.01974	0.000840
0.92190	0.03103	0.000790
0.92691	0.04182	0.000750
0.93162	0.05182	0.000720
0.93607	0.06128	0.000680
0.94025	0.07022	0.000650
0.94418	0.07857	0.000610
0.94788	0.08647	0.000580
0.95136	0.09390	0.000560
0.95483	0.10110	0.000530
0.95829	0.10833	0.000500
0.96170	0.11548	0.000470
0.96502	0.12246	0.000440
0.96825	0.12918	0.000410
0.97134	0.13559	0.000390
0.97429	0.14166	0.000360
0.97707	0.14733	0.000340
0.97968	0.15267	0.000320
0.98211	0.15760	0.000300
0.98435	0.16205	0.000280
0.98642	0.16618	0.000260
0.98831	0.16988	0.000250
0.99003	0.17319	0.000230
0.99159	0.17623	0.000220
0.99300	0.17884	0.000210
0.99426	0.18119	0.000200
0.99539	0.18334	0.000200
0.99641	0.18513	0.000200
0.99731	0.18666	0.000190
0.99811	0.18814	0.000200
0.99882	0.18906	0.000220
0.99945	0.19050	0.000350
1.00000	0.19177	0.000350

WING SECTION 3   Y/BO2 0.289 (Y = 220. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.02235	-0.000420
0.00001	1.02698	-0.000140
0.00005	1.02694	0.000150
0.00012	1.02384	0.000460
0.00022	1.01736	0.000780
0.00035	1.00742	0.001100
0.00051	0.99381	0.001430
0.00071	0.97666	0.001740
0.00094	0.95606	0.002050
0.00120	0.93196	0.002350
0.00150	0.90485	0.002640
0.00184	0.87478	0.002910
0.00221	0.84221	0.003170
0.00261	0.80765	0.003410
0.00304	0.77138	0.003620
0.00351	0.73425	0.003800
0.00400	0.69670	0.003960
0.00452	0.65937	0.004080
0.00507	0.62289	0.004170
0.00564	0.58767	0.004240
0.00623	0.55404	0.004280
0.00685	0.52241	0.004310
0.00747	0.49268	0.004320
0.00812	0.46518	0.004330
0.00878	0.43901	0.004330
0.00878	0.43901	0.004330
0.00942	0.41487	0.004330
0.01012	0.39183	0.004340
0.01088	0.36750	0.004360
0.01170	0.34339	0.004380
0.01259	0.31823	0.004430
0.01355	0.29175	0.004480
0.01459	0.26502	0.004530
0.01570	0.23771	0.004570
0.01690	0.21016	0.004610
0.01819	0.18313	0.004620
0.01957	0.15717	0.004630
0.02105	0.13297	0.004620
0.02263	0.11103	0.004590
0.02432	0.09134	0.004560
0.02612	0.07380	0.004520
0.02802	0.05801	0.004500
0.03004	0.04284	0.004490
0.03217	0.02781	0.004480
0.03442	0.01395	0.004450
0.03678	0.00122	0.004430
0.03926	-0.01057	0.004410
0.04186	-0.02140	0.004380
0.04460	-0.03163	0.004360
0.04746	-0.04129	0.004340
0.05042	-0.05052	0.004320
0.05350	-0.05925	0.004290
0.05667	-0.06734	0.004260
0.05995	-0.07422	0.004230
0.06332	-0.08009	0.004200
0.06677	-0.08556	0.004170
0.07030	-0.09126	0.004150
0.07390	-0.09738	0.004140
0.07758	-0.10356	0.004130
0.08131	-0.10975	0.004110
0.08509	-0.11581	0.004100
0.08890	-0.12169	0.004080
0.09272	-0.12748	0.004070
0.09656	-0.13321	0.004060
0.10040	-0.13871	0.004050
0.10422	-0.14443	0.004040
0.10805	-0.15008	0.004030
0.11212	-0.15575	0.004030
0.11645	-0.16201	0.004020
0.12105	-0.16866	0.004020
0.12593	-0.17566	0.004020
0.13111	-0.18301	0.004010
0.13660	-0.19073	0.004010
0.14242	-0.19866	0.004000
0.14857	-0.20679	0.004000
0.15507	-0.21511	0.003990
0.16194	-0.22348	0.003980
0.16919	-0.23179	0.003970
0.17683	-0.23998	0.003960
0.18487	-0.24803	0.003940
0.19333	-0.25632	0.003940
0.20225	-0.26597	0.003940
0.21161	-0.27729	0.003950
0.22142	-0.29045	0.003970
0.23167	-0.30525	0.003990
0.24237	-0.32038	0.004000
0.25354	-0.33504	0.004000
0.26515	-0.34854	0.004000
0.27723	-0.36020	0.003970
0.28975	-0.36928	0.003940
0.30271	-0.37616	0.003910
0.31610	-0.38305	0.003890
0.32991	-0.39069	0.003870
0.34411	-0.39686	0.003830
0.35871	-0.39915	0.003780
0.37366	-0.39691	0.003710
0.38895	-0.39119	0.003620
0.40455	-0.38303	0.003550
0.42042	-0.37380	0.003480
0.43654	-0.36433	0.003410
0.45285	-0.35387	0.003350
0.46934	-0.34234	0.003280
0.48595	-0.33046	0.003220
0.50264	-0.31709	0.003150
0.51938	-0.29853	0.003030
0.53612	-0.27234	0.002890
0.55282	-0.23979	0.002720
0.56943	-0.20371	0.002550
0.58592	-0.16681	0.002390
0.60224	-0.13015	0.002240
0.61835	-0.09379	0.002090
0.63424	-0.05784	0.001950
0.64986	-0.02259	0.001810
0.66518	0.01191	0.001680
0.68019	0.04589	0.001550
0.69486	0.07914	0.001420
0.70917	0.11171	0.001290
0.72309	0.14338	0.001160
0.73662	0.17291	0.001060
0.74974	0.19927	0.000970
0.76245	0.22201	0.000920
0.77474	0.24086	0.000890
0.78660	0.25612	0.000880
0.79804	0.26846	0.000880
0.80903	0.27849	0.000890
0.81958	0.28673	0.000900
0.82969	0.29350	0.000920
0.83937	0.29898	0.000930
0.84862	0.30341	0.000960
0.85745	0.30691	0.000980
0.86587	0.30953	0.001000
0.87388	0.31146	0.001030
0.88149	0.31273	0.001060
0.88871	0.31342	0.001080
0.89556	0.31362	0.001110
0.90205	0.31339	0.001140
0.90820	0.31279	0.001170
0.91400	0.31187	0.001200
0.91949	0.31066	0.001220
0.92467	0.30922	0.001250
0.92955	0.30759	0.001280
0.93416	0.30575	0.001310
0.93849	0.30380	0.001330
0.94257	0.30163	0.001360
0.94641	0.29951	0.001390
0.95002	0.29711	0.001410
0.95363	0.29446	0.001440
0.95722	0.29178	0.001470
0.96075	0.28875	0.001500
0.96419	0.28559	0.001530
0.96752	0.28222	0.001560
0.97071	0.27870	0.001590
0.97374	0.27506	0.001620
0.97660	0.27132	0.001650
0.97927	0.26751	0.001690
0.98176	0.26366	0.001720
0.98405	0.25979	0.001750
0.98615	0.25592	0.001790
0.98808	0.25209	0.001820
0.98982	0.24826	0.001850
0.99140	0.24449	0.001890
0.99283	0.24075	0.001920
0.99410	0.23706	0.001960
0.99524	0.23336	0.002000
0.99626	0.22969	0.002040
0.99717	0.22597	0.002070
0.99797	0.22250	0.002130
0.99868	0.21887	0.002300
0.99931	0.21613	0.002970

WING SECTION 3   Y/BO2 0.289 (Y = 220. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.02631	0.000630
0.00001	1.01953	0.000670
0.00004	1.01237	0.000930
0.00008	1.00254	0.001190
0.00015	0.99029	0.001440
0.00024	0.97558	0.001690
0.00035	0.95842	0.001930
0.00049	0.93883	0.002170
0.00065	0.91688	0.002400
0.00084	0.89286	0.002610
0.00105	0.86672	0.002830
0.00129	0.83851	0.003030
0.00155	0.80863	0.003230
0.00184	0.77705	0.003410
0.00216	0.74407	0.003590
0.00250	0.70996	0.003750
0.00288	0.67488	0.003900
0.00328	0.63917	0.004030
0.00370	0.60310	0.004150
0.00416	0.56678	0.004270
0.00464	0.53052	0.004370
0.00514	0.49445	0.004460
0.00568	0.45860	0.004540
0.00623	0.42329	0.004630
0.00682	0.38769	0.004760
0.00740	0.35272	0.004790
0.00805	0.31741	0.004880
0.00875	0.27934	0.005000
0.00952	0.23838	0.005140
0.01035	0.19446	0.005270
0.01125	0.14765	0.005420
0.01224	0.09733	0.005590
0.01330	0.04306	0.005760
0.01445	-0.01575	0.005950
0.01570	-0.07878	0.006150
0.01705	-0.14613	0.006340
0.01850	-0.21775	0.006510
0.02007	-0.29212	0.006670
0.02175	-0.36769	0.006790
0.02356	-0.44287	0.006870
0.02550	-0.51556	0.006900
0.02758	-0.58357	0.006880
0.02979	-0.64519	0.006830
0.03213	-0.69989	0.006750
0.03460	-0.74811	0.006660
0.03719	-0.79012	0.006570
0.03991	-0.82738	0.006490
0.04276	-0.86133	0.006420
0.04573	-0.89243	0.006350
0.04882	-0.92177	0.006290
0.05202	-0.94967	0.006240
0.05532	-0.97590	0.006180
0.05872	-1.00003	0.006120
0.06222	-1.02195	0.006060
0.06580	-1.04231	0.006000
0.06945	-1.06085	0.005940
0.07316	-1.07721	0.005870
0.07694	-1.09130	0.005800
0.08075	-1.10270	0.005730
0.08460	-1.11170	0.005660
0.08847	-1.11935	0.005590
0.09234	-1.12497	0.005520
0.09622	-1.12830	0.005450
0.10008	-1.12999	0.005370
0.10392	-1.13043	0.005310
0.10778	-1.13026	0.005250
0.11189	-1.13005	0.005210
0.11626	-1.13010	0.005170
0.12090	-1.12948	0.005110
0.12583	-1.12791	0.005060
0.13106	-1.12549	0.005010
0.13660	-1.12267	0.004960
0.14247	-1.11986	0.004910
0.14869	-1.11685	0.004870
0.15526	-1.11424	0.004830
0.16220	-1.11157	0.004780
0.16954	-1.10845	0.004740
0.17729	-1.10510	0.004700
0.18544	-1.10146	0.004660
0.19401	-1.09805	0.004620
0.20300	-1.09433	0.004580
0.21244	-1.08982	0.004530
0.22232	-1.08461	0.004490
0.23265	-1.07799	0.004430
0.24344	-1.06952	0.004380
0.25469	-1.05735	0.004310
0.26639	-1.03980	0.004230
0.27854	-1.01696	0.004130
0.29114	-0.98978	0.003990
0.30420	-0.96068	0.003850
0.31768	-0.93323	0.003720
0.33159	-0.91055	0.003640
0.34590	-0.89523	0.003610
0.36059	-0.88722	0.003640
0.37564	-0.88357	0.003680
0.39102	-0.88200	0.003720
0.40671	-0.88041	0.003730
0.42267	-0.87562	0.003690
0.43888	-0.85974	0.003510
0.45529	-0.81315	0.003050
0.47187	-0.72457	0.002530
0.48858	-0.63089	0.002360
0.50538	-0.57379	0.002470
0.52223	-0.55328	0.002640
0.53909	-0.55290	0.002800
0.55591	-0.55727	0.002910
0.57265	-0.55858	0.002950
0.58927	-0.55519	0.002970
0.60574	-0.54747	0.002950
0.62200	-0.53612	0.002920
0.63804	-0.52189	0.002870
0.65380	-0.50573	0.002810
0.66926	-0.48672	0.002730
0.68440	-0.46314	0.002630
0.69917	-0.43633	0.002520
0.71356	-0.40823	0.002410
0.72755	-0.37963	0.002300
0.74112	-0.35107	0.002190
0.75426	-0.32282	0.002090
0.76696	-0.29498	0.001980
0.77921	-0.26789	0.001890
0.79101	-0.24175	0.001790
0.80236	-0.21657	0.001700
0.81325	-0.19257	0.001620
0.82368	-0.16974	0.001540
0.83367	-0.14801	0.001470
0.84321	-0.12733	0.001390
0.85232	-0.10774	0.001330
0.86100	-0.08925	0.001260
0.86926	-0.07171	0.001200
0.87711	-0.05513	0.001150
0.88457	-0.03946	0.001090
0.89165	-0.02468	0.001040
0.89835	-0.01068	0.000990
0.90470	0.00249	0.000940
0.91070	0.01506	0.000890
0.91637	0.02685	0.000850
0.92173	0.03800	0.000810
0.92678	0.04862	0.000770
0.93155	0.05846	0.000730
0.93603	0.06778	0.000690
0.94026	0.07663	0.000660
0.94423	0.08484	0.000630
0.94797	0.09268	0.000600
0.95149	0.09998	0.000570
0.95499	0.10703	0.000540
0.95848	0.11421	0.000510
0.96192	0.12121	0.000480
0.96527	0.12808	0.000450
0.96851	0.13469	0.000420
0.97161	0.14098	0.000400
0.97456	0.14697	0.000370
0.97734	0.15248	0.000350
0.97995	0.15764	0.000330
0.98237	0.16255	0.000310
0.98460	0.16682	0.000290
0.98665	0.17086	0.000270
0.98853	0.17445	0.000260
0.99023	0.17767	0.000240
0.99177	0.18064	0.000230
0.99315	0.18312	0.000220
0.99439	0.18545	0.000210
0.99550	0.18751	0.000210
0.99650	0.18922	0.000200
0.99738	0.19071	0.000200
0.99816	0.19216	0.000210
0.99885	0.19302	0.000240
0.99946	0.19444	0.000370
1.00000	0.19576	0.000370

WING SECTION 4   Y/BO2 0.420 (Y = 320. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.02004	-0.000450
0.00001	1.02452	-0.000160
0.00005	1.02473	0.000120
0.00010	1.02223	0.000430
0.00019	1.01668	0.000740
0.00031	1.00802	0.001060
0.00045	0.99609	0.001380
0.00063	0.98092	0.001700
0.00083	0.96247	0.002010
0.00107	0.94078	0.002320
0.00134	0.91611	0.002610
0.00164	0.88866	0.002890
0.00197	0.85852	0.003160
0.00234	0.82623	0.003410
0.00273	0.79206	0.003640
0.00316	0.75650	0.003840
0.00361	0.72012	0.004020
0.00409	0.68338	0.004170
0.00460	0.64689	0.004290
0.00514	0.61113	0.004370
0.00570	0.57651	0.004440
0.00628	0.54334	0.004480
0.00689	0.51168	0.004490
0.00752	0.48239	0.004510
0.00816	0.45403	0.004510
0.00816	0.45403	0.004510
0.00879	0.42835	0.004490
0.00946	0.40450	0.004490
0.01019	0.37934	0.004500
0.01099	0.35400	0.004510
0.01185	0.32842	0.004530
0.01278	0.30221	0.004580
0.01378	0.27477	0.004630
0.01486	0.24672	0.004670
0.01602	0.21839	0.004710
0.01727	0.19000	0.004740
0.01861	0.16222	0.004750
0.02004	0.13610	0.004740
0.02157	0.11212	0.004720
0.02321	0.09039	0.004690
0.02495	0.07112	0.004650
0.02680	0.05408	0.004610
0.02875	0.03830	0.004590
0.03082	0.02309	0.004570
0.03300	0.00850	0.004560
0.03530	-0.00511	0.004540
0.03770	-0.01757	0.004510
0.04023	-0.02895	0.004480
0.04291	-0.03956	0.004460
0.04570	-0.04956	0.004430
0.04860	-0.05902	0.004410
0.05160	-0.06809	0.004390
0.05471	-0.07661	0.004370
0.05792	-0.08418	0.004340
0.06121	-0.09057	0.004300
0.06460	-0.09614	0.004270
0.06806	-0.10142	0.004240
0.07159	-0.10700	0.004220
0.07521	-0.11300	0.004210
0.07889	-0.11916	0.004200
0.08262	-0.12526	0.004180
0.08638	-0.13113	0.004170
0.09017	-0.13685	0.004160
0.09397	-0.14250	0.004140
0.09777	-0.14793	0.004130
0.10157	-0.15358	0.004120
0.10537	-0.15914	0.004110
0.10942	-0.16463	0.004100
0.11373	-0.17086	0.004100
0.11830	-0.17746	0.004100
0.12315	-0.18429	0.004090
0.12830	-0.19149	0.004080
0.13376	-0.19913	0.004080
0.13955	-0.20707	0.004070
0.14567	-0.21512	0.004070
0.15214	-0.22350	0.004060
0.15898	-0.23189	0.004050
0.16619	-0.24022	0.004040
0.17380	-0.24851	0.004030
0.18181	-0.25651	0.004010
0.19023	-0.26458	0.004000
0.19915	-0.27355	0.004000
0.20850	-0.28413	0.004000
0.21830	-0.29669	0.004020
0.22855	-0.31100	0.004040
0.23926	-0.32611	0.004050
0.25042	-0.34095	0.004060
0.26204	-0.35470	0.004060
0.27412	-0.36672	0.004040
0.28665	-0.37623	0.004000
0.29962	-0.38309	0.003970
0.31302	-0.38932	0.003940
0.32684	-0.39639	0.003920
0.34107	-0.40265	0.003890
0.35568	-0.40536	0.003830
0.37066	-0.40339	0.003760
0.38598	-0.39761	0.003680
0.40161	-0.38930	0.003600
0.41752	-0.37955	0.003530
0.43368	-0.36934	0.003460
0.45005	-0.35846	0.003390
0.46659	-0.34664	0.003320
0.48325	-0.33425	0.003260
0.50000	-0.32082	0.003190
0.51679	-0.30301	0.003080
0.53360	-0.27767	0.002930
0.55036	-0.24571	0.002760
0.56704	-0.20980	0.002590
0.58361	-0.17262	0.002420
0.59999	-0.13571	0.002270
0.61618	-0.09929	0.002120
0.63213	-0.06323	0.001970
0.64782	-0.02779	0.001840
0.66322	0.00684	0.001700
0.67830	0.04089	0.001570
0.69305	0.07421	0.001430
0.70745	0.10685	0.001300
0.72146	0.13859	0.001170
0.73506	0.16825	0.001060
0.74827	0.19487	0.000970
0.76105	0.21796	0.000910
0.77343	0.23718	0.000880
0.78538	0.25277	0.000870
0.79690	0.26538	0.000870
0.80797	0.27564	0.000880
0.81861	0.28406	0.000890
0.82880	0.29097	0.000910
0.83856	0.29657	0.000930
0.84788	0.30113	0.000950
0.85679	0.30473	0.000970
0.86529	0.30744	0.001000
0.87337	0.30946	0.001030
0.88105	0.31079	0.001050
0.88835	0.31154	0.001080
0.89527	0.31178	0.001110
0.90182	0.31160	0.001140
0.90803	0.31103	0.001170
0.91389	0.31013	0.001200
0.91943	0.30896	0.001230
0.92467	0.30752	0.001250
0.92960	0.30590	0.001280
0.93425	0.30405	0.001310
0.93864	0.30210	0.001340
0.94276	0.29993	0.001360
0.94664	0.29783	0.001390
0.95029	0.29538	0.001420
0.95394	0.29268	0.001450
0.95756	0.29002	0.001480
0.96112	0.28696	0.001510
0.96459	0.28377	0.001540
0.96793	0.28039	0.001570
0.97112	0.27685	0.001600
0.97415	0.27320	0.001640
0.97700	0.26946	0.001670
0.97966	0.26566	0.001700
0.98213	0.26182	0.001740
0.98440	0.25796	0.001770
0.98649	0.25413	0.001810
0.98838	0.25033	0.001840
0.99010	0.24655	0.001880
0.99165	0.24283	0.001910
0.99304	0.23916	0.001950
0.99429	0.23552	0.001980
0.99541	0.23191	0.002020
0.99640	0.22829	0.002060
0.99728	0.22466	0.002100
0.99806	0.22125	0.002170
0.99875	0.21766	0.002340
0.99936	0.21512	0.003040

