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


Date:  [Due 28 APR 2006]


PARTICIPANT INFORMATION
-----------------------
               Name: Christopher Rumsey, S. Melissa Rivers, Joe Morrison
              Email: c.l.rumsey@nasa.gov
              Phone: (757) 864-2165
            Address: NASA Langley Research Center
            Address: MS 128
            Address: Hampton, VA  23681
            Address:  
            Address:  
            Address:  


SOLVER INFORMATION
--------------------
        Method Name: OVERFLOW
    Basic Algorithm: full N-S, finite volume, upwind-biased, Roe FDS
   Turbulence Model: Menter SST k-omega
      Miscellaneous:  


GRID INFORMATION
--------------------
Grid-Generator Name: Grids were supplied by DPW committee
          Grid Type: structured overset



MEDIUM GRID SIZE            WB       WBF
----------------------------------------
              Zones:        12        12
        Field Nodes:   7985236   8020348
        Field Cells:   7689088   7723136
     Boundary Nodes:
     Boundary Faces:
   BL 1st-Cell Size:   0.00038   0.00038
 BL Max-Growth Rate:
           BL Cells:
      Miscellaneous:



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

WING/BODY

 GRID_SIZE      MACH     ALPHA
  7985236.      0.75     0.373

WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9981     -0.1447
   0.9958     -0.1078
   0.9933     -0.0757
   0.9906     -0.0474
   0.9878     -0.0220
   0.9848      0.0010
   0.9815      0.0218
   0.9781      0.0408
   0.9744      0.0581
   0.9705      0.0738
   0.9664      0.0877
   0.9620      0.1000
   0.9573      0.1105
   0.9523      0.1208
   0.9471      0.1327
   0.9415      0.1410
   0.9356      0.1501
   0.9293      0.1583
   0.9227      0.1660
   0.9157      0.1726
   0.9083      0.1780
   0.9006      0.1821
   0.8924      0.1854
   0.8837      0.1874
   0.8747      0.1887
   0.8652      0.1890
   0.8552      0.1884
   0.8448      0.1863
   0.8339      0.1830
   0.8225      0.1791
   0.8107      0.1742
   0.7984      0.1677
   0.7856      0.1579
   0.7724      0.1438
   0.7588      0.1241
   0.7447      0.0990
   0.7303      0.0682
   0.7154      0.0326
   0.7002     -0.0070
   0.6845     -0.0460
   0.6685     -0.0818
   0.6521     -0.1169
   0.6354     -0.1506
   0.6183     -0.1864
   0.6010     -0.2224
   0.5984     -0.2278
   0.5834     -0.2596
   0.5656     -0.2954
   0.5476     -0.3257
   0.5294     -0.3480
   0.5110     -0.3422
   0.4926     -0.3243
   0.4742     -0.3056
   0.4558     -0.2921
   0.4374     -0.2862
   0.4193     -0.2813
   0.4012     -0.2766
   0.3834     -0.2756
   0.3626     -0.2748
   0.3658     -0.2763
   0.3485     -0.2682
   0.3315     -0.2524
   0.3149     -0.2409
   0.2986     -0.2341
   0.2827     -0.2286
   0.2673     -0.2211
   0.2523     -0.2108
   0.2377     -0.1972
   0.2236     -0.1829
   0.2100     -0.1715
   0.1969     -0.1654
   0.1843     -0.1622
   0.1722     -0.1594
   0.1606     -0.1540
   0.1407     -0.1372
   0.1494     -0.1458
   0.1388     -0.1353
   0.1286     -0.1227
   0.1190     -0.1088
   0.1098     -0.0936
   0.1010     -0.0773
   0.0927     -0.0600
   0.0849     -0.0413
   0.0775     -0.0209
   0.0705      0.0016