WING SECTION 4   Y/BO2 0.420 (Y = 320. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.02382	0.000650
0.00001	1.01744	0.000680
0.00003	1.01086	0.000930
0.00008	1.00187	0.001190
0.00013	0.99067	0.001440
0.00022	0.97723	0.001680
0.00032	0.96152	0.001920
0.00044	0.94357	0.002160
0.00058	0.92352	0.002390
0.00075	0.90142	0.002610
0.00094	0.87731	0.002820
0.00115	0.85120	0.003030
0.00139	0.82333	0.003230
0.00166	0.79389	0.003420
0.00195	0.76286	0.003600
0.00226	0.73060	0.003760
0.00261	0.69719	0.003920
0.00298	0.66293	0.004060
0.00337	0.62804	0.004190
0.00379	0.59260	0.004310
0.00424	0.55703	0.004420
0.00472	0.52134	0.004520
0.00523	0.48559	0.004600
0.00576	0.45034	0.004690
0.00632	0.41460	0.004820
0.00689	0.37976	0.004850
0.00751	0.34459	0.004930
0.00818	0.30713	0.005030
0.00891	0.26732	0.005150
0.00971	0.22468	0.005270
0.01058	0.17935	0.005420
0.01153	0.13041	0.005590
0.01255	0.07762	0.005760
0.01365	0.02098	0.005940
0.01485	-0.03987	0.006130
0.01614	-0.10546	0.006330
0.01754	-0.17534	0.006520
0.01904	-0.24874	0.006690
0.02066	-0.32435	0.006840
0.02241	-0.40049	0.006940
0.02427	-0.47507	0.007000
0.02627	-0.54605	0.007000
0.02840	-0.61104	0.006950
0.03066	-0.66908	0.006880
0.03303	-0.72035	0.006800
0.03553	-0.76538	0.006710
0.03816	-0.80516	0.006620
0.04091	-0.84081	0.006540
0.04378	-0.87383	0.006470
0.04676	-0.90448	0.006420
0.04986	-0.93347	0.006360
0.05307	-0.96084	0.006300
0.05637	-0.98596	0.006240
0.05977	-1.00933	0.006190
0.06325	-1.03090	0.006120
0.06680	-1.05051	0.006060
0.07043	-1.06822	0.006000
0.07412	-1.08400	0.005940
0.07786	-1.09744	0.005860
0.08163	-1.10820	0.005780
0.08543	-1.11691	0.005720
0.08924	-1.12450	0.005650
0.09306	-1.12979	0.005570
0.09687	-1.13268	0.005500
0.10066	-1.13460	0.005440
0.10449	-1.13540	0.005380
0.10857	-1.13547	0.005320
0.11290	-1.13570	0.005280
0.11751	-1.13629	0.005230
0.12241	-1.13570	0.005170
0.12761	-1.13409	0.005120
0.13311	-1.13245	0.005070
0.13895	-1.13043	0.005020
0.14513	-1.12835	0.004970
0.15167	-1.12626	0.004930
0.15857	-1.12458	0.004890
0.16589	-1.12310	0.004850
0.17361	-1.12123	0.004810
0.18174	-1.11936	0.004770
0.19029	-1.11759	0.004730
0.19927	-1.11603	0.004700
0.20868	-1.11452	0.004660
0.21855	-1.11287	0.004620
0.22886	-1.11034	0.004580
0.23964	-1.10781	0.004540
0.25087	-1.10510	0.004500
0.26256	-1.10120	0.004450
0.27471	-1.09749	0.004410
0.28731	-1.09386	0.004380
0.30036	-1.09036	0.004340
0.31386	-1.08616	0.004300
0.32778	-1.08055	0.004250
0.34211	-1.07466	0.004220
0.35682	-1.06822	0.004180
0.37189	-1.05950	0.004130
0.38730	-1.04541	0.004020
0.40303	-1.01659	0.003730
0.41903	-0.92590	0.002790
0.43528	-0.76246	0.001620
0.45174	-0.60925	0.001290
0.46838	-0.52778	0.001560
0.48515	-0.50568	0.001910
0.50201	-0.50857	0.002230
0.51893	-0.51561	0.002470
0.53585	-0.52065	0.002630
0.55275	-0.52402	0.002750
0.56957	-0.52504	0.002820
0.58628	-0.52343	0.002870
0.60284	-0.51919	0.002890
0.61920	-0.51138	0.002880
0.63533	-0.49996	0.002850
0.65119	-0.48625	0.002800
0.66676	-0.47003	0.002730
0.68199	-0.44910	0.002640
0.69687	-0.42412	0.002530
0.71136	-0.39784	0.002430
0.72546	-0.37057	0.002320
0.73914	-0.34290	0.002210
0.75239	-0.31568	0.002100
0.76520	-0.28840	0.002000
0.77756	-0.26173	0.001900
0.78946	-0.23617	0.001810
0.80091	-0.21152	0.001720
0.81191	-0.18801	0.001630
0.82244	-0.16531	0.001550
0.83253	-0.14380	0.001480
0.84216	-0.12348	0.001400
0.85136	-0.10398	0.001330
0.86013	-0.08560	0.001270
0.86848	-0.06824	0.001210
0.87641	-0.05182	0.001150
0.88395	-0.03632	0.001090
0.89110	-0.02166	0.001040
0.89788	-0.00786	0.000990
0.90430	0.00527	0.000940
0.91037	0.01777	0.000890
0.91610	0.02942	0.000850
0.92152	0.04047	0.000810
0.92663	0.05102	0.000770
0.93145	0.06081	0.000730
0.93599	0.06997	0.000690
0.94027	0.07879	0.000660
0.94429	0.08691	0.000620
0.94808	0.09474	0.000590
0.95163	0.10194	0.000570
0.95518	0.10888	0.000540
0.95871	0.11607	0.000510
0.96217	0.12294	0.000480
0.96555	0.12970	0.000450
0.96881	0.13625	0.000420
0.97193	0.14245	0.000390
0.97488	0.14832	0.000370
0.97767	0.15372	0.000350
0.98027	0.15874	0.000320
0.98268	0.16358	0.000300
0.98490	0.16769	0.000290
0.98693	0.17164	0.000270
0.98878	0.17515	0.000260
0.99046	0.17824	0.000240
0.99197	0.18116	0.000230
0.99333	0.18350	0.000220
0.99455	0.18580	0.000210
0.99563	0.18779	0.000210
0.99660	0.18943	0.000210
0.99746	0.19080	0.000200
0.99822	0.19220	0.000210
0.99889	0.19305	0.000240
0.99948	0.19451	0.000370
1.00000	0.19587	0.000370

WING SECTION 5   Y/BO2 0.551 (Y = 420. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.01922	-0.000510
0.00001	1.02294	-0.000140
0.00004	1.02299	0.000140
0.00009	1.02073	0.000430
0.00017	1.01582	0.000740
0.00026	1.00820	0.001050
0.00039	0.99771	0.001370
0.00054	0.98430	0.001680
0.00072	0.96797	0.001990
0.00092	0.94871	0.002290
0.00116	0.92663	0.002590
0.00142	0.90175	0.002880
0.00171	0.87441	0.003160
0.00203	0.84474	0.003420
0.00238	0.81289	0.003660
0.00276	0.77940	0.003890
0.00317	0.74448	0.004100
0.00360	0.70865	0.004270
0.00407	0.67242	0.004420
0.00456	0.63619	0.004540
0.00508	0.60038	0.004620
0.00563	0.56543	0.004690
0.00621	0.53146	0.004720
0.00681	0.49966	0.004740
0.00745	0.46838	0.004740
0.00745	0.46838	0.004750
0.00805	0.44048	0.004720
0.00869	0.41531	0.004700
0.00939	0.38874	0.004710
0.01015	0.36241	0.004700
0.01098	0.33564	0.004710
0.01187	0.30890	0.004720
0.01284	0.28123	0.004770
0.01388	0.25249	0.004810
0.01499	0.22334	0.004850
0.01619	0.19383	0.004890
0.01748	0.16456	0.004910
0.01886	0.13610	0.004910
0.02033	0.10960	0.004890
0.02190	0.08549	0.004860
0.02358	0.06389	0.004810
0.02536	0.04496	0.004760
0.02724	0.02814	0.004720
0.02924	0.01259	0.004700
0.03134	-0.00251	0.004680
0.03355	-0.01686	0.004670
0.03586	-0.03004	0.004640
0.03831	-0.04222	0.004610
0.04091	-0.05331	0.004580
0.04363	-0.06357	0.004550
0.04645	-0.07321	0.004530
0.04937	-0.08240	0.004510
0.05240	-0.09114	0.004480
0.05552	-0.09922	0.004460
0.05873	-0.10631	0.004420
0.06203	-0.11217	0.004380
0.06541	-0.11701	0.004350
0.06886	-0.12210	0.004330
0.07241	-0.12784	0.004310
0.07603	-0.13359	0.004300
0.07970	-0.13942	0.004280
0.08341	-0.14521	0.004270
0.08714	-0.15081	0.004250
0.09090	-0.15629	0.004240
0.09466	-0.16157	0.004230
0.09843	-0.16707	0.004220
0.10221	-0.17248	0.004200
0.10623	-0.17780	0.004190
0.11050	-0.18371	0.004190
0.11504	-0.18998	0.004180
0.11986	-0.19670	0.004170
0.12498	-0.20383	0.004170
0.13041	-0.21126	0.004160
0.13615	-0.21900	0.004160
0.14224	-0.22714	0.004150
0.14867	-0.23541	0.004140
0.15548	-0.24382	0.004140
0.16265	-0.25216	0.004120
0.17022	-0.26036	0.004110
0.17819	-0.26858	0.004100
0.18657	-0.27657	0.004080
0.19548	-0.28481	0.004070
0.20483	-0.29470	0.004070
0.21462	-0.30655	0.004090
0.22487	-0.32024	0.004100
0.23557	-0.33525	0.004120
0.24674	-0.35040	0.004130
0.25836	-0.36466	0.004130
0.27045	-0.37726	0.004120
0.28299	-0.38761	0.004080
0.29597	-0.39503	0.004040
0.30938	-0.40073	0.004010
0.32322	-0.40730	0.003990
0.33747	-0.41377	0.003960
0.35211	-0.41717	0.003910
0.36712	-0.41589	0.003840
0.38247	-0.41022	0.003750
0.39815	-0.40176	0.003670
0.41410	-0.39154	0.003590
0.43031	-0.38073	0.003510
0.44674	-0.36936	0.003440
0.46334	-0.35699	0.003370
0.48006	-0.34411	0.003310
0.49687	-0.33035	0.003230
0.51374	-0.31312	0.003130
0.53062	-0.28882	0.002990
0.54746	-0.25730	0.002810
0.56423	-0.22133	0.002630
0.58088	-0.18371	0.002460
0.59735	-0.14640	0.002300
0.61361	-0.10959	0.002150
0.62964	-0.07303	0.002000
0.64542	-0.03713	0.001860
0.66091	-0.00219	0.001720
0.67608	0.03213	0.001580
0.69093	0.06573	0.001450
0.70542	0.09846	0.001310
0.71952	0.13038	0.001180
0.73323	0.16046	0.001060
0.74653	0.18747	0.000970
0.75941	0.21103	0.000910
0.77189	0.23080	0.000870
0.78394	0.24686	0.000860
0.79555	0.25988	0.000860
0.80673	0.27045	0.000870
0.81746	0.27913	0.000880
0.82774	0.28630	0.000900
0.83759	0.29209	0.000920
0.84701	0.29684	0.000940
0.85601	0.30060	0.000960
0.86460	0.30344	0.000990
0.87277	0.30558	0.001020
0.88054	0.30703	0.001050
0.88792	0.30787	0.001080
0.89491	0.30819	0.001100
0.90154	0.30808	0.001130
0.90782	0.30756	0.001160
0.91376	0.30672	0.001190
0.91937	0.30558	0.001220
0.92466	0.30417	0.001250
0.92966	0.30257	0.001280
0.93437	0.30074	0.001310
0.93881	0.29881	0.001340
0.94298	0.29663	0.001370
0.94691	0.29456	0.001400
0.95061	0.29208	0.001430
0.95431	0.28932	0.001450
0.95797	0.28668	0.001480
0.96156	0.28359	0.001520
0.96505	0.28036	0.001550
0.96841	0.27696	0.001580
0.97161	0.27344	0.001610
0.97464	0.26975	0.001650
0.97748	0.26601	0.001680
0.98013	0.26225	0.001720
0.98257	0.25839	0.001750
0.98482	0.25458	0.001790
0.98687	0.25082	0.001820
0.98874	0.24706	0.001860
0.99042	0.24332	0.001890
0.99194	0.23963	0.001930
0.99330	0.23606	0.001960
0.99452	0.23252	0.002000
0.99560	0.22896	0.002040
0.99656	0.22544	0.002080
0.99741	0.22192	0.002120
0.99816	0.21856	0.002190
0.99882	0.21506	0.002370
0.99941	0.21279	0.003110

WING SECTION 5   Y/BO2 0.551 (Y = 420. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.02243	0.000710
0.00001	1.01706	0.000640
0.00003	1.01150	0.000890
0.00006	1.00382	0.001140
0.00012	0.99418	0.001380
0.00019	0.98254	0.001620
0.00027	0.96890	0.001860
0.00038	0.95325	0.002090
0.00050	0.93564	0.002320
0.00065	0.91610	0.002540
0.00082	0.89465	0.002760
0.00101	0.87140	0.002960
0.00122	0.84635	0.003170
0.00145	0.81961	0.003360
0.00171	0.79134	0.003550
0.00199	0.76160	0.003720
0.00230	0.73056	0.003890
0.00263	0.69839	0.004040
0.00299	0.66530	0.004180
0.00338	0.63138	0.004310
0.00380	0.59685	0.004430
0.00424	0.56199	0.004540
0.00472	0.52662	0.004630
0.00522	0.49145	0.004720
0.00576	0.45564	0.004850
0.00630	0.42095	0.004880
0.00688	0.38647	0.004950
0.00752	0.34925	0.005050
0.00822	0.31080	0.005150
0.00898	0.26969	0.005270
0.00980	0.22547	0.005410
0.01070	0.17855	0.005560
0.01168	0.12818	0.005720
0.01273	0.07395	0.005900
0.01387	0.01546	0.006090
0.01510	-0.04740	0.006290
0.01643	-0.11453	0.006490
0.01786	-0.18591	0.006680
0.01940	-0.26053	0.006840
0.02106	-0.33664	0.006980
0.02284	-0.41270	0.007060
0.02474	-0.48635	0.007090
0.02677	-0.55491	0.007070
0.02894	-0.61715	0.007000
0.03121	-0.67206	0.006910
0.03359	-0.72000	0.006830
0.03610	-0.76257	0.006750
0.03873	-0.80120	0.006670
0.04149	-0.83627	0.006600
0.04436	-0.86835	0.006530
0.04733	-0.89859	0.006480
0.05042	-0.92734	0.006420
0.05361	-0.95406	0.006370
0.05688	-0.97868	0.006310
0.06025	-1.00170	0.006250
0.06369	-1.02265	0.006190
0.06722	-1.04177	0.006130
0.07080	-1.05922	0.006060
0.07444	-1.07458	0.006000
0.07813	-1.08752	0.005920
0.08184	-1.09791	0.005850
0.08558	-1.10635	0.005780
0.08933	-1.11367	0.005720
0.09308	-1.11863	0.005640
0.09682	-1.12169	0.005570
0.10061	-1.12377	0.005500
0.10465	-1.12432	0.005430
0.10895	-1.12446	0.005390
0.11352	-1.12516	0.005340
0.11838	-1.12530	0.005280
0.12353	-1.12457	0.005230
0.12900	-1.12336	0.005170
0.13480	-1.12145	0.005120
0.14094	-1.11954	0.005070
0.14743	-1.11757	0.005020
0.15429	-1.11591	0.004980
0.16158	-1.11466	0.004940
0.16928	-1.11320	0.004900
0.17738	-1.11150	0.004860
0.18590	-1.11010	0.004820
0.19486	-1.10908	0.004780
0.20425	-1.10803	0.004740
0.21409	-1.10670	0.004700
0.22439	-1.10531	0.004670
0.23515	-1.10391	0.004630
0.24636	-1.10204	0.004590
0.25805	-1.09944	0.004550
0.27019	-1.09665	0.004510
0.28278	-1.09420	0.004470
0.29583	-1.09214	0.004440
0.30934	-1.09005	0.004400
0.32328	-1.08702	0.004370
0.33762	-1.08359	0.004330
0.35236	-1.08053	0.004300
0.36746	-1.07723	0.004260
0.38291	-1.07237	0.004200
0.39868	-1.06028	0.004030
0.41473	-1.01173	0.003340
0.43103	-0.86699	0.001940
0.44754	-0.66617	0.001020
0.46424	-0.52348	0.001120
0.48108	-0.46764	0.001510
0.49802	-0.46408	0.001910
0.51501	-0.47353	0.002230
0.53203	-0.48181	0.002450
0.54901	-0.48895	0.002620
0.56593	-0.49403	0.002740
0.58275	-0.49660	0.002810
0.59941	-0.49595	0.002850
0.61588	-0.49156	0.002860
0.63212	-0.48345	0.002840
0.64810	-0.47239	0.002810
0.66378	-0.45837	0.002760
0.67914	-0.43968	0.002670
0.69415	-0.41679	0.002570
0.70877	-0.39162	0.002460
0.72299	-0.36543	0.002350
0.73680	-0.33874	0.002240
0.75018	-0.31193	0.002140
0.76311	-0.28526	0.002030
0.77560	-0.25901	0.001930
0.78763	-0.23371	0.001830
0.79920	-0.20931	0.001740
0.81032	-0.18572	0.001660
0.82097	-0.16326	0.001570
0.83117	-0.14188	0.001490
0.84092	-0.12158	0.001420
0.85022	-0.10230	0.001350
0.85910	-0.08389	0.001280
0.86755	-0.06660	0.001220
0.87558	-0.05023	0.001160
0.88322	-0.03477	0.001100
0.89046	-0.02015	0.001050
0.89732	-0.00641	0.001000
0.90382	0.00669	0.000950
0.90997	0.01914	0.000900
0.91579	0.03075	0.000860
0.92128	0.04178	0.000810
0.92646	0.05222	0.000770
0.93134	0.06195	0.000730
0.93595	0.07111	0.000690
0.94028	0.07989	0.000660
0.94436	0.08793	0.000620
0.94820	0.09574	0.000590
0.95181	0.10285	0.000570
0.95540	0.10971	0.000530
0.95897	0.11689	0.000500
0.96248	0.12369	0.000470
0.96588	0.13034	0.000450
0.96917	0.13671	0.000420
0.97230	0.14283	0.000390
0.97527	0.14855	0.000370
0.97805	0.15390	0.000340
0.98064	0.15877	0.000320
0.98304	0.16337	0.000300
0.98524	0.16749	0.000280
0.98725	0.17124	0.000270
0.98908	0.17461	0.000250
0.99073	0.17766	0.000240
0.99221	0.18034	0.000230
0.99354	0.18267	0.000220
0.99473	0.18488	0.000210
0.99578	0.18671	0.000210
0.99672	0.18829	0.000200
0.99755	0.18965	0.000200
0.99829	0.19102	0.000210
0.99893	0.19178	0.000240
0.99950	0.19326	0.000380
1.00000	0.19472	0.000380

WING SECTION 6   Y/BO2 0.682 (Y = 520. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.01898	-0.000650
0.00001	1.02131	-0.000040
0.00003	1.02080	0.000220
0.00007	1.01843	0.000500
0.00013	1.01387	0.000790
0.00021	1.00706	0.001090
0.00032	0.99782	0.001390
0.00044	0.98608	0.001690
0.00059	0.97182	0.001990
0.00075	0.95500	0.002290
0.00095	0.93563	0.002590
0.00117	0.91371	0.002880
0.00141	0.88935	0.003160
0.00168	0.86265	0.003430
0.00198	0.83360	0.003700
0.00231	0.80261	0.003950
0.00266	0.76978	0.004180
0.00304	0.73535	0.004380
0.00345	0.69971	0.004570
0.00389	0.66321	0.004730
0.00436	0.62621	0.004850
0.00487	0.58922	0.004950
0.00542	0.55225	0.005020
0.00600	0.51701	0.005070
0.00662	0.48165	0.005070
0.00662	0.48165	0.005100
0.00718	0.45045	0.005070
0.00779	0.42313	0.005040
0.00845	0.39434	0.005020
0.00917	0.36624	0.005000
0.00996	0.33797	0.004990
0.01080	0.30950	0.004980
0.01172	0.28118	0.004990
0.01271	0.25222	0.005020
0.01377	0.22209	0.005050
0.01492	0.19160	0.005090
0.01614	0.16068	0.005120
0.01745	0.13013	0.005140
0.01886	0.10078	0.005140
0.02035	0.07336	0.005110
0.02195	0.04853	0.005060
0.02365	0.02661	0.005000
0.02544	0.00766	0.004940
0.02734	-0.00900	0.004890
0.02935	-0.02427	0.004860
0.03146	-0.03923	0.004840
0.03367	-0.05333	0.004820
0.03601	-0.06621	0.004790
0.03852	-0.07820	0.004750
0.04114	-0.08900	0.004720
0.04387	-0.09884	0.004680
0.04670	-0.10802	0.004650
0.04963	-0.11670	0.004630
0.05265	-0.12500	0.004600
0.05576	-0.13257	0.004570
0.05896	-0.13912	0.004540
0.06224	-0.14451	0.004500
0.06559	-0.14881	0.004460
0.06905	-0.15344	0.004440
0.07259	-0.15872	0.004430
0.07619	-0.16407	0.004410
0.07983	-0.16956	0.004390
0.08351	-0.17489	0.004380
0.08721	-0.18007	0.004360
0.09093	-0.18504	0.004350
0.09466	-0.19026	0.004330
0.09841	-0.19537	0.004320
0.10239	-0.20046	0.004310
0.10663	-0.20615	0.004300
0.11113	-0.21195	0.004290
0.11591	-0.21834	0.004280
0.12099	-0.22509	0.004280
0.12638	-0.23213	0.004270
0.13208	-0.23976	0.004260
0.13812	-0.24756	0.004260
0.14451	-0.25580	0.004250
0.15127	-0.26413	0.004240
0.15840	-0.27248	0.004230
0.16592	-0.28090	0.004210
0.17385	-0.28902	0.004200
0.18218	-0.29670	0.004180
0.19107	-0.30467	0.004170
0.20042	-0.31361	0.004160
0.21021	-0.32449	0.004170
0.22045	-0.33735	0.004180
0.23115	-0.35198	0.004200
0.24232	-0.36751	0.004220
0.25395	-0.38215	0.004220
0.26605	-0.39567	0.004210
0.27860	-0.40684	0.004180
0.29159	-0.41498	0.004140
0.30502	-0.42075	0.004100
0.31888	-0.42645	0.004070
0.33315	-0.43269	0.004040
0.34783	-0.43679	0.003990
0.36287	-0.43629	0.003920
0.37827	-0.43090	0.003830
0.39399	-0.42198	0.003740
0.41001	-0.41090	0.003650
0.42628	-0.39912	0.003570
0.44277	-0.38688	0.003500
0.45945	-0.37365	0.003420
0.47625	-0.35983	0.003350
0.49313	-0.34535	0.003280
0.51008	-0.32832	0.003180
0.52705	-0.30484	0.003040
0.54399	-0.27374	0.002860
0.56085	-0.23757	0.002680
0.57761	-0.19928	0.002500
0.59418	-0.16118	0.002330
0.61054	-0.12358	0.002170
0.62667	-0.08632	0.002020
0.64255	-0.04980	0.001870
0.65814	-0.01427	0.001730
0.67342	0.02052	0.001590
0.68838	0.05461	0.001450
0.70299	0.08770	0.001310
0.71722	0.12000	0.001180
0.73104	0.15049	0.001060
0.74445	0.17795	0.000960
0.75745	0.20219	0.000900
0.77005	0.22263	0.000860
0.78222	0.23932	0.000840
0.79395	0.25289	0.000840
0.80524	0.26393	0.000850
0.81608	0.27300	0.000860
0.82648	0.28052	0.000880
0.83644	0.28661	0.000900
0.84596	0.29166	0.000920
0.85508	0.29571	0.000950
0.86378	0.29877	0.000970
0.87205	0.30113	0.001000
0.87992	0.30278	0.001030
0.88740	0.30382	0.001060
0.89449	0.30432	0.001090
0.90121	0.30434	0.001120
0.90758	0.30398	0.001150
0.91360	0.30327	0.001180
0.91929	0.30226	0.001210
0.92466	0.30095	0.001240
0.92973	0.29946	0.001270
0.93451	0.29773	0.001300
0.93901	0.29588	0.001330
0.94325	0.29377	0.001360
0.94724	0.29181	0.001390
0.95099	0.28937	0.001420
0.95475	0.28664	0.001450
0.95846	0.28408	0.001480
0.96209	0.28104	0.001510
0.96561	0.27792	0.001540
0.96899	0.27455	0.001580
0.97220	0.27112	0.001610
0.97523	0.26754	0.001650
0.97806	0.26390	0.001680
0.98069	0.26021	0.001720
0.98311	0.25649	0.001750
0.98532	0.25284	0.001780
0.98734	0.24919	0.001820
0.98917	0.24558	0.001860
0.99081	0.24202	0.001890
0.99229	0.23848	0.001930
0.99361	0.23506	0.001960
0.99478	0.23171	0.002000
0.99582	0.22828	0.002040
0.99675	0.22496	0.002080
0.99756	0.22160	0.002130
0.99828	0.21843	0.002200
0.99891	0.21520	0.002390
0.99947	0.21303	0.003150

WING SECTION 6   Y/BO2 0.682 (Y = 520. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.02122	0.000840
0.00001	1.01748	0.000520
0.00002	1.01338	0.000760
0.00005	1.00746	0.001000
0.00010	0.99995	0.001240
0.00015	0.99071	0.001470
0.00022	0.97970	0.001710
0.00031	0.96695	0.001940
0.00042	0.95248	0.002160
0.00054	0.93625	0.002380
0.00068	0.91826	0.002600
0.00084	0.89853	0.002810
0.00102	0.87712	0.003020
0.00122	0.85399	0.003220
0.00144	0.82927	0.003410
0.00168	0.80298	0.003590
0.00195	0.77519	0.003770
0.00225	0.74597	0.003940
0.00256	0.71547	0.004100
0.00291	0.68385	0.004240
0.00329	0.65110	0.004380
0.00369	0.61746	0.004500
0.00413	0.58293	0.004600
0.00460	0.54829	0.004710
0.00511	0.51252	0.004860
0.00561	0.47803	0.004880
0.00616	0.44419	0.004950
0.00675	0.40790	0.005050
0.00741	0.37007	0.005130
0.00812	0.33065	0.005240
0.00890	0.28858	0.005360
0.00974	0.24349	0.005500
0.01066	0.19576	0.005650
0.01165	0.14454	0.005820
0.01272	0.08933	0.006010
0.01388	0.02996	0.006200
0.01513	-0.03375	0.006400
0.01647	-0.10181	0.006610
0.01792	-0.17368	0.006800
0.01948	-0.24863	0.006960
0.02115	-0.32498	0.007090
0.02294	-0.40041	0.007170
0.02486	-0.47255	0.007180
0.02691	-0.53955	0.007140
0.02905	-0.59930	0.007060
0.03130	-0.65142	0.006960
0.03367	-0.69747	0.006870
0.03616	-0.73880	0.006800
0.03877	-0.77677	0.006730
0.04149	-0.81159	0.006660
0.04433	-0.84394	0.006610
0.04727	-0.87452	0.006550
0.05031	-0.90309	0.006490
0.05345	-0.92934	0.006440
0.05667	-0.95381	0.006380
0.05998	-0.97648	0.006320
0.06338	-0.99725	0.006260
0.06684	-1.01658	0.006200
0.07037	-1.03372	0.006140
0.07394	-1.04879	0.006070
0.07756	-1.06180	0.006000
0.08120	-1.07236	0.005920
0.08487	-1.08091	0.005860
0.08855	-1.08806	0.005790
0.09223	-1.09340	0.005710
0.09598	-1.09682	0.005640
0.09997	-1.09865	0.005570
0.10422	-1.09943	0.005510
0.10875	-1.09956	0.005450
0.11356	-1.09990	0.005400
0.11866	-1.09995	0.005340
0.12408	-1.09897	0.005280
0.12983	-1.09747	0.005220
0.13592	-1.09529	0.005170
0.14236	-1.09302	0.005120
0.14917	-1.09112	0.005070
0.15642	-1.08952	0.005030
0.16408	-1.08801	0.004990
0.17215	-1.08636	0.004940
0.18065	-1.08448	0.004900
0.18957	-1.08306	0.004860
0.19894	-1.08205	0.004820
0.20876	-1.08072	0.004780
0.21903	-1.07944	0.004740
0.22977	-1.07777	0.004700
0.24097	-1.07606	0.004660
0.25264	-1.07401	0.004620
0.26476	-1.07094	0.004570
0.27735	-1.06827	0.004540
0.29041	-1.06627	0.004510
0.30393	-1.06435	0.004470
0.31788	-1.06168	0.004430
0.33225	-1.05839	0.004390
0.34701	-1.05518	0.004360
0.36215	-1.05144	0.004310
0.37764	-1.04368	0.004190
0.39346	-1.02039	0.003740
0.40956	-0.92055	0.002510
0.42592	-0.73189	0.001290
0.44251	-0.55793	0.001160
0.45928	-0.47113	0.001550
0.47619	-0.45475	0.001980
0.49322	-0.46396	0.002320
0.51031	-0.47518	0.002570
0.52743	-0.48449	0.002750
0.54452	-0.49188	0.002870
0.56156	-0.49683	0.002960
0.57849	-0.49914	0.003010
0.59528	-0.49807	0.003020
0.61188	-0.49344	0.003020
0.62826	-0.48529	0.002990
0.64438	-0.47414	0.002950
0.66021	-0.46025	0.002890
0.67572	-0.44214	0.002800
0.69087	-0.41968	0.002690
0.70565	-0.39466	0.002570
0.72003	-0.36833	0.002460
0.73399	-0.34161	0.002350
0.74752	-0.31481	0.002230
0.76060	-0.28792	0.002130
0.77324	-0.26157	0.002020
0.78543	-0.23606	0.001920
0.79715	-0.21134	0.001830
0.80841	-0.18771	0.001730
0.81920	-0.16514	0.001650
0.82954	-0.14352	0.001570
0.83942	-0.12297	0.001490
0.84886	-0.10358	0.001420
0.85786	-0.08514	0.001350
0.86643	-0.06759	0.001280
0.87459	-0.05107	0.001220
0.88234	-0.03545	0.001160
0.88969	-0.02070	0.001100
0.89666	-0.00673	0.001050
0.90326	0.00657	0.001000
0.90950	0.01908	0.000950
0.91541	0.03088	0.000900
0.92099	0.04206	0.000850
0.92625	0.05264	0.000810
0.93122	0.06256	0.000770
0.93590	0.07185	0.000730
0.94030	0.08077	0.000690
0.94445	0.08894	0.000660
0.94835	0.09697	0.000620
0.95202	0.10415	0.000600
0.95567	0.11109	0.000560
0.95929	0.11849	0.000530
0.96284	0.12537	0.000500
0.96629	0.13218	0.000470
0.96960	0.13858	0.000440
0.97275	0.14473	0.000410
0.97573	0.15053	0.000390
0.97851	0.15596	0.000360
0.98110	0.16084	0.000340
0.98348	0.16538	0.000320
0.98566	0.16960	0.000300
0.98764	0.17331	0.000280
0.98944	0.17666	0.000270
0.99105	0.17974	0.000260
0.99250	0.18233	0.000250
0.99379	0.18468	0.000230
0.99495	0.18689	0.000230
0.99597	0.18866	0.000220
0.99687	0.19023	0.000210
0.99767	0.19160	0.000210
0.99837	0.19294	0.000220
0.99899	0.19370	0.000250
0.99953	0.19528	0.000400
1.00000	0.19678	0.000400

WING SECTION 7   Y/BO2 0.814 (Y = 620. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.01748	-0.000880
0.00001	1.01784	0.000160
0.00002	1.01628	0.000400
0.00006	1.01342	0.000650
0.00010	1.00890	0.000910
0.00016	1.00269	0.001180
0.00024	0.99456	0.001460
0.00033	0.98452	0.001740
0.00044	0.97241	0.002030
0.00057	0.95811	0.002310
0.00072	0.94173	0.002600
0.00089	0.92306	0.002890
0.00108	0.90216	0.003170
0.00129	0.87890	0.003450
0.00153	0.85338	0.003720
0.00179	0.82563	0.003990
0.00208	0.79555	0.004250
0.00239	0.76327	0.004490
0.00274	0.72889	0.004720
0.00312	0.69269	0.004930
0.00354	0.65468	0.005120
0.00399	0.61540	0.005280
0.00449	0.57464	0.005380
0.00504	0.53510	0.005490
0.00564	0.49390	0.005490
0.00564	0.49390	0.005600
0.00616	0.45782	0.005550
0.00672	0.42742	0.005520
0.00733	0.39482	0.005510
0.00800	0.36338	0.005460
0.00873	0.33215	0.005420
0.00953	0.30140	0.005390
0.01038	0.27090	0.005370
0.01131	0.24029	0.005350
0.01231	0.20980	0.005360
0.01338	0.17850	0.005390
0.01453	0.14612	0.005430
0.01576	0.11361	0.005450
0.01708	0.08129	0.005470
0.01849	0.04998	0.005460
0.01998	0.02090	0.005420
0.02158	-0.00540	0.005350
0.02327	-0.02843	0.005270
0.02506	-0.04806	0.005190
0.02695	-0.06508	0.005130
0.02894	-0.08021	0.005080
0.03101	-0.09469	0.005060
0.03322	-0.10875	0.005030
0.03562	-0.12177	0.004990
0.03813	-0.13364	0.004950
0.04073	-0.14412	0.004910
0.04344	-0.15343	0.004870
0.04625	-0.16201	0.004840
0.04914	-0.17001	0.004810
0.05213	-0.17767	0.004780
0.05521	-0.18466	0.004750
0.05836	-0.19081	0.004720
0.06159	-0.19572	0.004670
0.06494	-0.19961	0.004630
0.06839	-0.20326	0.004590
0.07190	-0.20738	0.004580
0.07546	-0.21206	0.004560
0.07907	-0.21684	0.004540
0.08270	-0.22170	0.004530
0.08637	-0.22631	0.004510
0.09005	-0.23109	0.004490
0.09375	-0.23570	0.004470
0.09769	-0.24028	0.004460
0.10189	-0.24535	0.004450
0.10634	-0.25060	0.004440
0.11108	-0.25647	0.004430
0.11611	-0.26263	0.004410
0.12144	-0.26913	0.004400
0.12710	-0.27623	0.004400
0.13309	-0.28366	0.004390
0.13943	-0.29148	0.004380
0.14613	-0.29956	0.004370
0.15321	-0.30778	0.004360
0.16068	-0.31596	0.004340
0.16855	-0.32409	0.004320
0.17682	-0.33170	0.004300
0.18568	-0.33914	0.004280
0.19502	-0.34719	0.004270
0.20481	-0.35633	0.004270
0.21505	-0.36797	0.004280
0.22576	-0.38177	0.004300
0.23692	-0.39681	0.004320
0.24856	-0.41207	0.004320
0.26067	-0.42612	0.004320
0.27324	-0.43822	0.004290
0.28625	-0.44727	0.004250
0.29970	-0.45286	0.004200
0.31359	-0.45720	0.004160
0.32789	-0.46218	0.004130
0.34260	-0.46618	0.004080
0.35769	-0.46606	0.004010
0.37314	-0.46040	0.003920
0.38893	-0.45039	0.003820
0.40501	-0.43762	0.003720
0.42136	-0.42370	0.003630
0.43793	-0.40975	0.003550
0.45470	-0.39511	0.003470
0.47159	-0.37963	0.003390
0.48857	-0.36371	0.003310
0.50562	-0.34618	0.003220
0.52269	-0.32332	0.003090
0.53975	-0.29286	0.002910
0.55673	-0.25657	0.002720
0.57362	-0.21765	0.002530
0.59032	-0.17846	0.002360
0.60680	-0.13986	0.002190
0.62305	-0.10186	0.002030
0.63906	-0.06456	0.001880
0.65478	-0.02837	0.001740
0.67018	0.00698	0.001590
0.68527	0.04158	0.001450
0.70003	0.07512	0.001310
0.71440	0.10768	0.001170
0.72837	0.13856	0.001050
0.74193	0.16668	0.000950
0.75507	0.19159	0.000870
0.76780	0.21278	0.000830
0.78012	0.23020	0.000810
0.79199	0.24443	0.000810
0.80342	0.25602	0.000820
0.81440	0.26557	0.000830
0.82494	0.27351	0.000850
0.83503	0.27999	0.000870
0.84469	0.28543	0.000890
0.85394	0.28983	0.000910
0.86277	0.29319	0.000940
0.87118	0.29587	0.000970
0.87917	0.29781	0.001000
0.88677	0.29913	0.001030
0.89398	0.29986	0.001060
0.90081	0.30014	0.001090
0.90728	0.30001	0.001120
0.91340	0.29951	0.001150
0.91919	0.29870	0.001190
0.92465	0.29760	0.001220
0.92981	0.29629	0.001250
0.93467	0.29473	0.001280
0.93926	0.29310	0.001310
0.94358	0.29110	0.001340
0.94764	0.28934	0.001360
0.95146	0.28703	0.001400
0.95528	0.28440	0.001420
0.95905	0.28205	0.001460
0.96273	0.27918	0.001490
0.96629	0.27623	0.001520
0.96969	0.27308	0.001560
0.97291	0.26979	0.001590
0.97594	0.26644	0.001620
0.97876	0.26303	0.001660
0.98137	0.25958	0.001690
0.98376	0.25616	0.001730
0.98594	0.25271	0.001760
0.98791	0.24932	0.001800
0.98969	0.24599	0.001830
0.99129	0.24274	0.001870
0.99272	0.23953	0.001900
0.99398	0.23632	0.001940
0.99511	0.23327	0.001980
0.99610	0.23016	0.002020
0.99698	0.22712	0.002060
0.99775	0.22403	0.002100
0.99843	0.22109	0.002170
0.99902	0.21822	0.002380
0.99954	0.21630	0.003150

WING SECTION 7   Y/BO2 0.814 (Y = 620. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01838	0.001070
0.00000	1.01683	0.000300
0.00002	1.01461	0.000530
0.00004	1.01096	0.000760
0.00007	1.00602	0.000980
0.00012	0.99973	0.001200
0.00017	0.99199	0.001430
0.00024	0.98287	0.001650
0.00032	0.97224	0.001870
0.00041	0.96005	0.002080
0.00053	0.94645	0.002300
0.00065	0.93122	0.002510
0.00079	0.91437	0.002720
0.00095	0.89589	0.002920
0.00114	0.87580	0.003120
0.00134	0.85406	0.003320
0.00156	0.83066	0.003510
0.00181	0.80567	0.003700
0.00208	0.77895	0.003870
0.00238	0.75063	0.004040
0.00271	0.72077	0.004200
0.00307	0.68945	0.004350
0.00346	0.65652	0.004490
0.00389	0.62296	0.004620
0.00437	0.58768	0.004810
0.00482	0.55378	0.004830
0.00532	0.52109	0.004910
0.00586	0.48581	0.005010
0.00646	0.44925	0.005100
0.00712	0.41086	0.005180
0.00783	0.37104	0.005280
0.00861	0.32897	0.005410
0.00946	0.28400	0.005550
0.01037	0.23603	0.005700
0.01136	0.18470	0.005870
0.01243	0.13002	0.006050
0.01358	0.07107	0.006250
0.01483	0.00777	0.006470
0.01616	-0.05983	0.006670
0.01760	-0.13146	0.006870
0.01915	-0.20582	0.007040
0.02081	-0.28135	0.007170
0.02258	-0.35616	0.007240
0.02448	-0.42795	0.007260
0.02646	-0.49349	0.007210
0.02854	-0.55113	0.007120
0.03074	-0.60208	0.007020
0.03306	-0.64763	0.006930
0.03549	-0.68898	0.006860
0.03804	-0.72723	0.006790
0.04070	-0.76256	0.006730
0.04346	-0.79572	0.006690
0.04633	-0.82705	0.006640
0.04929	-0.85616	0.006580
0.05235	-0.88253	0.006510
0.05548	-0.90686	0.006460
0.05872	-0.92974	0.006400
0.06204	-0.95089	0.006350
0.06542	-0.97050	0.006290
0.06887	-0.98828	0.006230
0.07236	-1.00389	0.006170
0.07589	-1.01750	0.006090
0.07945	-1.02869	0.006020
0.08304	-1.03753	0.005950
0.08664	-1.04515	0.005890
0.09034	-1.05177	0.005810
0.09428	-1.05578	0.005730
0.09847	-1.05778	0.005650
0.10294	-1.05845	0.005580
0.10769	-1.05810	0.005510
0.11274	-1.05793	0.005460
0.11810	-1.05761	0.005400
0.12378	-1.05643	0.005340
0.12980	-1.05423	0.005270
0.13618	-1.05139	0.005210
0.14292	-1.04866	0.005160
0.15014	-1.04620	0.005120
0.15776	-1.04372	0.005070
0.16579	-1.04140	0.005020
0.17424	-1.03891	0.004970
0.18313	-1.03645	0.004930
0.19247	-1.03443	0.004890
0.20225	-1.03246	0.004840
0.21250	-1.03037	0.004800
0.22321	-1.02810	0.004760
0.23439	-1.02592	0.004720
0.24604	-1.02315	0.004670
0.25815	-1.01922	0.004630
0.27073	-1.01527	0.004590
0.28379	-1.01194	0.004550
0.29732	-1.00912	0.004520
0.31129	-1.00455	0.004450
0.32569	-0.99596	0.004330
0.34049	-0.97644	0.003980
0.35567	-0.91127	0.002980
0.37121	-0.76496	0.001860
0.38708	-0.59494	0.001630
0.40325	-0.49307	0.001990
0.41968	-0.46529	0.002380
0.43635	-0.47309	0.002730
0.45321	-0.48811	0.002970
0.47022	-0.49908	0.003110
0.48735	-0.50667	0.003210
0.50456	-0.51159	0.003260
0.52180	-0.51342	0.003300
0.53903	-0.51367	0.003320
0.55620	-0.51179	0.003320
0.57328	-0.50825	0.003310
0.59022	-0.50314	0.003290
0.60698	-0.49472	0.003250
0.62353	-0.48438	0.003200
0.63982	-0.47221	0.003150
0.65583	-0.45777	0.003080
0.67152	-0.44005	0.002980
0.68686	-0.41811	0.002870
0.70183	-0.39342	0.002750
0.71639	-0.36728	0.002620
0.73054	-0.34048	0.002510
0.74426	-0.31409	0.002390
0.75753	-0.28770	0.002280
0.77036	-0.26134	0.002170
0.78273	-0.23590	0.002070
0.79463	-0.21149	0.001970
0.80607	-0.18781	0.001870
0.81704	-0.16493	0.001780
0.82755	-0.14365	0.001700
0.83760	-0.12319	0.001620
0.84720	-0.10348	0.001550
0.85635	-0.08519	0.001480
0.86507	-0.06781	0.001410
0.87337	-0.05121	0.001350
0.88126	-0.03547	0.001280
0.88874	-0.02061	0.001230
0.89584	-0.00650	0.001170
0.90257	0.00701	0.001120
0.90893	0.01952	0.001060
0.91495	0.03148	0.001010
0.92063	0.04289	0.000970
0.92600	0.05368	0.000920
0.93106	0.06380	0.000880
0.93583	0.07322	0.000830
0.94032	0.08254	0.000790
0.94455	0.09090	0.000760
0.94853	0.09922	0.000720
0.95228	0.10660	0.000690
0.95600	0.11375	0.000650
0.95968	0.12150	0.000610
0.96329	0.12862	0.000580
0.96678	0.13567	0.000550
0.97013	0.14236	0.000520
0.97330	0.14859	0.000490
0.97629	0.15453	0.000460
0.97907	0.16029	0.000430
0.98165	0.16537	0.000410
0.98401	0.16988	0.000390
0.98616	0.17435	0.000360
0.98812	0.17809	0.000350
0.98987	0.18150	0.000330
0.99145	0.18479	0.000310
0.99286	0.18726	0.000300
0.99410	0.18979	0.000290
0.99521	0.19209	0.000280
0.99619	0.19378	0.000280
0.99705	0.19536	0.000270
0.99781	0.19673	0.000260
0.99847	0.19807	0.000270
0.99905	0.19890	0.000300
0.99956	0.20055	0.000480
1.00000	0.20214	0.000480