   0.0639      0.0262
   0.0578      0.0528
   0.0520      0.0814
   0.0466      0.1131
   0.0415      0.1486
   0.0389      0.1701
   0.0368      0.1870
   0.0325      0.2283
   0.0285      0.2737
   0.0248      0.3222
   0.0214      0.3729
   0.0183      0.4265
   0.0155      0.4814
   0.0130      0.5383
   0.0108      0.5962
   0.0088      0.6520
   0.0071      0.7067
   0.0056      0.7582
   0.0043      0.8057
   0.0032      0.8480
   0.0023      0.8837
   0.0016      0.9115
   0.0011      0.9332
   0.0007      0.9470
   0.0002      0.9550
   0.0004      0.9545
   0.0002      0.9551
   0.0001      0.9507
   0.0000      0.9436
   0.0000      0.9326
   0.0000      0.9194
   0.0001      0.9043
   0.0002      0.8869
   0.0003      0.8658
   0.0005      0.8400
   0.0007      0.8083
   0.0010      0.7673
   0.0013      0.7105
   0.0018      0.6454
   0.0024      0.5771
   0.0031      0.5006
   0.0039      0.4161
   0.0050      0.3235
   0.0062      0.2227
   0.0076      0.1153
   0.0092      0.0063
   0.0111     -0.1035
   0.0132     -0.2124
   0.0155     -0.3210
   0.0181     -0.4279
   0.0210     -0.5259
   0.0242     -0.6178
   0.0277     -0.6991
   0.0315     -0.7643
   0.0356     -0.8196
   0.0401     -0.8639
   0.0449     -0.8900
   0.0501     -0.9093
   0.0556     -0.9250
   0.0614     -0.9289
   0.0677     -0.9252
   0.0743     -0.9211
   0.0813     -0.9168
   0.0888     -0.9123
   0.0967     -0.9077
   0.1050     -0.9035
   0.1137     -0.9000
   0.1229     -0.8908
   0.1326     -0.8728
   0.1427     -0.8594
   0.1534     -0.8633
   0.1645     -0.8630
   0.1761     -0.8576
   0.1882     -0.8530
   0.2008     -0.8453
   0.2140     -0.8392
   0.2276     -0.8308
   0.2416     -0.8182
   0.2562     -0.8010
   0.2712     -0.7755
   0.2867     -0.7442
   0.3026     -0.7060
   0.3189     -0.6705
   0.3356     -0.6469
   0.3526     -0.6314
   0.3700     -0.6170
   0.3877     -0.6037
   0.4056     -0.5888
   0.4237     -0.5720
   0.4420     -0.5552
   0.4605     -0.5371
   0.4790     -0.5168
   0.4976     -0.4949
   0.5162     -0.4709
   0.5348     -0.4460
   0.5533     -0.4207
   0.5717     -0.3964
   0.5898     -0.3733
   0.6078     -0.3514
   0.6255     -0.3307
   0.6430     -0.3111
   0.6601     -0.2927
   0.6768     -0.2755
   0.6932     -0.2597
   0.7091     -0.2457
   0.7139     -0.2414
   0.7247     -0.2315
   0.7397     -0.2146
   0.7543     -0.2021
   0.7685     -0.1935
   0.7821     -0.1897
   0.7952     -0.1877
   0.8079     -0.1878
   0.8200     -0.1890
   0.8317     -0.1908
   0.8428     -0.1941
   0.8534     -0.1982
   0.8636     -0.2032
   0.8732     -0.2090
   0.8824     -0.2153
   0.8911     -0.2221
   0.8911     -0.2221
   0.8993     -0.2287
   0.9071     -0.2346
   0.9145     -0.2398
   0.9215     -0.2440
   0.9281     -0.2475
   0.9343     -0.2503
   0.9401     -0.2526
   0.9457     -0.2541
   0.9509     -0.2552
   0.9558     -0.2515
   0.9604     -0.2510
   0.9648     -0.2285
   0.9689     -0.2106
   0.9727     -0.1962
   0.9763     -0.1849
   0.9797     -0.1763
   0.9829     -0.1702
   0.9859     -0.1665
   0.9887     -0.1652
   0.9913     -0.1666
   0.9919     -0.1676
   0.9938     -0.1712
   0.9961     -0.1795
   0.9983     -0.1928

WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1296
   0.9958      0.1306
   0.9934      0.1337
   0.9907      0.1386
   0.9879      0.1452
   0.9849      0.1531
   0.9818      0.1621
   0.9784      0.1722
   0.9747      0.1831
   0.9709      0.1949
   0.9668      0.2076
   0.9624      0.2213
   0.9578      0.2361
   0.9529      0.2396
   0.9477      0.2439
   0.9422      0.2470
   0.9363      0.2506
   0.9301      0.2538
   0.9236      0.2568
   0.9166      0.2594
   0.9093      0.2616
   0.9016      0.2633
   0.8934      0.2644
   0.8849      0.2649
   0.8759      0.2645
   0.8664      0.2631
   0.8565      0.2608
   0.8461      0.2572
   0.8353      0.2523
   0.8239      0.2456
   0.8121      0.2373
   0.7999      0.2268
   0.7871      0.2132
   0.7739      0.1961
   0.7602      0.1749
   0.7461      0.1484
   0.7316      0.1163
   0.7167      0.0801
   0.7013      0.0419
   0.6855      0.0018
   0.6693     -0.0371
   0.6528     -0.0769
   0.6359     -0.1156
   0.6187     -0.1551
   0.6012     -0.1967
   0.5835     -0.2387
   0.5655     -0.2804
   0.5473     -0.3166
   0.5290     -0.3467
   0.5105     -0.3617
   0.4920     -0.3581
   0.4735     -0.3523
   0.4550     -0.3493
   0.4367     -0.3490
   0.4184     -0.3493
   0.4004     -0.3483
   0.3825     -0.3502
   0.3649     -0.3520
   0.3476     -0.3454
   0.3307     -0.3322
   0.3140     -0.3233
   0.2978     -0.3161
   0.2820     -0.3087
   0.2667     -0.3004
   0.2517     -0.2883
   0.2373     -0.2726
   0.2233     -0.2574
   0.2098     -0.2450
   0.1969     -0.2356
   0.1844     -0.2278
   0.1724     -0.2205
   0.1609     -0.2123
   0.1500     -0.2021
   0.1395     -0.1900
   0.1295     -0.1761
   0.1200     -0.1612
   0.1109     -0.1455
   0.1023     -0.1293
   0.0942     -0.1126
   0.0865     -0.0953
   0.0792     -0.0768
   0.0723     -0.0567
   0.0659     -0.0348
   0.0598     -0.0114
   0.0541      0.0133
   0.0487      0.0402
   0.0437      0.0698
   0.0390      0.1016
   0.0347      0.1363
   0.0306      0.1748
   0.0269      0.2162
   0.0235      0.2605
   0.0203      0.3081
   0.0174      0.3567
   0.0148      0.4081
   0.0125      0.4622
   0.0103      0.5156
   0.0085      0.5695
   0.0068      0.6212
   0.0054      0.6703
   0.0041      0.7157
   0.0031      0.7550
   0.0022      0.7872
   0.0015      0.8122
   0.0010      0.8289
   0.0006      0.8387
   0.0003      0.8389
   0.0002      0.8326
   0.0000      0.8221
   0.0000      0.8069
   0.0000      0.7886
   0.0001      0.7676
   0.0002      0.7437
   0.0003      0.7151
   0.0005      0.6796
   0.0007      0.6362
   0.0010      0.5804
   0.0014      0.5087
   0.0020      0.4301
   0.0027      0.3498
   0.0035      0.2646
   0.0045      0.1712
   0.0056      0.0690
   0.0070     -0.0374
   0.0085     -0.1431
   0.0103     -0.2507
   0.0122     -0.3614
   0.0144     -0.4687
   0.0169     -0.5745
   0.0196     -0.6833
   0.0226     -0.7960
   0.0258     -0.9101
   0.0294     -1.0057
   0.0333     -1.0750
   0.0375     -1.1307
   0.0420     -1.1751
   0.0468     -1.2072
   0.0519     -1.2355
   0.0574     -1.2612
   0.0633     -1.2782
   0.0745     -1.2940
   0.0695     -1.2886
   0.0761     -1.2956
   0.0831     -1.3001
   0.0905     -1.3024
   0.0983     -1.3016
   0.1066     -1.2985
   0.1153     -1.2922
   0.1244     -1.2795
   0.1340     -1.2571
   0.1441     -1.2247
   0.1547     -1.1803
   0.1657     -1.1195
   0.1773     -1.0564
   0.1893     -1.0057
   0.2019     -0.9765
   0.2149     -0.9501
   0.2285     -0.9127
   0.2425     -0.8633
   0.2570     -0.7779
   0.2719     -0.6895
   0.2874     -0.6594
   0.3032     -0.6503
   0.3195     -0.6403
   0.3361     -0.6323
   0.3531     -0.6262
   0.3704     -0.6184
   0.3880     -0.6096
   0.4059     -0.6005
   0.4240     -0.5912
   0.4423     -0.5818
   0.4607     -0.5725
   0.4793     -0.5635
   0.4978     -0.5549
   0.5164     -0.5466
   0.5349     -0.5385
   0.5534     -0.5306
   0.5717     -0.5228
   0.5899     -0.5148
   0.6078     -0.5066
   0.6255     -0.4978
   0.6429     -0.4872
   0.6600     -0.4741
   0.6767     -0.4591
   0.6930     -0.4421
   0.7090     -0.4229
   0.7244     -0.4025
   0.7395     -0.3824
   0.7540     -0.3640
   0.7681     -0.3472
   0.7817     -0.3321
   0.7948     -0.3191
   0.8074     -0.3074
   0.8196     -0.2956
   0.8236     -0.2912
   0.8312     -0.2829
   0.8423     -0.2687
   0.8529     -0.2526
   0.8630     -0.2349
   0.8726     -0.2163
   0.8818     -0.1964
   0.8905     -0.1759
   0.8988     -0.1545
   0.9066     -0.1326
   0.9140     -0.1106
   0.9210     -0.0889
   0.9276     -0.0679
   0.9339     -0.0480
   0.9398     -0.0289
   0.9453     -0.0117
   0.9506      0.0053
   0.9555      0.0187
   0.9602      0.0325
   0.9646      0.0260
   0.9687      0.0221
   0.9725      0.0205
   0.9762      0.0212
   0.9796      0.0238
   0.9828      0.0283
   0.9858      0.0346
   0.9886      0.0426
   0.9913      0.0526
   0.9938      0.0646
   0.9961      0.0787
   0.9983      0.0952

WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1373
   0.9959      0.1471
   0.9935      0.1569
   0.9910      0.1666
   0.9883      0.1762
   0.9853      0.1856
   0.9822      0.1948
   0.9789      0.2038
   0.9754      0.2126
   0.9717      0.2211
   0.9677      0.2294
   0.9634      0.2374
   0.9589      0.2452
   0.9541      0.2507
   0.9491      0.2570
   0.9437      0.2617
   0.9379      0.2668
   0.9319      0.2716
   0.9255      0.2764
   0.9187      0.2810
   0.9115      0.2852
   0.9039      0.2891
   0.8960      0.2926
   0.8875      0.2953
   0.8787      0.2975
   0.8694      0.2983
   0.8596      0.2978
   0.8494      0.2959
   0.8386      0.2919
   0.8274      0.2855
   0.8157      0.2765
   0.8036      0.2647
   0.7909      0.2501
   0.7777      0.2324
   0.7641      0.2109
   0.7500      0.1851
   0.7355      0.1550
   0.7204      0.1213
   0.7050      0.0856
   0.6891      0.0492
   0.6728      0.0120
   0.6561     -0.0241
   0.6390     -0.0618
   0.6216     -0.0989
   0.6040     -0.1370
   0.5860     -0.1745
   0.5679     -0.2118
   0.5495     -0.2476
   0.5311     -0.2789
   0.5125     -0.3020
   0.4939     -0.3170
   0.4753     -0.3269
   0.4567     -0.3361
   0.4383     -0.3440
   0.4200     -0.3505
   0.4019     -0.3561
   0.3840     -0.3604
   0.3663     -0.3616
   0.3490     -0.3597
   0.3321     -0.3536
   0.3155     -0.3457
   0.2993     -0.3384
   0.2835     -0.3307
   0.2682     -0.3201
   0.2534     -0.3064
   0.2390     -0.2906
   0.2252     -0.2741
   0.2118     -0.2585
   0.1989     -0.2447
   0.1866     -0.2324
   0.1748     -0.2205
   0.1634     -0.2081
   0.1526     -0.1946
   0.1423     -0.1806
   0.1324     -0.1660
   0.1230     -0.1514
   0.1141     -0.1368
   0.1057     -0.1222
   0.0977     -0.1076
   0.0901     -0.0929
   0.0829     -0.0778
   0.0762     -0.0621
   0.0698     -0.0463
   0.0638     -0.0306
   0.0581     -0.0141
   0.0528      0.0045
   0.0478      0.0251
   0.0431      0.0467
   0.0388      0.0701
   0.0347      0.0964
   0.0309      0.1244
   0.0274      0.1554
   0.0241      0.1912
   0.0211      0.2298
   0.0183      0.2723
   0.0157      0.3182
   0.0134      0.3654
   0.0113      0.4167
   0.0094      0.4699
   0.0076      0.5244
   0.0061      0.5792
   0.0048      0.6311
   0.0037      0.6804
   0.0027      0.7236
   0.0019      0.7596
   0.0016      0.7727
   0.0012      0.7863
   0.0007      0.8034
   0.0004      0.8087
   0.0002      0.8030
   0.0000      0.7892
   0.0000      0.7688
   0.0000      0.7431
   0.0001      0.7128
   0.0002      0.6745
   0.0005      0.6251