WING SECTION 8   Y/BO2 0.945 (Y = 720. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	0.99524	-0.001310
0.00000	0.99360	0.000480
0.00002	0.99109	0.000710
0.00004	0.98746	0.000950
0.00007	0.98270	0.001190
0.00010	0.97667	0.001430
0.00015	0.96934	0.001670
0.00021	0.96077	0.001920
0.00028	0.95068	0.002180
0.00037	0.93892	0.002430
0.00047	0.92574	0.002690
0.00058	0.91050	0.002950
0.00071	0.89347	0.003220
0.00086	0.87440	0.003490
0.00103	0.85283	0.003770
0.00122	0.82917	0.004050
0.00143	0.80276	0.004340
0.00167	0.77341	0.004620
0.00194	0.74114	0.004890
0.00225	0.70588	0.005160
0.00259	0.66737	0.005420
0.00299	0.62580	0.005660
0.00343	0.58040	0.005860
0.00393	0.53489	0.006050
0.00450	0.48550	0.006050
0.00450	0.48550	0.006320
0.00495	0.44219	0.006270
0.00545	0.40679	0.006270
0.00600	0.36828	0.006290
0.00661	0.33072	0.006260
0.00727	0.29340	0.006220
0.00799	0.25711	0.006140
0.00877	0.22211	0.006060
0.00962	0.18807	0.006000
0.01053	0.15446	0.005970
0.01152	0.12104	0.005940
0.01257	0.08732	0.005950
0.01371	0.05299	0.005970
0.01492	0.01824	0.006000
0.01621	-0.01654	0.006010
0.01758	-0.05166	0.006010
0.01905	-0.08452	0.005960
0.02060	-0.11409	0.005890
0.02225	-0.14087	0.005790
0.02399	-0.16330	0.005670
0.02582	-0.18188	0.005570
0.02773	-0.19761	0.005490
0.02977	-0.21191	0.005440
0.03203	-0.22651	0.005410
0.03439	-0.24053	0.005350
0.03685	-0.25228	0.005300
0.03941	-0.26260	0.005250
0.04206	-0.27194	0.005210
0.04480	-0.27994	0.005160
0.04763	-0.28712	0.005120
0.05054	-0.29376	0.005080
0.05354	-0.29997	0.005040
0.05661	-0.30558	0.005000
0.05983	-0.31016	0.004950
0.06316	-0.31321	0.004890
0.06656	-0.31489	0.004840
0.07002	-0.31719	0.004820
0.07352	-0.32059	0.004800
0.07708	-0.32410	0.004770
0.08067	-0.32754	0.004750
0.08429	-0.33108	0.004720
0.08794	-0.33427	0.004690
0.09183	-0.33733	0.004680
0.09596	-0.34111	0.004660
0.10036	-0.34458	0.004630
0.10504	-0.34841	0.004610
0.11001	-0.35257	0.004600
0.11528	-0.35710	0.004580
0.12088	-0.36218	0.004560
0.12680	-0.36713	0.004540
0.13308	-0.37223	0.004520
0.13971	-0.37782	0.004500
0.14672	-0.38330	0.004480
0.15413	-0.38847	0.004450
0.16193	-0.39374	0.004420
0.17012	-0.39800	0.004390
0.17896	-0.40171	0.004360
0.18829	-0.40530	0.004320
0.19807	-0.40856	0.004300
0.20831	-0.41370	0.004290
0.21901	-0.42158	0.004300
0.23019	-0.43075	0.004310
0.24183	-0.44053	0.004310
0.25395	-0.44955	0.004300
0.26655	-0.45662	0.004270
0.27958	-0.46085	0.004220
0.29306	-0.46142	0.004150
0.30698	-0.45939	0.004090
0.32133	-0.45757	0.004050
0.33608	-0.45615	0.004010
0.35123	-0.45236	0.003940
0.36675	-0.44423	0.003850
0.38261	-0.43216	0.003760
0.39878	-0.41789	0.003670
0.41522	-0.40260	0.003580
0.43189	-0.38762	0.003510
0.44878	-0.37299	0.003440
0.46578	-0.35838	0.003380
0.48288	-0.34376	0.003320
0.50005	-0.32871	0.003250
0.51725	-0.31065	0.003150
0.53445	-0.28591	0.003000
0.55159	-0.25467	0.002830
0.56864	-0.21991	0.002650
0.58549	-0.18403	0.002480
0.60212	-0.14847	0.002320
0.61853	-0.11361	0.002160
0.63469	-0.07898	0.002010
0.65057	-0.04506	0.001870
0.66612	-0.01191	0.001730
0.68139	0.02076	0.001590
0.69632	0.05262	0.001450
0.71088	0.08382	0.001310
0.72503	0.11385	0.001180
0.73876	0.14165	0.001060
0.75207	0.16651	0.000980
0.76499	0.18770	0.000930
0.77748	0.20513	0.000900
0.78953	0.21925	0.000900
0.80113	0.23059	0.000900
0.81229	0.23985	0.000910
0.82300	0.24745	0.000930
0.83325	0.25362	0.000950
0.84307	0.25879	0.000970
0.85249	0.26292	0.001000
0.86149	0.26610	0.001020
0.87005	0.26859	0.001050
0.87820	0.27039	0.001080
0.88595	0.27162	0.001110
0.89330	0.27234	0.001140
0.90027	0.27262	0.001170
0.90687	0.27251	0.001200
0.91312	0.27206	0.001230
0.91903	0.27133	0.001260
0.92461	0.27037	0.001290
0.92988	0.26925	0.001320
0.93485	0.26785	0.001340
0.93953	0.26642	0.001370
0.94394	0.26462	0.001400
0.94810	0.26311	0.001430
0.95200	0.26104	0.001460
0.95591	0.25862	0.001480
0.95976	0.25664	0.001510
0.96350	0.25409	0.001540
0.96710	0.25150	0.001570
0.97053	0.24880	0.001600
0.97377	0.24601	0.001630
0.97680	0.24301	0.001660
0.97960	0.24010	0.001690
0.98218	0.23727	0.001730
0.98453	0.23427	0.001760
0.98666	0.23132	0.001790
0.98858	0.22853	0.001820
0.99031	0.22568	0.001850
0.99184	0.22304	0.001880
0.99321	0.22048	0.001920
0.99441	0.21757	0.001950
0.99548	0.21517	0.001990
0.99641	0.21251	0.002030
0.99723	0.20992	0.002070
0.99795	0.20745	0.002110
0.99857	0.20476	0.002190
0.99911	0.20252	0.002380
0.99959	0.20124	0.003180

WING SECTION 8   Y/BO2 0.945 (Y = 720. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	0.99457	0.001470
0.00000	0.99562	-0.000080
0.00001	0.99568	0.000120
0.00003	0.99470	0.000320
0.00005	0.99289	0.000520
0.00008	0.99011	0.000720
0.00011	0.98633	0.000930
0.00016	0.98159	0.001130
0.00021	0.97562	0.001340
0.00028	0.96855	0.001550
0.00036	0.96023	0.001760
0.00045	0.95063	0.001970
0.00055	0.93961	0.002170
0.00067	0.92710	0.002380
0.00080	0.91321	0.002590
0.00095	0.89749	0.002810
0.00112	0.88006	0.003010
0.00132	0.86087	0.003220
0.00153	0.83975	0.003420
0.00177	0.81661	0.003620
0.00205	0.79147	0.003820
0.00235	0.76409	0.004010
0.00269	0.73432	0.004180
0.00308	0.70349	0.004360
0.00351	0.66975	0.004630
0.00390	0.63760	0.004660
0.00434	0.60706	0.004760
0.00482	0.57350	0.004880
0.00535	0.53890	0.004980
0.00594	0.50261	0.005080
0.00657	0.46488	0.005180
0.00727	0.42514	0.005290
0.00802	0.38408	0.005400
0.00884	0.34066	0.005540
0.00973	0.29392	0.005700
0.01069	0.24436	0.005870
0.01173	0.19095	0.006050
0.01285	0.13463	0.006240
0.01405	0.07368	0.006460
0.01534	0.00830	0.006670
0.01673	-0.06021	0.006870
0.01822	-0.13258	0.007070
0.01982	-0.20689	0.007220
0.02153	-0.28147	0.007310
0.02331	-0.35217	0.007330
0.02517	-0.41679	0.007290
0.02715	-0.47587	0.007210
0.02925	-0.52855	0.007100
0.03145	-0.57532	0.007000
0.03377	-0.61771	0.006940
0.03620	-0.65749	0.006890
0.03874	-0.69497	0.006840
0.04138	-0.73002	0.006790
0.04412	-0.76308	0.006740
0.04696	-0.79389	0.006690
0.04988	-0.82202	0.006620
0.05292	-0.84739	0.006550
0.05604	-0.87099	0.006500
0.05924	-0.89392	0.006450
0.06251	-0.91503	0.006400
0.06583	-0.93455	0.006350
0.06922	-0.95247	0.006280
0.07265	-0.96792	0.006220
0.07612	-0.98132	0.006150
0.07962	-0.99273	0.006070
0.08324	-1.00204	0.006000
0.08711	-1.01053	0.005930
0.09123	-1.01629	0.005830
0.09563	-1.01932	0.005750
0.10030	-1.02148	0.005670
0.10528	-1.02188	0.005590
0.11056	-1.02175	0.005530
0.11617	-1.02159	0.005470
0.12211	-1.02039	0.005400
0.12842	-1.01841	0.005330
0.13507	-1.01570	0.005270
0.14223	-1.01234	0.005210
0.14980	-1.00894	0.005150
0.15778	-1.00552	0.005090
0.16619	-1.00120	0.005020
0.17503	-0.99455	0.004910
0.18432	-0.98211	0.004700
0.19407	-0.95185	0.004170
0.20428	-0.88114	0.003290
0.21496	-0.76536	0.002680
0.22611	-0.64354	0.002660
0.23774	-0.56049	0.002900
0.24984	-0.52190	0.003170
0.26240	-0.50955	0.003380
0.27545	-0.50835	0.003530
0.28900	-0.50917	0.003620
0.30300	-0.50813	0.003660
0.31743	-0.50380	0.003660
0.33228	-0.49835	0.003670
0.34751	-0.49314	0.003670
0.36311	-0.48711	0.003660
0.37904	-0.48043	0.003640
0.39529	-0.47336	0.003620
0.41181	-0.46648	0.003600
0.42858	-0.45989	0.003570
0.44555	-0.45295	0.003540
0.46269	-0.44594	0.003520
0.47995	-0.43955	0.003490
0.49730	-0.43300	0.003470
0.51470	-0.42696	0.003450
0.53209	-0.42134	0.003430
0.54944	-0.41620	0.003410
0.56670	-0.41125	0.003390
0.58384	-0.40580	0.003360
0.60080	-0.39995	0.003330
0.61755	-0.39218	0.003280
0.63406	-0.38313	0.003240
0.65029	-0.37344	0.003190
0.66621	-0.36164	0.003110
0.68179	-0.34606	0.003020
0.69699	-0.32724	0.002910
0.71179	-0.30687	0.002810
0.72618	-0.28566	0.002700
0.74013	-0.26438	0.002600
0.75364	-0.24279	0.002490
0.76670	-0.22091	0.002390
0.77931	-0.19979	0.002300
0.79144	-0.17938	0.002210
0.80310	-0.15977	0.002130
0.81429	-0.14099	0.002040
0.82501	-0.12271	0.001970
0.83527	-0.10555	0.001900
0.84506	-0.08925	0.001830
0.85441	-0.07348	0.001760
0.86333	-0.05870	0.001700
0.87181	-0.04468	0.001640
0.87987	-0.03132	0.001590
0.88752	-0.01862	0.001530
0.89478	-0.00652	0.001480
0.90166	0.00512	0.001430
0.90817	0.01595	0.001380
0.91432	0.02653	0.001330
0.92014	0.03668	0.001290
0.92564	0.04627	0.001240
0.93082	0.05543	0.001200
0.93571	0.06406	0.001150
0.94031	0.07264	0.001110
0.94464	0.08032	0.001070
0.94872	0.08815	0.001040
0.95256	0.09503	0.001010
0.95637	0.10182	0.000960
0.96013	0.10937	0.000920
0.96381	0.11623	0.000890
0.96735	0.12312	0.000850
0.97074	0.12965	0.000820
0.97395	0.13592	0.000790
0.97695	0.14166	0.000750
0.97974	0.14711	0.000720
0.98230	0.15250	0.000690
0.98464	0.15694	0.000670
0.98676	0.16127	0.000640
0.98867	0.16512	0.000620
0.99038	0.16861	0.000600
0.99191	0.17173	0.000590
0.99326	0.17433	0.000570
0.99445	0.17703	0.000560
0.99550	0.17903	0.000550	
0.99643	0.18078	0.000540	
0.99724	0.18238	0.000530	
0.99794	0.18376	0.000520	
0.99856	0.18510	0.000540	
0.99909	0.18588	0.000590	
0.99955	0.18754	0.000870	
0.99996	0.18920	0.000870	


DPW-W2			

GRID_SIZE	MACH	ALPHA	CL_TOT
14811489	0.76000	0.500000	0.50049

WING SECTION 1   Y/BO2 0.026 (Y =  20. mm) UPPER SURFACE			
XOC	CP	CFprime
0.00000	1.06890	-0.000590
0.00001	1.06818	0.000190
0.00005	1.06502	0.000440
0.00010	1.05888	0.000700
0.00019	1.04999	0.000950
0.00030	1.03834	0.001190
0.00043	1.02398	0.001420
0.00060	1.00698	0.001650
0.00079	0.98758	0.001870
0.00101	0.96576	0.002080
0.00126	0.94185	0.002270
0.00155	0.91605	0.002460
0.00186	0.88840	0.002640
0.00220	0.85934	0.002800
0.00257	0.82907	0.002950
0.00297	0.79771	0.003090
0.00339	0.76605	0.003220
0.00385	0.73371	0.003340
0.00433	0.70119	0.003440
0.00483	0.66924	0.003540
0.00536	0.63732	0.003630
0.00591	0.60566	0.003720
0.00648	0.57427	0.003810
0.00707	0.54324	0.003910
0.00767	0.51191	0.004030
0.00767	0.51191	0.003910
0.00829	0.48094	0.004070
0.00897	0.44898	0.004170
0.00970	0.41436	0.004280
0.01051	0.37735	0.004410
0.01138	0.33714	0.004560
0.01233	0.29398	0.004710
0.01336	0.24755	0.004870
0.01448	0.19720	0.005050
0.01569	0.14291	0.005230
0.01700	0.08472	0.005410
0.01842	0.02347	0.005580
0.01996	-0.04024	0.005740
0.02161	-0.10539	0.005870
0.02340	-0.17006	0.005970
0.02531	-0.23281	0.006030
0.02737	-0.29178	0.006050
0.02956	-0.34581	0.006050
0.03190	-0.39468	0.006030
0.03438	-0.43802	0.005980
0.03699	-0.47653	0.005930
0.03975	-0.51118	0.005880
0.04264	-0.54304	0.005840
0.04566	-0.57339	0.005800
0.04881	-0.60258	0.005770
0.05209	-0.63083	0.005740
0.05547	-0.65694	0.005700
0.05897	-0.68063	0.005650
0.06256	-0.70213	0.005600
0.06625	-0.72180	0.005560
0.07001	-0.74019	0.005500
0.07385	-0.75576	0.005430
0.07774	-0.76740	0.005350
0.08168	-0.77560	0.005260
0.08565	-0.78174	0.005180
0.08964	-0.78538	0.005100
0.09364	-0.78573	0.004990
0.09763	-0.78348	0.004890
0.10161	-0.78066	0.004830
0.10555	-0.77949	0.004790
0.10946	-0.78186	0.004790
0.11337	-0.78688	0.004790
0.11752	-0.79307	0.004780
0.12194	-0.79963	0.004770
0.12663	-0.80617	0.004760
0.13161	-0.81406	0.004750
0.13690	-0.82270	0.004740
0.14250	-0.83161	0.004730
0.14843	-0.84146	0.004720
0.15470	-0.85205	0.004710
0.16133	-0.86328	0.004690
0.16833	-0.87344	0.004660
0.17571	-0.88317	0.004640
0.18349	-0.89782	0.004660
0.19168	-0.91364	0.004630
0.20028	-0.92046	0.004540
0.20931	-0.92197	0.004470
0.21877	-0.92256	0.004400
0.22868	-0.92043	0.004320
0.23903	-0.91637	0.004250
0.24983	-0.90975	0.004170
0.26108	-0.90157	0.004100
0.27278	-0.89426	0.004050
0.28493	-0.89000	0.004030
0.29752	-0.88910	0.004020
0.31055	-0.88681	0.003970
0.32400	-0.87787	0.003890
0.33786	-0.86280	0.003800
0.35212	-0.84601	0.003720
0.36675	-0.83084	0.003670
0.38173	-0.81897	0.003650
0.39704	-0.81155	0.003650
0.41264	-0.80823	0.003660
0.42852	-0.80696	0.003670
0.44462	-0.80506	0.003650
0.46092	-0.80067	0.003620
0.47737	-0.79428	0.003590
0.49395	-0.78846	0.003580
0.51060	-0.78891	0.003620
0.52729	-0.79727	0.003630
0.54397	-0.79905	0.003530
0.56060	-0.76830	0.003180
0.57714	-0.68185	0.002600
0.59356	-0.57590	0.002190
0.60981	-0.50112	0.002090
0.62586	-0.45495	0.002090
0.64169	-0.42608	0.002130
0.65726	-0.40709	0.002170
0.67254	-0.39317	0.002230
0.68750	-0.38224	0.002260
0.70211	-0.37067	0.002260
0.71634	-0.35485	0.002230
0.73018	-0.33727	0.002190
0.74361	-0.32233	0.002180
0.75663	-0.31066	0.002190
0.76921	-0.30173	0.002200
0.78136	-0.29487	0.002220
0.79306	-0.28879	0.002230
0.80430	-0.28245	0.002230
0.81510	-0.27517	0.002220
0.82543	-0.26600	0.002190
0.83532	-0.25464	0.002140
0.84476	-0.24111	0.002080
0.85377	-0.22548	0.002000
0.86234	-0.20818	0.001910
0.87049	-0.18970	0.001820
0.87823	-0.17062	0.001730
0.88557	-0.15132	0.001640
0.89253	-0.13219	0.001550
0.89912	-0.11383	0.001470
0.90536	-0.09638	0.001390
0.91126	-0.07988	0.001320
0.91683	-0.06410	0.001250
0.92208	-0.04876	0.001180
0.92704	-0.03403	0.001110
0.93171	-0.01993	0.001050
0.93610	-0.00652	0.000990
0.94024	0.00624	0.000930
0.94413	0.01835	0.000870
0.94779	0.02976	0.000820
0.95122	0.04064	0.000770
0.95466	0.05123	0.000720
0.95808	0.06178	0.000670
0.96146	0.07218	0.000620
0.96477	0.08226	0.000570
0.96798	0.09205	0.000530
0.97107	0.10133	0.000490
0.97402	0.11010	0.000450
0.97681	0.11821	0.000410
0.97943	0.12576	0.000380
0.98187	0.13277	0.000350
0.98414	0.13902	0.000320
0.98622	0.14476	0.000300
0.98813	0.14987	0.000280
0.98987	0.15441	0.000260
0.99145	0.15849	0.000250
0.99288	0.16195	0.000240
0.99416	0.16503	0.000230
0.99531	0.16767	0.000230
0.99634	0.16980	0.000230
0.99726	0.17155	0.000240
0.99807	0.17316	0.000270
0.99879	0.17402	0.000360
0.99943	0.17639	0.000650

WING SECTION 1   Y/BO2 0.026 (Y =  20. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.06840	0.000800
0.00002	1.06649	0.000360
0.00006	1.06073	0.000660
0.00014	1.05110	0.000980
0.00025	1.03749	0.001290
0.00041	1.02010	0.001600
0.00060	0.99894	0.001900
0.00082	0.97390	0.002210
0.00109	0.94510	0.002500
0.00139	0.91314	0.002780
0.00174	0.87822	0.003040
0.00212	0.84085	0.003280
0.00253	0.80160	0.003490
0.00298	0.76115	0.003680
0.00347	0.71999	0.003840
0.00399	0.67879	0.003980
0.00454	0.63850	0.004090
0.00511	0.59923	0.004170
0.00571	0.56227	0.004210
0.00634	0.52798	0.004230
0.00698	0.49599	0.004230
0.00763	0.46763	0.004210
0.00830	0.44156	0.004220
0.00898	0.41731	0.004230
0.00966	0.39424	0.004230
0.01036	0.37339	0.004210
0.01111	0.35312	0.004230
0.01192	0.33109	0.004260
0.01281	0.30949	0.004290
0.01376	0.28716	0.004320
0.01479	0.26489	0.004350
0.01591	0.24211	0.004380
0.01710	0.21910	0.004400
0.01839	0.19733	0.004410
0.01977	0.17679	0.004390
0.02124	0.15870	0.004360
0.02283	0.14298	0.004320
0.02451	0.12953	0.004270
0.02631	0.11820	0.004220
0.02822	0.10859	0.004180
0.03025	0.09978	0.004150
0.03240	0.09100	0.004120
0.03466	0.08355	0.004080
0.03704	0.07715	0.004040
0.03955	0.07160	0.004000
0.04218	0.06694	0.003960
0.04493	0.06259	0.003930
0.04779	0.05876	0.003890
0.05078	0.05528	0.003850
0.05388	0.05211	0.003820
0.05708	0.04932	0.003780
0.06040	0.04735	0.003740
0.06381	0.04609	0.003700
0.06731	0.04490	0.003660
0.07090	0.04310	0.003640
0.07457	0.04053	0.003620
0.07830	0.03764	0.003610
0.08208	0.03454	0.003590
0.08592	0.03126	0.003580
0.08979	0.02788	0.003560
0.09368	0.02449	0.003550
0.09758	0.02118	0.003540
0.10149	0.01798	0.003520
0.10538	0.01503	0.003510
0.10926	0.01179	0.003500
0.11313	0.00842	0.003490
0.11725	0.00494	0.003480
0.12163	0.00076	0.003480
0.12627	-0.00402	0.003480
0.13120	-0.00947	0.003480
0.13643	-0.01575	0.003490
0.14197	-0.02295	0.003500
0.14782	-0.03109	0.003510
0.15402	-0.04035	0.003520
0.16057	-0.05078	0.003540
0.16748	-0.06266	0.003570
0.17477	-0.07619	0.003600
0.18244	-0.09084	0.003620
0.19052	-0.10546	0.003640
0.19901	-0.11984	0.003650
0.20793	-0.13654	0.003690
0.21727	-0.15659	0.003740
0.22705	-0.17894	0.003790
0.23729	-0.20263	0.003830
0.24797	-0.22614	0.003860
0.25910	-0.24827	0.003880
0.27070	-0.26818	0.003870
0.28274	-0.28537	0.003860
0.29524	-0.30122	0.003850
0.30817	-0.31928	0.003870
0.32152	-0.34061	0.003900
0.33530	-0.36131	0.003900
0.34947	-0.37669	0.003860
0.36403	-0.38414	0.003790
0.37894	-0.38344	0.003690
0.39417	-0.37666	0.003580
0.40971	-0.36689	0.003490
0.42552	-0.35728	0.003420
0.44156	-0.34983	0.003370
0.45781	-0.34550	0.003340
0.47421	-0.34484	0.003340
0.49074	-0.34713	0.003330
0.50735	-0.34602	0.003290
0.52401	-0.33666	0.003200
0.54066	-0.32294	0.003120
0.55727	-0.30853	0.003050
0.57380	-0.29402	0.002980
0.59021	-0.27899	0.002910
0.60645	-0.26118	0.002820
0.62248	-0.23757	0.002690
0.63827	-0.20666	0.002530
0.65379	-0.16890	0.002330
0.66899	-0.12554	0.002110
0.68386	-0.07905	0.001900
0.69837	-0.03249	0.001700
0.71251	0.01145	0.001510
0.72626	0.05343	0.001340
0.73961	0.09401	0.001170
0.75254	0.13195	0.001020
0.76506	0.16612	0.000910
0.77715	0.19566	0.000820
0.78882	0.22114	0.000760
0.80006	0.24302	0.000720
0.81087	0.26182	0.000690
0.82125	0.27791	0.000670
0.83120	0.29163	0.000660
0.84073	0.30310	0.000670
0.84983	0.31256	0.000680
0.85852	0.32020	0.000700
0.86680	0.32619	0.000720
0.87468	0.33076	0.000750
0.88217	0.33407	0.000780
0.88928	0.33629	0.000820
0.89602	0.33772	0.000850
0.90240	0.33861	0.000880
0.90845	0.33904	0.000920
0.91416	0.33906	0.000950
0.91955	0.33856	0.000980
0.92464	0.33756	0.001020
0.92944	0.33615	0.001050
0.93397	0.33440	0.001090
0.93823	0.33231	0.001120
0.94223	0.32987	0.001160
0.94601	0.32731	0.001200
0.94955	0.32443	0.001230
0.95309	0.32121	0.001270
0.95662	0.31776	0.001300
0.96011	0.31397	0.001340
0.96352	0.30988	0.001380
0.96683	0.30544	0.001430
0.97002	0.30088	0.001470
0.97305	0.29608	0.001510
0.97593	0.29116	0.001550
0.97862	0.28613	0.001600
0.98114	0.28094	0.001640
0.98347	0.27580	0.001680
0.98562	0.27060	0.001730
0.98759	0.26537	0.001770
0.98939	0.26010	0.001820
0.99101	0.25481	0.001860
0.99248	0.24948	0.001910
0.99380	0.24431	0.001960
0.99499	0.23880	0.002020
0.99605	0.23323	0.002080
0.99700	0.22728	0.002140
0.99784	0.22143	0.002250
0.99859	0.21506	0.002510
0.99925	0.21091	0.003430
0.99983	0.21069	0.003430

WING SECTION 2   Y/BO2 0.157 (Y = 120. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.02233	-0.000200
0.00001	1.01861	0.000890
0.00005	1.00901	0.001150
0.00011	0.99618	0.001410
0.00019	0.98067	0.001670
0.00030	0.96226	0.001920
0.00043	0.94103	0.002170
0.00060	0.91714	0.002400
0.00079	0.89079	0.002630
0.00101	0.86203	0.002860
0.00126	0.83090	0.003070
0.00154	0.79784	0.003270
0.00185	0.76304	0.003470
0.00219	0.72666	0.003650
0.00256	0.68910	0.003820
0.00296	0.65071	0.003970
0.00339	0.61189	0.004110
0.00385	0.57287	0.004230
0.00433	0.53428	0.004330
0.00484	0.49612	0.004430
0.00538	0.45835	0.004530
0.00593	0.42121	0.004620
0.00651	0.38464	0.004710
0.00710	0.34887	0.004810
0.00771	0.31250	0.004930
0.00771	0.31250	0.004810
0.00833	0.27741	0.004970
0.00901	0.24171	0.005070
0.00975	0.20251	0.005190
0.01055	0.16087	0.005330
0.01142	0.11545	0.005480
0.01237	0.06677	0.005630
0.01340	0.01435	0.005800
0.01452	-0.04270	0.005980
0.01573	-0.10429	0.006170
0.01704	-0.17067	0.006350
0.01846	-0.24066	0.006520
0.01999	-0.31379	0.006680
0.02164	-0.38918	0.006800
0.02342	-0.46424	0.006880
0.02533	-0.53759	0.006910
0.02738	-0.60649	0.006890
0.02957	-0.66934	0.006840
0.03190	-0.72592	0.006760
0.03436	-0.77560	0.006670
0.03697	-0.81867	0.006570
0.03971	-0.85627	0.006460
0.04259	-0.88905	0.006370
0.04560	-0.91910	0.006290
0.04873	-0.94740	0.006210
0.05198	-0.97324	0.006140
0.05535	-0.99780	0.006080
0.05882	-1.02028	0.006010
0.06239	-1.04025	0.005940
0.06605	-1.05866	0.005870
0.06980	-1.07524	0.005810
0.07361	-1.08958	0.005740
0.07748	-1.10145	0.005660
0.08140	-1.11063	0.005580
0.08535	-1.11763	0.005510
0.08933	-1.12259	0.005430
0.09331	-1.12535	0.005350
0.09730	-1.12607	0.005280
0.10126	-1.12501	0.005200
0.10521	-1.12283	0.005140
0.10911	-1.12076	0.005090
0.11302	-1.11872	0.005040
0.11717	-1.11579	0.004990
0.12159	-1.11195	0.004930
0.12627	-1.10682	0.004870
0.13125	-1.10083	0.004810
0.13652	-1.09423	0.004760
0.14210	-1.08672	0.004700
0.14801	-1.07866	0.004650
0.15427	-1.06994	0.004600
0.16087	-1.06011	0.004540
0.16785	-1.04846	0.004470
0.17520	-1.03506	0.004430
0.18295	-1.02453	0.004390
0.19110	-1.01636	0.004330
0.19968	-1.00381	0.004250
0.20867	-0.99009	0.004180
0.21811	-0.97990	0.004150
0.22798	-0.97293	0.004130
0.23831	-0.96911	0.004140
0.24908	-0.96761	0.004140
0.26030	-0.96778	0.004160
0.27198	-0.96912	0.004180
0.28411	-0.97101	0.004180
0.29668	-0.97178	0.004170
0.30969	-0.96848	0.004120
0.32312	-0.95911	0.004050
0.33697	-0.94326	0.003960
0.35121	-0.92210	0.003850
0.36582	-0.89827	0.003730
0.38079	-0.87481	0.003630
0.39609	-0.85326	0.003550
0.41168	-0.83295	0.003470
0.42755	-0.81590	0.003450
0.44365	-0.80752	0.003490
0.45995	-0.80955	0.003560
0.47640	-0.81682	0.003620
0.49297	-0.82104	0.003610
0.50962	-0.81450	0.003490
0.52631	-0.78096	0.003150
0.54299	-0.69510	0.002590
0.55962	-0.59269	0.002220
0.57615	-0.52069	0.002110
0.59255	-0.47093	0.002040
0.60879	-0.43096	0.001970
0.62484	-0.39564	0.001920
0.64066	-0.36678	0.001910
0.65622	-0.34460	0.001930
0.67150	-0.32781	0.001970
0.68647	-0.31552	0.002000
0.70109	-0.30375	0.002010
0.71534	-0.28827	0.001980
0.72920	-0.27103	0.001950
0.74266	-0.25622	0.001940
0.75570	-0.24462	0.001950
0.76832	-0.23576	0.001970
0.78050	-0.22915	0.002000
0.79224	-0.22337	0.002010
0.80352	-0.21764	0.002020
0.81436	-0.21141	0.002020
0.82474	-0.20350	0.002000
0.83467	-0.19361	0.001960
0.84416	-0.18171	0.001910
0.85320	-0.16786	0.001840
0.86182	-0.15250	0.001770
0.87001	-0.13602	0.001690
0.87779	-0.11885	0.001600
0.88518	-0.10146	0.001520
0.89218	-0.08423	0.001440
0.89882	-0.06770	0.001360
0.90509	-0.05204	0.001290
0.91103	-0.03731	0.001230
0.91664	-0.02326	0.001170
0.92193	-0.00962	0.001100
0.92692	0.00343	0.001040
0.93162	0.01592	0.000980
0.93605	0.02777	0.000930
0.94022	0.03904	0.000870
0.94414	0.04966	0.000820
0.94783	0.05977	0.000780
0.95129	0.06926	0.000730
0.95476	0.07848	0.000690
0.95822	0.08782	0.000650
0.96162	0.09694	0.000600
0.96496	0.10577	0.000560
0.96818	0.11431	0.000520
0.97128	0.12243	0.000490
0.97424	0.13008	0.000450
0.97703	0.13716	0.000420
0.97965	0.14372	0.000390
0.98208	0.14982	0.000360
0.98434	0.15525	0.000340
0.98641	0.16024	0.000320
0.98831	0.16468	0.000300
0.99003	0.16862	0.000290
0.99159	0.17215	0.000270
0.99300	0.17513	0.000270
0.99427	0.17779	0.000260
0.99540	0.18003	0.000260
0.99641	0.18183	0.000260
0.99731	0.18328	0.000270
0.99811	0.18462	0.000310
0.99882	0.18524	0.000390
0.99945	0.18733	0.000700

WING SECTION 2   Y/BO2 0.157 (Y = 120. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.02987	0.000410
0.00001	1.03139	-0.000350
0.00006	1.03288	-0.000030
0.00014	1.03093	0.000290
0.00025	1.02511	0.000620
0.00041	1.01540	0.000950
0.00060	1.00182	0.001280
0.00083	0.98428	0.001590
0.00109	0.96312	0.001900
0.00140	0.93854	0.002190
0.00174	0.91080	0.002460
0.00212	0.88051	0.002710
0.00253	0.84800	0.002940
0.00298	0.81382	0.003150
0.00347	0.77865	0.003330
0.00398	0.74275	0.003490
0.00452	0.70700	0.003620
0.00509	0.67192	0.003720
0.00569	0.63792	0.003790
0.00630	0.60578	0.003840
0.00694	0.57526	0.003860
0.00759	0.54733	0.003880
0.00825	0.52115	0.003910
0.00892	0.49623	0.003930
0.00960	0.47259	0.003930
0.01030	0.45034	0.003960
0.01105	0.42809	0.004000
0.01186	0.40450	0.004040
0.01274	0.38079	0.004080
0.01369	0.35618	0.004130
0.01471	0.33120	0.004180
0.01581	0.30540	0.004230
0.01699	0.27918	0.004280
0.01826	0.25359	0.004300
0.01963	0.22877	0.004320
0.02109	0.20552	0.004310
0.02265	0.18424	0.004300
0.02431	0.16480	0.004280
0.02609	0.14686	0.004270
0.02797	0.13038	0.004250
0.02997	0.11470	0.004250
0.03208	0.09933	0.004250
0.03431	0.08442	0.004240
0.03666	0.07078	0.004220
0.03912	0.05804	0.004210
0.04171	0.04572	0.004190
0.04441	0.03435	0.004180
0.04723	0.02342	0.004170
0.05017	0.01284	0.004160
0.05322	0.00274	0.004140
0.05638	-0.00668	0.004130
0.05964	-0.01527	0.004100
0.06300	-0.02291	0.004080
0.06646	-0.02969	0.004050
0.07000	-0.03699	0.004050
0.07361	-0.04486	0.004040
0.07729	-0.05239	0.004020
0.08104	-0.05988	0.004010
0.08483	-0.06736	0.004010
0.08866	-0.07468	0.004000
0.09252	-0.08181	0.003990
0.09639	-0.08878	0.003980
0.10028	-0.09567	0.003970
0.10415	-0.10236	0.003970
0.10801	-0.10950	0.003970
0.11187	-0.11673	0.003960
0.11597	-0.12399	0.003960
0.12034	-0.13199	0.003960
0.12498	-0.14022	0.003960
0.12989	-0.14879	0.003960
0.13511	-0.15783	0.003960
0.14064	-0.16736	0.003960
0.14650	-0.17721	0.003960
0.15269	-0.18717	0.003960
0.15924	-0.19736	0.003950
0.16616	-0.20809	0.003950
0.17345	-0.21926	0.003950
0.18114	-0.23017	0.003940
0.18923	-0.23972	0.003910
0.19774	-0.24735	0.003880
0.20667	-0.25564	0.003870
0.21603	-0.26642	0.003870
0.22583	-0.27960	0.003890
0.23608	-0.29399	0.003900
0.24678	-0.30808	0.003900
0.25792	-0.32171	0.003900
0.26952	-0.33432	0.003890
0.28157	-0.34524	0.003870
0.29407	-0.35436	0.003850
0.30700	-0.36279	0.003830
0.32035	-0.37113	0.003810
0.33412	-0.37771	0.003770
0.34828	-0.37963	0.003710
0.36282	-0.37517	0.003620
0.37771	-0.36524	0.003520
0.39293	-0.35225	0.003430
0.40846	-0.33866	0.003350
0.42425	-0.32657	0.003290
0.44029	-0.31706	0.003250
0.45652	-0.31020	0.003230
0.47292	-0.30581	0.003220
0.48945	-0.30293	0.003200
0.50606	-0.29582	0.003140
0.52271	-0.28146	0.003050
0.53938	-0.26520	0.002980
0.55600	-0.25076	0.002920
0.57255	-0.23832	0.002880
0.58898	-0.22699	0.002840
0.60526	-0.21392	0.002780
0.62133	-0.19533	0.002680
0.63717	-0.16910	0.002530
0.65273	-0.13512	0.002340
0.66799	-0.09449	0.002120
0.68291	-0.04992	0.001900
0.69747	-0.00511	0.001700
0.71166	0.03688	0.001520
0.72546	0.07633	0.001350
0.73885	0.11448	0.001180
0.75182	0.15042	0.001030
0.76438	0.18267	0.000920
0.77651	0.21064	0.000830
0.78821	0.23464	0.000760
0.79949	0.25510	0.000720
0.81034	0.27256	0.000680
0.82075	0.28742	0.000670
0.83074	0.29990	0.000660
0.84031	0.31025	0.000660
0.84945	0.31864	0.000670
0.85818	0.32527	0.000690
0.86650	0.33033	0.000720
0.87441	0.33401	0.000750
0.88194	0.33654	0.000780
0.88909	0.33802	0.000820
0.89587	0.33878	0.000850
0.90229	0.33907	0.000880
0.90837	0.33897	0.000910
0.91412	0.33853	0.000950
0.91955	0.33765	0.000980
0.92468	0.33633	0.001010
0.92951	0.33467	0.001050
0.93407	0.33270	0.001080
0.93836	0.33047	0.001120
0.94240	0.32791	0.001150
0.94620	0.32532	0.001180
0.94977	0.32239	0.001220
0.95334	0.31910	0.001250
0.95689	0.31570	0.001290
0.96039	0.31193	0.001330
0.96382	0.30799	0.001360
0.96714	0.30376	0.001400
0.97033	0.29935	0.001440
0.97336	0.29484	0.001480
0.97623	0.29021	0.001520
0.97892	0.28549	0.001560
0.98142	0.28072	0.001600
0.98374	0.27598	0.001640
0.98587	0.27121	0.001690
0.98782	0.26644	0.001730
0.98959	0.26165	0.001770
0.99120	0.25686	0.001810
0.99265	0.25203	0.001860
0.99395	0.24737	0.001910
0.99511	0.24246	0.001960
0.99615	0.23744	0.002020
0.99708	0.23212	0.002080
0.99790	0.22693	0.002180
0.99863	0.22124	0.002440
0.99928	0.21767	0.003340
0.99985	0.21758	0.003340

WING SECTION 3   Y/BO2 0.289 (Y = 220. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.00664	-0.000010
0.00001	1.00176	0.001190
0.00005	0.98960	0.001450
0.00011	0.97408	0.001720
0.00019	0.95597	0.001980
0.00030	0.93486	0.002240
0.00043	0.91099	0.002500
0.00059	0.88437	0.002750
0.00078	0.85527	0.002990
0.00100	0.82382	0.003220
0.00125	0.79001	0.003450
0.00152	0.75415	0.003660
0.00183	0.71665	0.003860
0.00217	0.67758	0.004040
0.00254	0.63735	0.004210
0.00294	0.59648	0.004370
0.00337	0.55484	0.004510
0.00383	0.51353	0.004630
0.00431	0.47290	0.004730
0.00482	0.43258	0.004830
0.00535	0.39309	0.004910
0.00591	0.35438	0.005000
0.00649	0.31638	0.005080
0.00708	0.27925	0.005180
0.00770	0.24145	0.005300
0.00770	0.24145	0.005180
0.00831	0.20521	0.005330
0.00899	0.16864	0.005420
0.00972	0.12845	0.005540
0.01052	0.08584	0.005680
0.01139	0.03934	0.005820
0.01233	-0.01042	0.005970
0.01336	-0.06396	0.006140
0.01447	-0.12230	0.006320
0.01567	-0.18531	0.006510
0.01698	-0.25353	0.006700
0.01838	-0.32531	0.006860
0.01990	-0.40031	0.007010
0.02154	-0.47788	0.007120
0.02331	-0.55470	0.007180
0.02520	-0.62957	0.007200
0.02723	-0.69992	0.007160
0.02940	-0.76421	0.007090
0.03171	-0.82196	0.006990
0.03415	-0.87271	0.006870
0.03673	-0.91672	0.006760
0.03945	-0.95535	0.006640
0.04230	-0.98864	0.006520
0.04527	-1.01736	0.006430
0.04837	-1.04437	0.006350
0.05159	-1.06894	0.006260
0.05492	-1.09088	0.006180
0.05835	-1.11069	0.006100
0.06189	-1.12856	0.006020
0.06551	-1.14462	0.005950
0.06922	-1.15848	0.005870
0.07300	-1.17027	0.005800
0.07684	-1.17967	0.005710
0.08072	-1.18663	0.005630
0.08465	-1.19161	0.005560
0.08860	-1.19489	0.005490
0.09256	-1.19637	0.005410
0.09652	-1.19634	0.005340
0.10048	-1.19447	0.005260
0.10441	-1.19130	0.005200
0.10831	-1.18796	0.005150
0.11221	-1.18429	0.005090
0.11636	-1.17983	0.005040
0.12077	-1.17428	0.004980
0.12545	-1.16768	0.004920
0.13041	-1.15966	0.004860
0.13567	-1.15042	0.004800
0.14124	-1.14067	0.004740
0.14714	-1.13031	0.004690
0.15337	-1.11970	0.004640
0.15996	-1.10881	0.004590
0.16691	-1.09766	0.004530
0.17424	-1.08639	0.004500
0.18197	-1.07860	0.004500
0.19009	-1.07522	0.004490
0.19864	-1.06855	0.004440
0.20761	-1.05919	0.004390
0.21702	-1.05169	0.004370
0.22686	-1.04549	0.004340
0.23716	-1.04000	0.004320
0.24791	-1.03480	0.004300
0.25911	-1.02942	0.004270
0.27077	-1.02223	0.004220
0.28287	-1.01214	0.004160
0.29543	-0.99778	0.004090
0.30842	-0.97780	0.003970
0.32184	-0.95459	0.003860
0.33566	-0.93335	0.003770
0.34989	-0.91786	0.003740
0.36450	-0.90984	0.003750
0.37946	-0.90964	0.003800
0.39476	-0.91569	0.003870
0.41036	-0.92488	0.003940
0.42623	-0.93264	0.003970
0.44234	-0.93238	0.003930
0.45864	-0.91775	0.003830
0.47512	-0.88678	0.003630
0.49170	-0.84047	0.003320
0.50837	-0.77694	0.002910
0.52509	-0.69957	0.002540
0.54180	-0.62597	0.002360
0.55846	-0.56896	0.002270
0.57502	-0.52233	0.002170
0.59145	-0.47684	0.002050
0.60771	-0.43248	0.001940
0.62378	-0.39314	0.001870
0.63963	-0.36117	0.001840
0.65522	-0.33649	0.001850
0.67053	-0.31786	0.001890
0.68553	-0.30421	0.001920
0.70019	-0.29177	0.001930
0.71447	-0.27622	0.001910
0.72837	-0.25877	0.001880
0.74187	-0.24351	0.001870
0.75495	-0.23149	0.001880
0.76761	-0.22212	0.001900
0.77983	-0.21501	0.001920
0.79161	-0.20881	0.001940
0.80295	-0.20272	0.001950
0.81383	-0.19623	0.001940
0.82426	-0.18822	0.001920
0.83424	-0.17836	0.001880
0.84377	-0.16660	0.001830
0.85286	-0.15301	0.001770
0.86152	-0.13797	0.001690
0.86976	-0.12187	0.001610
0.87759	-0.10510	0.001530
0.88502	-0.08811	0.001450
0.89206	-0.07134	0.001370
0.89873	-0.05525	0.001300
0.90505	-0.03998	0.001230
0.91102	-0.02559	0.001170
0.91666	-0.01188	0.001100
0.92199	0.00136	0.001040
0.92701	0.01404	0.000980
0.93175	0.02613	0.000920
0.93621	0.03759	0.000870
0.94040	0.04850	0.000820
0.94435	0.05868	0.000770
0.94806	0.06852	0.000720
0.95155	0.07755	0.000690
0.95505	0.08628	0.000640
0.95853	0.09536	0.000600
0.96195	0.10405	0.000560
0.96530	0.11250	0.000520
0.96853	0.12059	0.000480
0.97164	0.12830	0.000450
0.97459	0.13554	0.000410
0.97737	0.14225	0.000380
0.97998	0.14841	0.000360
0.98240	0.15413	0.000330
0.98463	0.15924	0.000310
0.98668	0.16389	0.000290
0.98856	0.16803	0.000270
0.99025	0.17171	0.000260
0.99179	0.17496	0.000250
0.99317	0.17773	0.000240
0.99441	0.18019	0.000240
0.99552	0.18222	0.000240
0.99651	0.18388	0.000240
0.99739	0.18520	0.000260
0.99817	0.18640	0.000290
0.99885	0.18695	0.000380
0.99946	0.18901	0.000690

WING SECTION 3   Y/BO2 0.289 (Y = 220. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01769	0.000230
0.00001	1.02063	-0.000630
0.00006	1.02517	-0.000300
0.00014	1.02658	0.000030
0.00025	1.02422	0.000370
0.00041	1.01794	0.000710
0.00060	1.00773	0.001050
0.00083	0.99360	0.001380
0.00109	0.97578	0.001700
0.00140	0.95441	0.002000
0.00174	0.92988	0.002290
0.00212	0.90261	0.002550
0.00253	0.87298	0.002790
0.00298	0.84151	0.003010
0.00346	0.80878	0.003210
0.00397	0.77514	0.003380
0.00451	0.74131	0.003510
0.00508	0.70786	0.003620
0.00567	0.67513	0.003710
0.00629	0.64389	0.003770
0.00692	0.61393	0.003800
0.00757	0.58626	0.003820
0.00824	0.56008	0.003850
0.00891	0.53503	0.003880
0.00960	0.51112	0.003880
0.01029	0.48837	0.003920
0.01105	0.46552	0.003960
0.01186	0.44127	0.004010
0.01274	0.41675	0.004060
0.01369	0.39121	0.004110
0.01471	0.36525	0.004160
0.01581	0.33841	0.004210
0.01699	0.31108	0.004260
0.01826	0.28422	0.004290
0.01961	0.25783	0.004310
0.02107	0.23263	0.004320
0.02262	0.20918	0.004320
0.02427	0.18734	0.004310
0.02603	0.16671	0.004310
0.02789	0.14744	0.004300
0.02987	0.12892	0.004310
0.03196	0.11062	0.004320
0.03416	0.09245	0.004320
0.03648	0.07531	0.004320
0.03892	0.05904	0.004320
0.04148	0.04357	0.004310
0.04414	0.02884	0.004310
0.04693	0.01424	0.004310
0.04983	0.00007	0.004310
0.05284	-0.01371	0.004300
0.05596	-0.02690	0.004300
0.05918	-0.03919	0.004280
0.06250	-0.05021	0.004260
0.06592	-0.06065	0.004250
0.06941	-0.07105	0.004240
0.07299	-0.08144	0.004240
0.07664	-0.09203	0.004230
0.08034	-0.10241	0.004230
0.08410	-0.11244	0.004220
0.08790	-0.12211	0.004220
0.09174	-0.13152	0.004210
0.09559	-0.14077	0.004210
0.09945	-0.15001	0.004210
0.10331	-0.15910	0.004210
0.10717	-0.16869	0.004210
0.11102	-0.17824	0.004210
0.11512	-0.18767	0.004210
0.11948	-0.19777	0.004210
0.12411	-0.20824	0.004220
0.12902	-0.21910	0.004220
0.13424	-0.23001	0.004210
0.13976	-0.24075	0.004210
0.14561	-0.25134	0.004190
0.15180	-0.26164	0.004180
0.15835	-0.27156	0.004160
0.16526	-0.28087	0.004140
0.17256	-0.29001	0.004130
0.18024	-0.29842	0.004090
0.18834	-0.30407	0.004040
0.19684	-0.30647	0.003980
0.20577	-0.30872	0.003950
0.21514	-0.31309	0.003930
0.22494	-0.31948	0.003920
0.23518	-0.32717	0.003910
0.24588	-0.33508	0.003900
0.25702	-0.34280	0.003890
0.26861	-0.35021	0.003870
0.28065	-0.35688	0.003850
0.29314	-0.36181	0.003820
0.30606	-0.36495	0.003780
0.31940	-0.36651	0.003740
0.33315	-0.36598	0.003680
0.34729	-0.36179	0.003610
0.36180	-0.35268	0.003510
0.37668	-0.33944	0.003420
0.39187	-0.32439	0.003330
0.40738	-0.30961	0.003250
0.42315	-0.29669	0.003200
0.43917	-0.28647	0.003170
0.45539	-0.27872	0.003150
0.47177	-0.27317	0.003140
0.48828	-0.26895	0.003120
0.50487	-0.26112	0.003060
0.52151	-0.24663	0.002970
0.53816	-0.23060	0.002900
0.55477	-0.21721	0.002860
0.57132	-0.20652	0.002830
0.58775	-0.19761	0.002800
0.60403	-0.18765	0.002760
0.62011	-0.17271	0.002670
0.63596	-0.15017	0.002540
0.65154	-0.11952	0.002360
0.66681	-0.08163	0.002150
0.68175	-0.03908	0.001930
0.69635	0.00437	0.001730
0.71057	0.04536	0.001550
0.72441	0.08372	0.001380
0.73784	0.12087	0.001210
0.75087	0.15619	0.001060
0.76348	0.18801	0.000940
0.77566	0.21571	0.000850
0.78743	0.23954	0.000790
0.79876	0.25983	0.000740
0.80967	0.27715	0.000710
0.82015	0.29187	0.000690
0.83019	0.30425	0.000680
0.83982	0.31449	0.000680
0.84902	0.32275	0.000700
0.85780	0.32927	0.000710
0.86618	0.33424	0.000740
0.87415	0.33781	0.000770
0.88173	0.34022	0.000800
0.88893	0.34157	0.000840
0.89575	0.34221	0.000870
0.90222	0.34238	0.000900
0.90834	0.34216	0.000940
0.91413	0.34160	0.000970
0.91960	0.34060	0.001000
0.92477	0.33917	0.001040
0.92964	0.33740	0.001070
0.93423	0.33531	0.001110
0.93855	0.33296	0.001140
0.94262	0.33028	0.001180
0.94645	0.32759	0.001210
0.95005	0.32454	0.001250
0.95365	0.32113	0.001280
0.95723	0.31765	0.001320
0.96075	0.31374	0.001360
0.96419	0.30967	0.001400
0.96752	0.30536	0.001440
0.97071	0.30081	0.001480
0.97374	0.29622	0.001520
0.97660	0.29148	0.001560
0.97928	0.28661	0.001600
0.98176	0.28183	0.001640
0.98406	0.27699	0.001690
0.98617	0.27210	0.001730
0.98809	0.26724	0.001770
0.98984	0.26248	0.001820
0.99142	0.25766	0.001860
0.99284	0.25273	0.001910
0.99412	0.24799	0.001960
0.99526	0.24310	0.002010
0.99628	0.23806	0.002070
0.99718	0.23271	0.002140
0.99798	0.22758	0.002250
0.99869	0.22189	0.002520
0.99932	0.21831	0.003460
0.99987	0.21821	0.003460

WING SECTION 4   Y/BO2 0.420 (Y = 320. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.00319	0.000000
0.00001	0.99823	0.001260
0.00005	0.98584	0.001530
0.00010	0.97008	0.001810
0.00019	0.95173	0.002080
0.00029	0.93039	0.002350
0.00043	0.90628	0.002620
0.00058	0.87939	0.002880
0.00077	0.84998	0.003130
0.00099	0.81822	0.003370
0.00123	0.78411	0.003600
0.00151	0.74791	0.003820
0.00182	0.71013	0.004020
0.00216	0.67074	0.004210
0.00252	0.63022	0.004390
0.00292	0.58905	0.004550
0.00335	0.54716	0.004690
0.00380	0.50567	0.004800
0.00428	0.46480	0.004910
0.00479	0.42421	0.005000
0.00532	0.38437	0.005090
0.00587	0.34529	0.005170
0.00645	0.30693	0.005250
0.00704	0.26944	0.005340
0.00765	0.23193	0.005460
0.00765	0.23193	0.005340
0.00827	0.19545	0.005490
0.00894	0.15840	0.005580
0.00967	0.11841	0.005690
0.01046	0.07579	0.005820
0.01133	0.02926	0.005970
0.01226	-0.02043	0.006120
0.01328	-0.07393	0.006290
0.01438	-0.13232	0.006470
0.01557	-0.19526	0.006660
0.01686	-0.26329	0.006850
0.01825	-0.33502	0.007010
0.01975	-0.41019	0.007170
0.02137	-0.48794	0.007280
0.02312	-0.56472	0.007320
0.02499	-0.63893	0.007330
0.02699	-0.70926	0.007300
0.02913	-0.77404	0.007220
0.03140	-0.83167	0.007100
0.03381	-0.88138	0.006970
0.03636	-0.92471	0.006850
0.03903	-0.96315	0.006730
0.04184	-0.99641	0.006620
0.04477	-1.02562	0.006520
0.04783	-1.05199	0.006430
0.05100	-1.07637	0.006350
0.05429	-1.09838	0.006260
0.05768	-1.11783	0.006180
0.06117	-1.13518	0.006100
0.06475	-1.15070	0.006030
0.06841	-1.16452	0.005950
0.07215	-1.17591	0.005870
0.07595	-1.18493	0.005780
0.07980	-1.19151	0.005700
0.08368	-1.19612	0.005630
0.08760	-1.19911	0.005550
0.09154	-1.20036	0.005480
0.09548	-1.19991	0.005400
0.09941	-1.19787	0.005330
0.10333	-1.19466	0.005260
0.10721	-1.19100	0.005210
0.11111	-1.18704	0.005150
0.11525	-1.18236	0.005100
0.11964	-1.17637	0.005040
0.12431	-1.16880	0.004970
0.12926	-1.16013	0.004910
0.13450	-1.15033	0.004850
0.14006	-1.13947	0.004790
0.14594	-1.12796	0.004730
0.15216	-1.11609	0.004680
0.15872	-1.10421	0.004630
0.16566	-1.09207	0.004570
0.17297	-1.07970	0.004530
0.18067	-1.07017	0.004530
0.18877	-1.06595	0.004530
0.19729	-1.05973	0.004480
0.20623	-1.05025	0.004440
0.21561	-1.04290	0.004410
0.22543	-1.03743	0.004400
0.23570	-1.03381	0.004390
0.24642	-1.03172	0.004380
0.25759	-1.03038	0.004360
0.26922	-1.02919	0.004340
0.28130	-1.02766	0.004320
0.29383	-1.02422	0.004270
0.30680	-1.01765	0.004220
0.32020	-1.00761	0.004150
0.33401	-0.99522	0.004090
0.34822	-0.98105	0.004020
0.36281	-0.96466	0.003950
0.37777	-0.94733	0.003880
0.39306	-0.93339	0.003860
0.40866	-0.92692	0.003880
0.42454	-0.92684	0.003910
0.44065	-0.92805	0.003920
0.45698	-0.92451	0.003870
0.47347	-0.91239	0.003760
0.49008	-0.88915	0.003580
0.50678	-0.84587	0.003240
0.52352	-0.76184	0.002710
0.54028	-0.65988	0.002300
0.55699	-0.58402	0.002200
0.57360	-0.53438	0.002170
0.59008	-0.49419	0.002110
0.60640	-0.45420	0.002020
0.62252	-0.41671	0.001950
0.63841	-0.38549	0.001930
0.65405	-0.36111	0.001940
0.66941	-0.34228	0.001970
0.68446	-0.32780	0.002000
0.69918	-0.31446	0.002000
0.71352	-0.29823	0.001970
0.72747	-0.27971	0.001930
0.74102	-0.26292	0.001910
0.75416	-0.24906	0.001910
0.76687	-0.23754	0.001910
0.77914	-0.22799	0.001920
0.79097	-0.21933	0.001920
0.80236	-0.21073	0.001920
0.81330	-0.20169	0.001900
0.82378	-0.19136	0.001870
0.83381	-0.17946	0.001820
0.84340	-0.16600	0.001760
0.85254	-0.15105	0.001690
0.86125	-0.13495	0.001610
0.86954	-0.11806	0.001530
0.87742	-0.10079	0.001450
0.88490	-0.08349	0.001360
0.89198	-0.06649	0.001280
0.89870	-0.05022	0.001210
0.90506	-0.03481	0.001140
0.91107	-0.02030	0.001080
0.91675	-0.00652	0.001010
0.92212	0.00673	0.000950
0.92718	0.01934	0.000890
0.93195	0.03133	0.000840
0.93644	0.04263	0.000780
0.94067	0.05340	0.000730
0.94465	0.06329	0.000680
0.94839	0.07299	0.000640
0.95191	0.08168	0.000600
0.95543	0.09003	0.000560
0.95893	0.09896	0.000520
0.96238	0.10731	0.000480
0.96574	0.11546	0.000440
0.96898	0.12317	0.000410
0.97208	0.13050	0.000370
0.97503	0.13737	0.000340
0.97780	0.14373	0.000310
0.98038	0.14951	0.000290
0.98278	0.15484	0.000270
0.98499	0.15965	0.000250
0.98702	0.16395	0.000230
0.98886	0.16779	0.000210
0.99053	0.17119	0.000200
0.99203	0.17416	0.000190
0.99338	0.17671	0.000190
0.99459	0.17897	0.000190
0.99567	0.18080	0.000190
0.99663	0.18231	0.000200
0.99748	0.18351	0.000210
0.99823	0.18462	0.000250
0.99890	0.18513	0.000340
0.99948	0.18726	0.000630

WING SECTION 4   Y/BO2 0.420 (Y = 320. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01461	0.000230
0.00001	1.01769	-0.000670
0.00006	1.02246	-0.000330
0.00014	1.02415	0.000010
0.00025	1.02212	0.000370
0.00041	1.01616	0.000720
0.00060	1.00627	0.001080
0.00083	0.99243	0.001420
0.00109	0.97488	0.001750
0.00139	0.95377	0.002070
0.00173	0.92942	0.002370
0.00211	0.90230	0.002640
0.00252	0.87271	0.002900
0.00297	0.84125	0.003130
0.00344	0.80843	0.003330
0.00396	0.77459	0.003510
0.00450	0.74057	0.003650
0.00506	0.70670	0.003770
0.00566	0.67368	0.003850
0.00628	0.64208	0.003910
0.00691	0.61166	0.003950
0.00757	0.58347	0.003970
0.00824	0.55659	0.004000
0.00892	0.53102	0.004030
0.00961	0.50609	0.004030
0.01032	0.48281	0.004050
0.01108	0.45975	0.004090
0.01190	0.43477	0.004140
0.01279	0.40967	0.004190
0.01374	0.38335	0.004240
0.01477	0.35677	0.004290
0.01587	0.32933	0.004340
0.01706	0.30131	0.004380
0.01832	0.27396	0.004410
0.01968	0.24704	0.004430
0.02113	0.22126	0.004440
0.02268	0.19718	0.004430
0.02432	0.17460	0.004430
0.02607	0.15326	0.004420
0.02793	0.13327	0.004420
0.02989	0.11409	0.004420
0.03197	0.09516	0.004430
0.03415	0.07639	0.004440
0.03645	0.05836	0.004440
0.03886	0.04136	0.004440
0.04139	0.02514	0.004430
0.04403	0.00937	0.004430
0.04679	-0.00606	0.004430
0.04966	-0.02100	0.004430
0.05263	-0.03554	0.004430
0.05571	-0.04952	0.004420
0.05890	-0.06267	0.004410
0.06218	-0.07477	0.004390
0.06556	-0.08590	0.004380
0.06902	-0.09663	0.004370
0.07256	-0.10786	0.004370
0.07617	-0.11946	0.004370
0.07984	-0.13065	0.004370
0.08357	-0.14132	0.004360
0.08734	-0.15142	0.004350
0.09115	-0.16114	0.004340
0.09498	-0.17079	0.004340
0.09883	-0.18053	0.004340
0.10269	-0.19021	0.004350
0.10653	-0.20048	0.004350
0.11039	-0.21063	0.004350
0.11448	-0.22068	0.004350
0.11884	-0.23165	0.004360
0.12346	-0.24262	0.004350
0.12837	-0.25385	0.004350
0.13358	-0.26527	0.004350
0.13910	-0.27648	0.004340
0.14495	-0.28742	0.004330
0.15113	-0.29766	0.004310
0.15767	-0.30735	0.004290
0.16457	-0.31657	0.004270
0.17186	-0.32494	0.004240
0.17954	-0.33201	0.004200
0.18762	-0.33671	0.004140
0.19611	-0.33757	0.004070
0.20503	-0.33726	0.004020
0.21438	-0.33920	0.004000
0.22417	-0.34312	0.003980
0.23440	-0.34808	0.003960
0.24508	-0.35341	0.003950
0.25621	-0.35873	0.003930
0.26778	-0.36384	0.003910
0.27981	-0.36819	0.003880
0.29227	-0.37096	0.003840
0.30517	-0.37147	0.003790
0.31849	-0.37008	0.003740
0.33222	-0.36673	0.003680
0.34634	-0.35996	0.003600
0.36083	-0.34851	0.003500
0.37568	-0.33327	0.003400
0.39086	-0.31639	0.003300
0.40634	-0.29979	0.003230
0.42209	-0.28512	0.003170
0.43808	-0.27305	0.003130
0.45428	-0.26339	0.003100
0.47064	-0.25582	0.003090
0.48713	-0.24969	0.003060
0.50369	-0.24083	0.003010
0.52030	-0.22565	0.002920
0.53693	-0.20826	0.002840
0.55353	-0.19300	0.002790
0.57006	-0.18004	0.002750
0.58647	-0.16880	0.002710
0.60274	-0.15700	0.002660
0.61880	-0.14124	0.002580
0.63464	-0.11910	0.002450
0.65022	-0.09003	0.002290
0.66549	-0.05460	0.002090
0.68045	-0.01476	0.001880
0.69506	0.02637	0.001690
0.70931	0.06549	0.001510
0.72318	0.10216	0.001350
0.73666	0.13755	0.001190
0.74973	0.17102	0.001050
0.76240	0.20122	0.000940
0.77466	0.22756	0.000850
0.78649	0.25013	0.000790
0.79791	0.26929	0.000750
0.80889	0.28563	0.000730
0.81944	0.29947	0.000710
0.82956	0.31112	0.000700
0.83926	0.32070	0.000710
0.84853	0.32843	0.000720
0.85738	0.33449	0.000740
0.86582	0.33906	0.000770
0.87386	0.34234	0.000800
0.88150	0.34444	0.000840
0.88875	0.34554	0.000870
0.89564	0.34592	0.000910
0.90216	0.34584	0.000940
0.90833	0.34540	0.000970
0.91417	0.34460	0.001010
0.91968	0.34338	0.001040
0.92489	0.34171	0.001080
0.92980	0.33973	0.001120
0.93443	0.33742	0.001150
0.93879	0.33487	0.001190
0.94290	0.33202	0.001220
0.94677	0.32922	0.001260
0.95040	0.32594	0.001300
0.95402	0.32233	0.001330
0.95763	0.31870	0.001370
0.96118	0.31454	0.001410
0.96463	0.31022	0.001450
0.96797	0.30572	0.001500
0.97116	0.30096	0.001540
0.97419	0.29609	0.001580
0.97704	0.29113	0.001630
0.97970	0.28609	0.001670
0.98217	0.28110	0.001710
0.98444	0.27600	0.001760
0.98652	0.27094	0.001800
0.98842	0.26593	0.001850
0.99013	0.26097	0.001890
0.99168	0.25606	0.001940
0.99307	0.25103	0.001990
0.99432	0.24607	0.002040
0.99543	0.24109	0.002100
0.99642	0.23596	0.002160
0.99729	0.23050	0.002230
0.99807	0.22528	0.002340
0.99875	0.21954	0.002630
0.99936	0.21594	0.003610
0.99989	0.21578	0.003610

WING SECTION 5   Y/BO2 0.551 (Y = 420. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.00335	-0.000030
0.00001	0.99853	0.001270
0.00005	0.98646	0.001550
0.00010	0.97108	0.001840
0.00019	0.95309	0.002130
0.00029	0.93211	0.002410
0.00042	0.90838	0.002690
0.00058	0.88189	0.002960
0.00077	0.85290	0.003210
0.00099	0.82156	0.003460
0.00123	0.78789	0.003700
0.00151	0.75209	0.003930
0.00181	0.71465	0.004140
0.00215	0.67564	0.004340
0.00252	0.63543	0.004520
0.00291	0.59461	0.004680
0.00334	0.55302	0.004820
0.00379	0.51169	0.004940
0.00427	0.47102	0.005040
0.00477	0.43064	0.005140
0.00530	0.39098	0.005220
0.00585	0.35211	0.005300
0.00643	0.31392	0.005380
0.00702	0.27668	0.005460
0.00763	0.23912	0.005580
0.00763	0.23912	0.005460
0.00824	0.20271	0.005610
0.00890	0.16591	0.005690
0.00962	0.12592	0.005810
0.01041	0.08353	0.005940
0.01127	0.03713	0.006090
0.01219	-0.01224	0.006230
0.01320	-0.06523	0.006400
0.01428	-0.12322	0.006590
0.01546	-0.18550	0.006780
0.01673	-0.25261	0.006960
0.01810	-0.32400	0.007140
0.01958	-0.39906	0.007290
0.02118	-0.47581	0.007390
0.02289	-0.55223	0.007450
0.02473	-0.62625	0.007450
0.02670	-0.69568	0.007400
0.02880	-0.75935	0.007310
0.03104	-0.81610	0.007190
0.03340	-0.86602	0.007070
0.03590	-0.90964	0.006950
0.03853	-0.94797	0.006830
0.04129	-0.98135	0.006710
0.04417	-1.01093	0.006610
0.04718	-1.03811	0.006530
0.05030	-1.06262	0.006440
0.05353	-1.08457	0.006350
0.05687	-1.10467	0.006270
0.06030	-1.12256	0.006190
0.06383	-1.13831	0.006120
0.06744	-1.15256	0.006040
0.07113	-1.16467	0.005960
0.07488	-1.17426	0.005880
0.07868	-1.18147	0.005790
0.08253	-1.18665	0.005720
0.08641	-1.19014	0.005640
0.09031	-1.19188	0.005570
0.09422	-1.19203	0.005490
0.09813	-1.19031	0.005410
0.10203	-1.18718	0.005340
0.10590	-1.18366	0.005290
0.10979	-1.17978	0.005230
0.11391	-1.17523	0.005180
0.11830	-1.16956	0.005120
0.12295	-1.16260	0.005050
0.12788	-1.15412	0.004990
0.13311	-1.14440	0.004920
0.13865	-1.13391	0.004860
0.14452	-1.12267	0.004800
0.15071	-1.11103	0.004750
0.15726	-1.09915	0.004700
0.16417	-1.08702	0.004640
0.17146	-1.07467	0.004600
0.17913	-1.06429	0.004590
0.18721	-1.05965	0.004590
0.19569	-1.05398	0.004550
0.20461	-1.04434	0.004500
0.21395	-1.03641	0.004470
0.22374	-1.03018	0.004450
0.23397	-1.02587	0.004440
0.24465	-1.02296	0.004420
0.25579	-1.02066	0.004410
0.26739	-1.01879	0.004390
0.27943	-1.01689	0.004360
0.29192	-1.01354	0.004320
0.30486	-1.00722	0.004270
0.31822	-0.99817	0.004200
0.33200	-0.98713	0.004140
0.34618	-0.97490	0.004080
0.36075	-0.96102	0.004010
0.37569	-0.94493	0.003930
0.39096	-0.92979	0.003890
0.40654	-0.92127	0.003910
0.42241	-0.92171	0.003950
0.43852	-0.92803	0.004010
0.45484	-0.93486	0.004010
0.47133	-0.93363	0.003940
0.48796	-0.91132	0.003710
0.50467	-0.84791	0.003190
0.52144	-0.74648	0.002610
0.53823	-0.65156	0.002350
0.55497	-0.59084	0.002350
0.57164	-0.55305	0.002360
0.58818	-0.51992	0.002310
0.60456	-0.48415	0.002230
0.62074	-0.44928	0.002160
0.63669	-0.41909	0.002130
0.65240	-0.39480	0.002120
0.66782	-0.37585	0.002140
0.68294	-0.36034	0.002150
0.69773	-0.34517	0.002140
0.71214	-0.32722	0.002090
0.72616	-0.30700	0.002040
0.73978	-0.28788	0.002000
0.75298	-0.27119	0.001980
0.76575	-0.25649	0.001960
0.77809	-0.24337	0.001950
0.78998	-0.23116	0.001930
0.80143	-0.21909	0.001910
0.81243	-0.20665	0.001880
0.82298	-0.19335	0.001830
0.83308	-0.17899	0.001780
0.84273	-0.16356	0.001710
0.85194	-0.14719	0.001640
0.86072	-0.13006	0.001560
0.86907	-0.11255	0.001480
0.87701	-0.09495	0.001390
0.88455	-0.07752	0.001310
0.89170	-0.06055	0.001230
0.89848	-0.04433	0.001160
0.90489	-0.02897	0.001090
0.91096	-0.01453	0.001030
0.91670	-0.00082	0.000960
0.92212	0.01229	0.000900
0.92723	0.02474	0.000850
0.93205	0.03654	0.000790
0.93659	0.04763	0.000740
0.94087	0.05818	0.000690
0.94489	0.06777	0.000640
0.94868	0.07733	0.000600
0.95223	0.08568	0.000570
0.95580	0.09374	0.000520
0.95933	0.10255	0.000480
0.96280	0.11060	0.000450
0.96618	0.11849	0.000410
0.96944	0.12593	0.000380
0.97255	0.13296	0.000340
0.97549	0.13952	0.000310
0.97825	0.14563	0.000290
0.98082	0.15115	0.000260
0.98320	0.15622	0.000240
0.98539	0.16080	0.000220
0.98738	0.16487	0.000210
0.98919	0.16849	0.000190
0.99083	0.17172	0.000180
0.99230	0.17449	0.000180
0.99361	0.17688	0.000170
0.99479	0.17901	0.000170
0.99584	0.18070	0.000170
0.99676	0.18211	0.000180
0.99758	0.18324	0.000200
0.99831	0.18429	0.000240
0.99894	0.18476	0.000330
0.99951	0.18690	0.000630

WING SECTION 5   Y/BO2 0.551 (Y = 420. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01435	0.000270
0.00001	1.01728	-0.000660
0.00006	1.02160	-0.000300
0.00013	1.02271	0.000070
0.00025	1.02016	0.000440
0.00040	1.01370	0.000810
0.00059	1.00335	0.001170
0.00081	0.98907	0.001530
0.00108	0.97107	0.001870
0.00137	0.94956	0.002200
0.00171	0.92470	0.002510
0.00208	0.89709	0.002800
0.00249	0.86690	0.003070
0.00293	0.83484	0.003310
0.00341	0.80138	0.003520
0.00392	0.76686	0.003710
0.00446	0.73215	0.003860
0.00503	0.69749	0.003980
0.00562	0.66372	0.004070
0.00624	0.63116	0.004120
0.00688	0.60008	0.004150
0.00754	0.57123	0.004170
0.00822	0.54363	0.004190
0.00891	0.51764	0.004210
0.00961	0.49223	0.004210
0.01032	0.46818	0.004230
0.01110	0.44438	0.004260
0.01193	0.41881	0.004310
0.01283	0.39310	0.004350
0.01379	0.36644	0.004400
0.01483	0.33946	0.004440
0.01594	0.31164	0.004500
0.01713	0.28302	0.004540
0.01840	0.25502	0.004560
0.01976	0.22780	0.004570
0.02121	0.20192	0.004570
0.02275	0.17789	0.004560
0.02439	0.15533	0.004550
0.02613	0.13418	0.004530
0.02798	0.11426	0.004530
0.02993	0.09511	0.004530
0.03199	0.07633	0.004540
0.03415	0.05782	0.004540
0.03643	0.03986	0.004540
0.03882	0.02301	0.004540
0.04132	0.00693	0.004530
0.04393	-0.00886	0.004530
0.04665	-0.02397	0.004530
0.04948	-0.03862	0.004530
0.05241	-0.05314	0.004530
0.05545	-0.06716	0.004520
0.05860	-0.08020	0.004510
0.06184	-0.09209	0.004490
0.06517	-0.10324	0.004470
0.06859	-0.11370	0.004460
0.07208	-0.12475	0.004470
0.07565	-0.13629	0.004460
0.07929	-0.14706	0.004460
0.08298	-0.15748	0.004450
0.08672	-0.16763	0.004440
0.09050	-0.17747	0.004440
0.09431	-0.18713	0.004430
0.09814	-0.19674	0.004430
0.10198	-0.20621	0.004430
0.10582	-0.21621	0.004430
0.10967	-0.22623	0.004430
0.11377	-0.23623	0.004440
0.11811	-0.24698	0.004440
0.12273	-0.25818	0.004440
0.12764	-0.26949	0.004440
0.13284	-0.28096	0.004440
0.13835	-0.29229	0.004430
0.14418	-0.30311	0.004420
0.15036	-0.31364	0.004400
0.15688	-0.32353	0.004380
0.16377	-0.33259	0.004350
0.17104	-0.34102	0.004330
0.17871	-0.34854	0.004290
0.18677	-0.35365	0.004230
0.19525	-0.35468	0.004160
0.20414	-0.35408	0.004100
0.21347	-0.35532	0.004070
0.22324	-0.35879	0.004060
0.23345	-0.36357	0.004040
0.24410	-0.36861	0.004020
0.25521	-0.37344	0.004000
0.26676	-0.37794	0.003980
0.27877	-0.38167	0.003950
0.29121	-0.38349	0.003900
0.30409	-0.38310	0.003850
0.31739	-0.38082	0.003800
0.33110	-0.37668	0.003740
0.34520	-0.36951	0.003660
0.35968	-0.35791	0.003560
0.37451	-0.34248	0.003450
0.38967	-0.32518	0.003350
0.40513	-0.30783	0.003270
0.42087	-0.29194	0.003200
0.43685	-0.27842	0.003160
0.45303	-0.26712	0.003120
0.46937	-0.25760	0.003100
0.48585	-0.24942	0.003070
0.50240	-0.23926	0.003010
0.51900	-0.22316	0.002920
0.53562	-0.20390	0.002830
0.55220	-0.18548	0.002750
0.56872	-0.16826	0.002690
0.58513	-0.15231	0.002640
0.60138	-0.13613	0.002570
0.61744	-0.11711	0.002480
0.63328	-0.09334	0.002350
0.64885	-0.06435	0.002190
0.66413	-0.03056	0.002010
0.67910	0.00674	0.001820
0.69373	0.04518	0.001630
0.70801	0.08233	0.001470
0.72192	0.11727	0.001310
0.73544	0.15075	0.001160
0.74856	0.18208	0.001030
0.76129	0.21033	0.000930
0.77361	0.23498	0.000850
0.78552	0.25577	0.000800
0.79700	0.27347	0.000770
0.80805	0.28847	0.000740
0.81868	0.30118	0.000730
0.82888	0.31182	0.000730
0.83864	0.32060	0.000740
0.84799	0.32769	0.000760
0.85691	0.33322	0.000780
0.86542	0.33736	0.000800
0.87352	0.34033	0.000840
0.88122	0.34220	0.000870
0.88854	0.34316	0.000910
0.89548	0.34341	0.000940
0.90206	0.34321	0.000980
0.90829	0.34264	0.001010
0.91418	0.34170	0.001040
0.91975	0.34037	0.001080
0.92501	0.33859	0.001120
0.92997	0.33654	0.001150
0.93465	0.33417	0.001190
0.93906	0.33157	0.001230
0.94321	0.32867	0.001260
0.94711	0.32587	0.001300
0.95078	0.32253	0.001340
0.95445	0.31882	0.001370
0.95809	0.31524	0.001410
0.96166	0.31112	0.001450
0.96513	0.30679	0.001490
0.96848	0.30223	0.001530
0.97168	0.29755	0.001580
0.97470	0.29268	0.001620
0.97754	0.28773	0.001660
0.98019	0.28279	0.001710
0.98263	0.27775	0.001750
0.98488	0.27272	0.001800
0.98693	0.26775	0.001840
0.98879	0.26279	0.001890
0.99047	0.25786	0.001930
0.99199	0.25308	0.001980
0.99334	0.24821	0.002030
0.99455	0.24323	0.002080
0.99563	0.23843	0.002140
0.99658	0.23341	0.002210
0.99743	0.22807	0.002280
0.99818	0.22302	0.002400
0.99883	0.21745	0.002690
0.99941	0.21403	0.003720
0.99992	0.21387	0.003720

WING SECTION 6   Y/BO2 0.682 (Y = 520. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.00310	-0.000070
0.00001	0.99853	0.001260
0.00005	0.98707	0.001550
0.00011	0.97234	0.001850
0.00020	0.95502	0.002140
0.00030	0.93474	0.002440
0.00044	0.91169	0.002730
0.00060	0.88585	0.003010
0.00079	0.85749	0.003290
0.00100	0.82676	0.003540
0.00125	0.79370	0.003790
0.00153	0.75863	0.004020
0.00184	0.72191	0.004240
0.00217	0.68365	0.004440
0.00254	0.64417	0.004630
0.00293	0.60394	0.004800
0.00336	0.56302	0.004940
0.00381	0.52227	0.005060
0.00429	0.48217	0.005160
0.00479	0.44241	0.005250
0.00532	0.40326	0.005330
0.00587	0.36486	0.005410
0.00645	0.32710	0.005490
0.00704	0.29016	0.005580
0.00764	0.25286	0.005690
0.00764	0.25286	0.005580
0.00825	0.21695	0.005710
0.00891	0.18065	0.005800
0.00963	0.14123	0.005910
0.01041	0.09960	0.006040
0.01125	0.05393	0.006180
0.01217	0.00548	0.006330
0.01316	-0.04670	0.006500
0.01423	-0.10397	0.006690
0.01538	-0.16523	0.006880
0.01663	-0.23087	0.007070
0.01798	-0.30141	0.007250
0.01943	-0.37483	0.007390
0.02099	-0.44972	0.007490
0.02267	-0.52495	0.007550
0.02447	-0.59764	0.007550
0.02640	-0.66650	0.007500
0.02846	-0.72946	0.007400
0.03064	-0.78518	0.007280
0.03296	-0.83426	0.007150
0.03540	-0.87761	0.007040
0.03797	-0.91614	0.006920
0.04067	-0.94998	0.006810
0.04349	-0.98023	0.006720
0.04642	-1.00789	0.006620
0.04948	-1.03279	0.006540
0.05264	-1.05557	0.006460
0.05591	-1.07643	0.006380
0.05928	-1.09492	0.006300
0.06274	-1.11137	0.006220
0.06629	-1.12618	0.006150
0.06991	-1.13899	0.006070
0.07360	-1.14970	0.005990
0.07735	-1.15808	0.005900
0.08114	-1.16397	0.005820
0.08498	-1.16795	0.005740
0.08884	-1.17036	0.005670
0.09271	-1.17109	0.005590
0.09659	-1.17038	0.005520
0.10046	-1.16814	0.005450
0.10432	-1.16490	0.005380
0.10819	-1.16120	0.005330
0.11230	-1.15687	0.005270
0.11666	-1.15171	0.005210
0.12129	-1.14507	0.005150
0.12621	-1.13690	0.005080
0.13142	-1.12755	0.005010
0.13694	-1.11722	0.004950
0.14277	-1.10611	0.004890
0.14895	-1.09440	0.004830
0.15547	-1.08248	0.004780
0.16235	-1.07055	0.004720
0.16961	-1.05848	0.004670
0.17725	-1.04739	0.004660
0.18530	-1.04231	0.004670
0.19375	-1.03795	0.004630
0.20263	-1.02915	0.004580
0.21193	-1.02137	0.004550
0.22168	-1.01575	0.004540
0.23187	-1.01203	0.004520
0.24252	-1.01012	0.004510
0.25361	-1.00893	0.004500
0.26517	-1.00771	0.004480
0.27717	-1.00634	0.004450
0.28963	-1.00351	0.004410
0.30252	-0.99756	0.004350
0.31585	-0.98809	0.004280
0.32959	-0.97597	0.004200
0.34374	-0.96189	0.004130
0.35828	-0.94539	0.004040
0.37319	-0.92739	0.003970
0.38844	-0.91258	0.003960
0.40400	-0.90600	0.003990
0.41984	-0.90761	0.004040
0.43594	-0.91316	0.004060
0.45225	-0.91607	0.004020
0.46874	-0.90517	0.003850
0.48536	-0.86199	0.003380
0.50208	-0.77502	0.002780
0.51886	-0.67892	0.002510
0.53567	-0.61473	0.002550
0.55244	-0.57968	0.002610
0.56914	-0.55388	0.002580
0.58572	-0.52197	0.002490
0.60214	-0.48439	0.002360
0.61837	-0.44838	0.002270
0.63439	-0.41739	0.002220
0.65015	-0.39239	0.002210
0.66564	-0.37276	0.002220
0.68083	-0.35671	0.002220
0.69569	-0.34131	0.002210
0.71018	-0.32356	0.002160
0.72428	-0.30335	0.002110
0.73798	-0.28379	0.002060
0.75127	-0.26667	0.002040
0.76413	-0.25165	0.002020
0.77655	-0.23833	0.002000
0.78854	-0.22598	0.001990
0.80008	-0.21390	0.001960
0.81117	-0.20149	0.001930
0.82181	-0.18838	0.001890
0.83199	-0.17429	0.001830
0.84173	-0.15915	0.001770
0.85103	-0.14306	0.001690
0.85990	-0.12624	0.001610
0.86834	-0.10898	0.001530
0.87637	-0.09160	0.001450
0.88399	-0.07438	0.001360
0.89122	-0.05761	0.001280
0.89808	-0.04153	0.001210
0.90457	-0.02623	0.001140
0.91072	-0.01186	0.001080
0.91653	0.00179	0.001010
0.92202	0.01485	0.000950
0.92720	0.02726	0.000890
0.93208	0.03905	0.000840
0.93669	0.05013	0.000780
0.94103	0.06070	0.000730
0.94511	0.07024	0.000680
0.94895	0.07989	0.000640
0.95256	0.08815	0.000610
0.95618	0.09618	0.000560
0.95976	0.10518	0.000520
0.96327	0.11323	0.000480
0.96668	0.12118	0.000440
0.96995	0.12864	0.000410
0.97307	0.13567	0.000370
0.97602	0.14221	0.000340
0.97877	0.14830	0.000310
0.98133	0.15383	0.000290
0.98369	0.15884	0.000270
0.98584	0.16339	0.000250
0.98780	0.16742	0.000230
0.98958	0.17099	0.000220
0.99117	0.17418	0.000210
0.99261	0.17690	0.000200
0.99388	0.17926	0.000190
0.99502	0.18135	0.000190
0.99603	0.18299	0.000200
0.99692	0.18437	0.000200
0.99770	0.18549	0.000220
0.99839	0.18651	0.000270
0.99900	0.18695	0.000360
0.99953	0.18902	0.000670

WING SECTION 6   Y/BO2 0.682 (Y = 520. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01323	0.000320
0.00001	1.01622	-0.000640
0.00005	1.02034	-0.000260
0.00013	1.02097	0.000120
0.00023	1.01787	0.000520
0.00038	1.01081	0.000910
0.00057	0.99985	0.001300
0.00078	0.98488	0.001680
0.00104	0.96614	0.002050
0.00133	0.94391	0.002400
0.00166	0.91817	0.002730
0.00203	0.88963	0.003040
0.00243	0.85854	0.003320
0.00287	0.82540	0.003580
0.00334	0.79077	0.003800
0.00384	0.75516	0.003990
0.00438	0.71910	0.004150
0.00495	0.68327	0.004270
0.00554	0.64841	0.004360
0.00616	0.61449	0.004420
0.00680	0.58239	0.004440
0.00746	0.55255	0.004450
0.00815	0.52396	0.004460
0.00884	0.49727	0.004470
0.00956	0.47113	0.004470
0.01029	0.44602	0.004490
0.01108	0.42122	0.004520
0.01192	0.39486	0.004560
0.01283	0.36818	0.004590
0.01381	0.34103	0.004630
0.01486	0.31342	0.004670
0.01597	0.28493	0.004720
0.01717	0.25581	0.004760
0.01845	0.22699	0.004780
0.01981	0.19953	0.004770
0.02126	0.17370	0.004760
0.02280	0.14949	0.004730
0.02444	0.12727	0.004700
0.02618	0.10672	0.004680
0.02801	0.08731	0.004670
0.02995	0.06856	0.004670
0.03199	0.04994	0.004680
0.03413	0.03169	0.004680
0.03638	0.01404	0.004670
0.03874	-0.00233	0.004660
0.04121	-0.01794	0.004660
0.04378	-0.03325	0.004650
0.04647	-0.04769	0.004640
0.04925	-0.06183	0.004640
0.05215	-0.07591	0.004640
0.05514	-0.08952	0.004630
0.05824	-0.10245	0.004620
0.06143	-0.11405	0.004590
0.06471	-0.12452	0.004580
0.06808	-0.13491	0.004570
0.07152	-0.14515	0.004560
0.07505	-0.15538	0.004560
0.07864	-0.16589	0.004550
0.08229	-0.17622	0.004550
0.08599	-0.18615	0.004540
0.08974	-0.19566	0.004530
0.09352	-0.20492	0.004520
0.09734	-0.21409	0.004520
0.10117	-0.22321	0.004520
0.10501	-0.23291	0.004520
0.10885	-0.24263	0.004520
0.11294	-0.25238	0.004530
0.11729	-0.26289	0.004530
0.12190	-0.27352	0.004530
0.12680	-0.28471	0.004530
0.13199	-0.29593	0.004520
0.13749	-0.30684	0.004510
0.14332	-0.31765	0.004500
0.14948	-0.32777	0.004480
0.15600	-0.33712	0.004460
0.16288	-0.34586	0.004430
0.17013	-0.35383	0.004400
0.17777	-0.36074	0.004360
0.18582	-0.36527	0.004300
0.19428	-0.36584	0.004220
0.20315	-0.36438	0.004160
0.21246	-0.36418	0.004120
0.22220	-0.36666	0.004100
0.23238	-0.37061	0.004090
0.24301	-0.37472	0.004070
0.25409	-0.37899	0.004050
0.26561	-0.38294	0.004020
0.27759	-0.38620	0.004000
0.29000	-0.38806	0.003960
0.30285	-0.38761	0.003910
0.31612	-0.38504	0.003850
0.32980	-0.38074	0.003790
0.34387	-0.37397	0.003710
0.35833	-0.36318	0.003620
0.37314	-0.34858	0.003520
0.38828	-0.33216	0.003420
0.40372	-0.31562	0.003340
0.41943	-0.30042	0.003270
0.43539	-0.28737	0.003230
0.45156	-0.27625	0.003190
0.46789	-0.26670	0.003160
0.48435	-0.25845	0.003140
0.50090	-0.24876	0.003080
0.51751	-0.23318	0.002980
0.53412	-0.21382	0.002890
0.55071	-0.19498	0.002810
0.56724	-0.17714	0.002740
0.58366	-0.16053	0.002690
0.59993	-0.14390	0.002620
0.61602	-0.12476	0.002520
0.63188	-0.10109	0.002400
0.64748	-0.07232	0.002240
0.66279	-0.03889	0.002050
0.67779	-0.00204	0.001860
0.69246	0.03617	0.001670
0.70678	0.07336	0.001490
0.72073	0.10827	0.001330
0.73429	0.14173	0.001180
0.74746	0.17299	0.001040
0.76023	0.20135	0.000930
0.77261	0.22617	0.000860
0.78456	0.24702	0.000800
0.79611	0.26488	0.000770
0.80722	0.27999	0.000740
0.81791	0.29282	0.000730
0.82816	0.30361	0.000730
0.83800	0.31256	0.000740
0.84741	0.31981	0.000750
0.85639	0.32554	0.000770
0.86497	0.32990	0.000800
0.87314	0.33304	0.000830
0.88091	0.33513	0.000870
0.88830	0.33630	0.000900
0.89530	0.33673	0.000940
0.90195	0.33670	0.000970
0.90824	0.33630	0.001010
0.91419	0.33550	0.001040
0.91982	0.33432	0.001080
0.92514	0.33272	0.001120
0.93016	0.33079	0.001150
0.93489	0.32855	0.001190
0.93935	0.32611	0.001230
0.94355	0.32333	0.001260
0.94751	0.32071	0.001300
0.95123	0.31744	0.001340
0.95494	0.31375	0.001380
0.95862	0.31030	0.001420
0.96223	0.30630	0.001460
0.96573	0.30216	0.001500
0.96909	0.29772	0.001540
0.97229	0.29320	0.001580
0.97532	0.28852	0.001630
0.97814	0.28378	0.001670
0.98077	0.27899	0.001710
0.98319	0.27413	0.001760
0.98540	0.26936	0.001800
0.98742	0.26460	0.001850
0.98924	0.25987	0.001890
0.99088	0.25517	0.001940
0.99235	0.25056	0.001990
0.99366	0.24603	0.002040
0.99483	0.24133	0.002090
0.99587	0.23678	0.002150
0.99678	0.23207	0.002220
0.99759	0.22702	0.002290
0.99830	0.22232	0.002410
0.99892	0.21710	0.002710
0.99947	0.21401	0.003760
0.99995	0.21389	0.003760

WING SECTION 7   Y/BO2 0.814 (Y = 620. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	1.00716	-0.000360
0.00002	1.00348	0.001010
0.00005	0.99403	0.001330
0.00012	0.98139	0.001660
0.00020	0.96603	0.001980
0.00031	0.94778	0.002290
0.00044	0.92677	0.002600
0.00061	0.90310	0.002890
0.00080	0.87700	0.003160
0.00102	0.84854	0.003430
0.00126	0.81771	0.003690
0.00154	0.78494	0.003930
0.00184	0.75047	0.004160
0.00218	0.71443	0.004370
0.00255	0.67716	0.004560
0.00294	0.63913	0.004730
0.00336	0.60050	0.004880
0.00381	0.56171	0.005000
0.00429	0.52338	0.005110
0.00479	0.48536	0.005210
0.00532	0.44784	0.005290
0.00586	0.41096	0.005370
0.00643	0.37453	0.005450
0.00702	0.33897	0.005550
0.00762	0.30252	0.005650
0.00762	0.30252	0.005550
0.00822	0.26769	0.005670
0.00887	0.23271	0.005760
0.00958	0.19415	0.005880
0.01035	0.15374	0.006000
0.01118	0.10966	0.006150
0.01208	0.06271	0.006300
0.01305	0.01209	0.006470
0.01410	-0.04312	0.006660
0.01523	-0.10213	0.006840
0.01645	-0.16507	0.007020
0.01777	-0.23193	0.007210
0.01918	-0.30282	0.007370
0.02070	-0.37573	0.007480
0.02234	-0.44817	0.007540
0.02409	-0.51869	0.007540
0.02596	-0.58477	0.007490
0.02796	-0.64552	0.007400
0.03008	-0.70017	0.007290
0.03232	-0.74815	0.007170
0.03470	-0.79104	0.007060
0.03720	-0.82904	0.006960
0.03982	-0.86376	0.006870
0.04256	-0.89519	0.006780
0.04541	-0.92372	0.006710
0.04838	-0.95053	0.006630
0.05146	-0.97487	0.006560
0.05465	-0.99753	0.006490
0.05794	-1.01797	0.006420
0.06132	-1.03673	0.006350
0.06478	-1.05374	0.006280
0.06832	-1.06846	0.006210
0.07194	-1.08143	0.006130
0.07562	-1.09185	0.006050
0.07935	-1.09987	0.005970
0.08312	-1.10602	0.005890
0.08692	-1.11047	0.005810
0.09075	-1.11309	0.005740
0.09459	-1.11404	0.005660
0.09843	-1.11320	0.005580
0.10227	-1.11122	0.005520
0.10611	-1.10860	0.005460
0.11020	-1.10546	0.005400
0.11454	-1.10184	0.005340
0.11915	-1.09664	0.005280
0.12404	-1.08993	0.005210
0.12923	-1.08211	0.005140
0.13472	-1.07321	0.005080
0.14053	-1.06362	0.005010
0.14667	-1.05347	0.004950
0.15316	-1.04313	0.004900
0.16001	-1.03290	0.004850
0.16724	-1.02261	0.004790
0.17485	-1.01273	0.004770
0.18286	-1.00818	0.004790
0.19127	-1.00633	0.004760
0.20011	-1.00030	0.004710
0.20938	-0.99371	0.004670
0.21908	-0.98943	0.004660
0.22923	-0.98681	0.004640
0.23983	-0.98522	0.004620
0.25089	-0.98372	0.004590
0.26239	-0.98164	0.004560
0.27435	-0.97775	0.004510
0.28675	-0.97059	0.004430
0.29960	-0.95848	0.004340
0.31288	-0.94117	0.004230
0.32657	-0.92121	0.004130
0.34068	-0.90274	0.004090
0.35518	-0.88984	0.004090
0.37005	-0.88370	0.004100
0.38526	-0.88074	0.004070
0.40078	-0.87278	0.003930
0.41659	-0.84328	0.003520
0.43266	-0.77482	0.003010
0.44895	-0.68828	0.002840
0.46542	-0.62792	0.002960
0.48203	-0.60393	0.003110
0.49875	-0.59953	0.003230
0.51553	-0.60061	0.003280
0.53234	-0.59623	0.003240
0.54914	-0.57310	0.003080
0.56586	-0.53429	0.002880
0.58248	-0.49280	0.002710
0.59896	-0.45344	0.002570
0.61525	-0.41787	0.002460
0.63134	-0.38738	0.002400
0.64719	-0.36302	0.002380
0.66276	-0.34421	0.002380
0.67804	-0.32939	0.002390
0.69299	-0.31598	0.002370
0.70758	-0.30031	0.002330
0.72179	-0.28182	0.002270
0.73561	-0.26383	0.002220
0.74901	-0.24842	0.002200
0.76198	-0.23535	0.002190
0.77453	-0.22419	0.002180
0.78664	-0.21428	0.002170
0.79830	-0.20469	0.002160
0.80951	-0.19476	0.002130
0.82027	-0.18400	0.002090
0.83057	-0.17200	0.002040
0.84044	-0.15855	0.001980
0.84985	-0.14385	0.001900
0.85883	-0.12806	0.001820
0.86739	-0.11156	0.001740
0.87553	-0.09468	0.001650
0.88326	-0.07774	0.001560
0.89060	-0.06108	0.001470
0.89756	-0.04494	0.001390
0.90415	-0.02958	0.001320
0.91040	-0.01519	0.001250
0.91630	-0.00144	0.001180
0.92188	0.01183	0.001120
0.92715	0.02451	0.001050
0.93212	0.03661	0.000990
0.93680	0.04804	0.000930
0.94121	0.05902	0.000880
0.94537	0.06894	0.000820
0.94928	0.07910	0.000780
0.95296	0.08766	0.000740
0.95664	0.09610	0.000680
0.96028	0.10572	0.000630
0.96384	0.11415	0.000590
0.96728	0.12254	0.000550
0.97058	0.13038	0.000510
0.97372	0.13781	0.000470
0.97667	0.14467	0.000440
0.97941	0.15102	0.000400
0.98195	0.15692	0.000380
0.98428	0.16212	0.000350
0.98640	0.16693	0.000330
0.98832	0.17115	0.000310
0.99005	0.17489	0.000290
0.99160	0.17825	0.000280
0.99299	0.18106	0.000270
0.99422	0.18358	0.000260
0.99531	0.18572	0.000260
0.99626	0.18741	0.000270
0.99711	0.18886	0.000270
0.99785	0.19005	0.000280
0.99850	0.19113	0.000330
0.99907	0.19157	0.000430
0.99957	0.19354	0.000780

WING SECTION 7   Y/BO2 0.814 (Y = 620. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	1.01390	0.000620
0.00001	1.01569	-0.000340
0.00005	1.01731	0.000050
0.00012	1.01527	0.000460
0.00022	1.00943	0.000870
0.00037	0.99964	0.001280
0.00055	0.98594	0.001690
0.00076	0.96818	0.002100
0.00101	0.94645	0.002490
0.00129	0.92110	0.002870
0.00162	0.89235	0.003230
0.00198	0.86038	0.003560
0.00237	0.82590	0.003870
0.00280	0.78921	0.004140
0.00327	0.75107	0.004380
0.00377	0.71192	0.004590
0.00431	0.67231	0.004750
0.00487	0.63333	0.004870
0.00547	0.59504	0.004960
0.00609	0.55832	0.004990
0.00674	0.52379	0.005000
0.00741	0.49131	0.005000
0.00810	0.46084	0.004980
0.00882	0.43249	0.004970
0.00954	0.40482	0.004970
0.01029	0.37817	0.004960
0.01110	0.35168	0.004980
0.01197	0.32405	0.005010
0.01290	0.29593	0.005030
0.01389	0.26787	0.005060
0.01495	0.23890	0.005100
0.01609	0.20921	0.005130
0.01730	0.17987	0.005150
0.01858	0.15072	0.005150
0.01995	0.12322	0.005130
0.02141	0.09750	0.005090
0.02296	0.07389	0.005050
0.02459	0.05256	0.005000
0.02633	0.03309	0.004960
0.02815	0.01519	0.004920
0.03007	-0.00225	0.004920
0.03210	-0.01967	0.004910
0.03422	-0.03657	0.004910
0.03644	-0.05268	0.004880
0.03877	-0.06720	0.004860
0.04121	-0.08106	0.004850
0.04374	-0.09444	0.004830
0.04638	-0.10690	0.004810
0.04912	-0.11922	0.004800
0.05196	-0.13130	0.004790
0.05491	-0.14290	0.004780
0.05794	-0.15374	0.004760
0.06108	-0.16362	0.004730
0.06430	-0.17252	0.004700
0.06762	-0.18029	0.004670
0.07101	-0.18816	0.004660
0.07448	-0.19714	0.004670
0.07802	-0.20652	0.004660
0.08162	-0.21516	0.004640
0.08528	-0.22300	0.004620
0.08900	-0.23072	0.004610
0.09276	-0.23841	0.004600
0.09655	-0.24614	0.004600
0.10037	-0.25386	0.004590
0.10421	-0.26204	0.004590
0.10806	-0.27029	0.004590
0.11214	-0.27857	0.004580
0.11648	-0.28745	0.004580
0.12109	-0.29687	0.004580
0.12598	-0.30624	0.004570
0.13117	-0.31582	0.004570
0.13666	-0.32541	0.004560
0.14247	-0.33451	0.004540
0.14863	-0.34340	0.004520
0.15512	-0.35147	0.004490
0.16198	-0.35851	0.004460
0.16922	-0.36504	0.004430
0.17684	-0.37109	0.004400
0.18486	-0.37501	0.004330
0.19329	-0.37503	0.004260
0.20213	-0.37268	0.004190
0.21141	-0.37189	0.004160
0.22111	-0.37376	0.004140
0.23126	-0.37718	0.004130
0.24185	-0.38144	0.004110
0.25289	-0.38591	0.004100
0.26437	-0.39027	0.004080
0.27630	-0.39417	0.004050
0.28868	-0.39664	0.004020
0.30148	-0.39687	0.003970
0.31471	-0.39521	0.003920
0.32835	-0.39226	0.003860
0.34239	-0.38766	0.003800
0.35681	-0.37994	0.003720
0.37160	-0.36887	0.003630
0.38670	-0.35592	0.003550
0.40212	-0.34257	0.003470
0.41781	-0.33011	0.003420
0.43375	-0.31942	0.003370
0.44990	-0.31024	0.003340
0.46622	-0.30201	0.003310
0.48268	-0.29441	0.003270
0.49924	-0.28532	0.003210
0.51585	-0.27082	0.003120
0.53248	-0.25213	0.003020
0.54909	-0.23303	0.002930
0.56563	-0.21438	0.002850
0.58208	-0.19655	0.002780
0.59838	-0.17850	0.002700
0.61450	-0.15786	0.002590
0.63040	-0.13262	0.002450
0.64605	-0.10220	0.002280
0.66140	-0.06710	0.002080
0.67645	-0.02862	0.001870
0.69115	0.01117	0.001670
0.70551	0.04979	0.001490
0.71949	0.08597	0.001320
0.73310	0.12055	0.001160
0.74631	0.15290	0.001020
0.75912	0.18233	0.000900
0.77153	0.20820	0.000820
0.78354	0.23008	0.000760
0.79513	0.24885	0.000720
0.80630	0.26480	0.000700
0.81704	0.27839	0.000680
0.82736	0.28988	0.000680
0.83726	0.29950	0.000690
0.84674	0.30738	0.000700
0.85580	0.31370	0.000720
0.86445	0.31862	0.000750
0.87270	0.32229	0.000780
0.88055	0.32489	0.000820
0.88801	0.32655	0.000850
0.89509	0.32742	0.000890
0.90181	0.32778	0.000930
0.90818	0.32778	0.000960
0.91421	0.32734	0.001000
0.91991	0.32651	0.001030
0.92530	0.32525	0.001070
0.93039	0.32364	0.001110
0.93519	0.32169	0.001150
0.93971	0.31957	0.001190
0.94398	0.31700	0.001220
0.94799	0.31468	0.001260
0.95177	0.31159	0.001300
0.95554	0.30805	0.001340
0.95927	0.30490	0.001380
0.96292	0.30110	0.001420
0.96645	0.29722	0.001460
0.96983	0.29310	0.001510
0.97304	0.28880	0.001550
0.97606	0.28444	0.001590
0.97888	0.28001	0.001640
0.98148	0.27551	0.001680
0.98387	0.27110	0.001720
0.98604	0.26670	0.001760
0.98801	0.26231	0.001810
0.98979	0.25797	0.001850
0.99138	0.25366	0.001900
0.99279	0.24936	0.001950
0.99405	0.24527	0.002000
0.99517	0.24102	0.002050
0.99616	0.23677	0.002110
0.99703	0.23244	0.002180
0.99779	0.22786	0.002260
0.99845	0.22352	0.002380
0.99904	0.21874	0.002690
0.99955	0.21604	0.003750
0.99999	0.21596	0.003750

WING SECTION 8   Y/BO2 0.945 (Y = 720. mm) UPPER SURFACE		
XOC	CP	CFprime
0.00000	0.99027	-0.001290
0.00001	0.99009	0.000090
0.00004	0.98790	0.000470
0.00009	0.98253	0.000830
0.00017	0.97426	0.001190
0.00027	0.96303	0.001540
0.00040	0.94893	0.001870
0.00055	0.93212	0.002190
0.00074	0.91272	0.002500
0.00094	0.89078	0.002800
0.00118	0.86649	0.003070
0.00145	0.84019	0.003340
0.00175	0.81181	0.003590
0.00207	0.78186	0.003810
0.00242	0.75058	0.004020
0.00280	0.71806	0.004210
0.00321	0.68512	0.004390
0.00365	0.65123	0.004540
0.00411	0.61718	0.004660
0.00460	0.58367	0.004770
0.00510	0.55011	0.004870
0.00563	0.51686	0.004970
0.00618	0.48382	0.005070
0.00675	0.45133	0.005170
0.00733	0.41756	0.005300
0.00733	0.41756	0.005180
0.00792	0.38507	0.005320
0.00856	0.35236	0.005420
0.00925	0.31629	0.005540
0.01001	0.27846	0.005670
0.01082	0.23711	0.005810
0.01169	0.19335	0.005960
0.01264	0.14604	0.006140
0.01366	0.09469	0.006320
0.01476	0.04003	0.006510
0.01594	-0.01877	0.006700
0.01721	-0.08056	0.006870
0.01857	-0.14578	0.007030
0.02004	-0.21281	0.007150
0.02162	-0.27933	0.007210
0.02331	-0.34425	0.007230
0.02511	-0.40542	0.007190
0.02703	-0.46171	0.007120
0.02908	-0.51256	0.007030
0.03124	-0.55817	0.006940
0.03352	-0.59957	0.006880
0.03592	-0.63834	0.006820
0.03844	-0.67457	0.006760
0.04108	-0.70793	0.006710
0.04383	-0.74005	0.006680
0.04670	-0.77061	0.006620
0.04967	-0.79772	0.006550
0.05274	-0.82325	0.006500
0.05592	-0.84734	0.006450
0.05919	-0.86953	0.006400
0.06255	-0.89034	0.006350
0.06599	-0.90864	0.006270
0.06951	-0.92432	0.006210
0.07309	-0.93867	0.006140
0.07674	-0.95059	0.006060
0.08043	-0.95933	0.005980
0.08416	-0.96647	0.005910
0.08793	-0.97202	0.005840
0.09172	-0.97582	0.005760
0.09551	-0.97742	0.005680
0.09932	-0.97727	0.005600
0.10313	-0.97616	0.005540
0.10718	-0.97486	0.005500
0.11148	-0.97407	0.005440
0.11605	-0.97137	0.005370
0.12090	-0.96690	0.005300
0.12604	-0.96142	0.005230
0.13149	-0.95467	0.005160
0.13726	-0.94739	0.005100
0.14336	-0.93906	0.005030
0.14981	-0.93000	0.004950
0.15662	-0.91954	0.004830
0.16379	-0.90188	0.004560
0.17136	-0.86741	0.004130
0.17932	-0.81253	0.003710
0.18769	-0.74707	0.003560
0.19648	-0.68950	0.003680
0.20570	-0.65753	0.003940
0.21536	-0.65451	0.004190
0.22546	-0.66914	0.004410
0.23601	-0.69053	0.004550
0.24702	-0.71081	0.004600
0.25848	-0.72476	0.004580
0.27039	-0.72988	0.004500
0.28275	-0.72297	0.004340
0.29555	-0.70137	0.004150
0.30877	-0.67243	0.004010
0.32242	-0.64726	0.003950
0.33648	-0.63146	0.003950
0.35094	-0.62197	0.003930
0.36577	-0.61239	0.003890
0.38094	-0.59937	0.003820
0.39643	-0.58110	0.003720
0.41220	-0.55936	0.003610
0.42824	-0.53663	0.003520
0.44449	-0.51431	0.003440
0.46094	-0.49325	0.003370
0.47754	-0.47386	0.003310
0.49425	-0.45652	0.003270
0.51104	-0.44157	0.003240
0.52786	-0.42627	0.003180
0.54466	-0.40653	0.003080
0.56142	-0.38215	0.002960
0.57808	-0.35503	0.002840
0.59461	-0.32739	0.002720
0.61098	-0.30126	0.002630
0.62714	-0.27801	0.002560
0.64307	-0.25870	0.002520
0.65873	-0.24315	0.002500
0.67410	-0.23016	0.002480
0.68915	-0.21789	0.002440
0.70384	-0.20443	0.002390
0.71816	-0.18913	0.002330
0.73209	-0.17381	0.002270
0.74561	-0.16026	0.002230
0.75871	-0.14855	0.002200
0.77138	-0.13849	0.002170
0.78362	-0.12954	0.002150
0.79541	-0.12131	0.002130
0.80675	-0.11347	0.002110
0.81765	-0.10552	0.002080
0.82809	-0.09714	0.002040
0.83809	-0.08828	0.002000
0.84765	-0.07891	0.001950
0.85678	-0.06905	0.001890
0.86548	-0.05871	0.001830
0.87377	-0.04819	0.001770
0.88165	-0.03766	0.001720
0.88914	-0.02711	0.001660
0.89624	-0.01673	0.001610
0.90298	-0.00683	0.001560
0.90937	0.00254	0.001510
0.91541	0.01166	0.001460
0.92112	0.02056	0.001410
0.92652	0.02927	0.001360
0.93161	0.03759	0.001320
0.93642	0.04566	0.001270
0.94095	0.05361	0.001230
0.94523	0.06069	0.001190
0.94925	0.06839	0.001150
0.95303	0.07465	0.001120
0.95682	0.08105	0.001070
0.96055	0.08880	0.001030
0.96420	0.09552	0.001000
0.96772	0.10241	0.000960
0.97108	0.10890	0.000930
0.97426	0.11522	0.000890
0.97724	0.12105	0.000860
0.97999	0.12631	0.000830
0.98253	0.13161	0.000800
0.98484	0.13623	0.000770
0.98694	0.14042	0.000750
0.98883	0.14421	0.000730
0.99052	0.14770	0.000720
0.99203	0.15056	0.000710
0.99336	0.15298	0.000690
0.99454	0.15558	0.000690
0.99558	0.15721	0.000700
0.99649	0.15849	0.000700
0.99728	0.15980	0.000700
0.99798	0.16088	0.000710
0.99858	0.16168	0.000780
0.99910	0.16173	0.000930
0.99956	0.16304	0.001460

WING SECTION 8   Y/BO2 0.945 (Y = 720. mm) LOWER SURFACE		
XOC	CP	CFprime
0.00000	0.98813	0.001570
0.00002	0.98581	0.000670
0.00006	0.97884	0.001100
0.00014	0.96773	0.001540
0.00025	0.95262	0.001990
0.00039	0.93337	0.002440
0.00057	0.91004	0.002880
0.00078	0.88242	0.003330
0.00103	0.85061	0.003770
0.00132	0.81472	0.004190
0.00164	0.77509	0.004590
0.00200	0.73239	0.004970
0.00240	0.68656	0.005310
0.00283	0.63887	0.005600
0.00330	0.58975	0.005860
0.00381	0.53978	0.006070
0.00435	0.48990	0.006240
0.00493	0.44062	0.006350
0.00554	0.39344	0.006400
0.00618	0.34857	0.006400
0.00685	0.30652	0.006350
0.00754	0.26822	0.006270
0.00826	0.23349	0.006190
0.00900	0.20119	0.006140
0.00976	0.16982	0.006140
0.01054	0.14003	0.006060
0.01137	0.11080	0.006060
0.01227	0.08020	0.006070
0.01322	0.04967	0.006060
0.01424	0.01930	0.006070
0.01532	-0.01233	0.006110
0.01648	-0.04441	0.006120
0.01770	-0.07560	0.006100
0.01901	-0.10569	0.006060
0.02039	-0.13373	0.006000
0.02185	-0.15936	0.005910
0.02340	-0.18174	0.005810
0.02504	-0.20129	0.005720
0.02676	-0.21866	0.005630
0.02858	-0.23378	0.005570
0.03048	-0.24818	0.005530
0.03248	-0.26177	0.005480
0.03458	-0.27424	0.005450
0.03677	-0.28677	0.005420
0.03906	-0.29776	0.005370
0.04145	-0.30753	0.005320
0.04394	-0.31661	0.005280
0.04652	-0.32476	0.005240
0.04921	-0.33281	0.005210
0.05198	-0.34018	0.005180
0.05486	-0.34741	0.005140
0.05783	-0.35395	0.005100
0.06090	-0.35923	0.005050
0.06405	-0.36312	0.004990
0.06729	-0.36592	0.004950
0.07062	-0.36953	0.004910
0.07402	-0.37289	0.004880
0.07750	-0.37622	0.004860
0.08105	-0.38066	0.004850
0.08466	-0.38490	0.004820
0.08833	-0.38864	0.004790
0.09206	-0.39168	0.004760
0.09583	-0.39467	0.004740
0.09964	-0.39761	0.004720
0.10349	-0.40092	0.004700
0.10733	-0.40439	0.004680
0.11142	-0.40799	0.004670
0.11576	-0.41234	0.004660
0.12037	-0.41687	0.004630
0.12525	-0.42051	0.004610
0.13043	-0.42400	0.004580
0.13591	-0.42734	0.004550
0.14171	-0.42941	0.004510
0.14785	-0.43073	0.004460
0.15433	-0.43077	0.004410
0.16117	-0.42914	0.004350
0.16838	-0.42676	0.004300
0.17597	-0.42373	0.004250
0.18396	-0.41849	0.004170
0.19236	-0.40964	0.004070
0.20117	-0.39821	0.003980
0.21040	-0.38795	0.003930
0.22006	-0.38068	0.003900
0.23016	-0.37546	0.003880
0.24070	-0.37153	0.003870
0.25169	-0.36881	0.003860
0.26312	-0.36691	0.003840
0.27499	-0.36534	0.003830
0.28730	-0.36366	0.003810
0.30004	-0.36053	0.003770
0.31321	-0.35551	0.003730
0.32678	-0.35003	0.003700
0.34076	-0.34512	0.003660
0.35512	-0.33977	0.003630
0.36985	-0.33346	0.003580
0.38490	-0.32673	0.003540
0.40027	-0.32041	0.003510
0.41591	-0.31524	0.003490
0.43181	-0.31147	0.003470
0.44793	-0.30855	0.003460
0.46423	-0.30573	0.003440
0.48067	-0.30251	0.003420
0.49722	-0.29788	0.003370
0.51384	-0.28942	0.003300
0.53048	-0.27644	0.003210
0.54710	-0.26076	0.003120
0.56367	-0.24385	0.003030
0.58013	-0.22647	0.002940
0.59647	-0.20861	0.002860
0.61263	-0.18914	0.002750
0.62858	-0.16624	0.002620
0.64428	-0.13909	0.002470
0.65970	-0.10822	0.002300
0.67480	-0.07454	0.002110
0.68958	-0.03930	0.001920
0.70400	-0.00403	0.001740
0.71806	0.02961	0.001580
0.73173	0.06211	0.001420
0.74501	0.09265	0.001280
0.75788	0.12032	0.001170
0.77036	0.14451	0.001090
0.78243	0.16451	0.001040
0.79408	0.18145	0.001000
0.80532	0.19559	0.000980
0.81613	0.20745	0.000970
0.82652	0.21739	0.000970
0.83649	0.22558	0.000970
0.84603	0.23217	0.000990
0.85516	0.23742	0.001000
0.86389	0.24147	0.001030
0.87221	0.24445	0.001050
0.88013	0.24656	0.001080
0.88767	0.24787	0.001110
0.89483	0.24854	0.001140
0.90163	0.24881	0.001170
0.90808	0.24881	0.001200
0.91418	0.24854	0.001230
0.91996	0.24793	0.001260
0.92543	0.24707	0.001280
0.93059	0.24598	0.001310
0.93547	0.24464	0.001340
0.94007	0.24328	0.001370
0.94440	0.24148	0.001390
0.94849	0.24025	0.001420
0.95234	0.23803	0.001460
0.95618	0.23547	0.001480
0.95998	0.23367	0.001500
0.96368	0.23117	0.001530
0.96726	0.22878	0.001560
0.97067	0.22617	0.001590
0.97390	0.22340	0.001620
0.97692	0.22077	0.001650
0.97972	0.21811	0.001680
0.98229	0.21533	0.001700
0.98464	0.21274	0.001730
0.98677	0.21015	0.001760
0.98869	0.20755	0.001790
0.99041	0.20495	0.001820
0.99194	0.20223	0.001860
0.99329	0.19981	0.001890
0.99449	0.19724	0.001930
0.99555	0.19452	0.001980
0.99647	0.19173	0.002020
0.99728	0.18911	0.002080
0.99799	0.18593	0.002150
0.99860	0.18269	0.002250
0.99913	0.18009	0.002540
0.99960	0.17837	0.003620
0.99996	0.09943	0.000710


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 perpendicular to cell trailing edge (downstream)	
* BO2              Semispan   (762.0 mm)