   0.0008      0.5643
   0.0012      0.4913
   0.0017      0.4091
   0.0024      0.3225
   0.0032      0.2335
   0.0043      0.1416
   0.0054      0.0454
   0.0068     -0.0530
   0.0083     -0.1539
   0.0101     -0.2538
   0.0120     -0.3566
   0.0142     -0.4608
   0.0165     -0.5614
   0.0192     -0.6670
   0.0220     -0.7888
   0.0252     -0.9266
   0.0286     -1.0525
   0.0323     -1.1359
   0.0363     -1.1760
   0.0405     -1.2064
   0.0451     -1.2307
   0.0500     -1.2495
   0.0552     -1.2610
   0.0607     -1.2679
   0.0666     -1.2750
   0.0729     -1.2796
   0.0795     -1.2804
   0.0865     -1.2802
   0.0939     -1.2784
   0.1018     -1.2761
   0.1100     -1.2729
   0.1187     -1.2688
   0.1278     -1.2637
   0.1375     -1.2576
   0.1475     -1.2503
   0.1581     -1.2419
   0.1691     -1.2329
   0.1807     -1.2227
   0.1927     -1.2114
   0.2053     -1.1855
   0.2183     -1.1405
   0.2318     -0.9586
   0.2458     -0.7509
   0.2603     -0.6076
   0.2753     -0.5962
   0.2907     -0.6023
   0.3065     -0.6147
   0.3228     -0.6291
   0.3394     -0.6426
   0.3564     -0.6543
   0.3737     -0.6622
   0.3913     -0.6692
   0.4092     -0.6726
   0.4273     -0.6752
   0.4455     -0.6757
   0.4639     -0.6746
   0.4824     -0.6728
   0.5009     -0.6706
   0.5194     -0.6684
   0.5379     -0.6664
   0.5563     -0.6644
   0.5746     -0.6620
   0.5927     -0.6582
   0.6105     -0.6514
   0.6281     -0.6397
   0.6454     -0.6241
   0.6624     -0.6048
   0.6790     -0.5801
   0.6952     -0.5511
   0.7110     -0.5197
   0.7264     -0.4879
   0.7413     -0.4569
   0.7557     -0.4277
   0.7697     -0.4001
   0.7832     -0.3737
   0.7961     -0.3486
   0.8086     -0.3244
   0.8206     -0.3010
   0.8321     -0.2780
   0.8431     -0.2552
   0.8536     -0.2324
   0.8636     -0.2096
   0.8732     -0.1866
   0.8823     -0.1640
   0.8909     -0.1422
   0.8991     -0.1209
   0.9069     -0.1004
   0.9132     -0.0832
   0.9142     -0.0805
   0.9212     -0.0615
   0.9278     -0.0435
   0.9340     -0.0266
   0.9399     -0.0108
   0.9455      0.0037
   0.9507      0.0172
   0.9556      0.0288
   0.9603      0.0398
   0.9646      0.0450
   0.9687      0.0504
   0.9726      0.0559
   0.9762      0.0615
   0.9796      0.0672
   0.9828      0.0728
   0.9858      0.0786
   0.9887      0.0843
   0.9913      0.0901
   0.9938      0.0959
   0.9961      0.1017
   0.9982      0.1075

WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1153
   0.9960      0.1266
   0.9936      0.1379
   0.9910      0.1492
   0.9883      0.1603
   0.9854      0.1712
   0.9823      0.1818
   0.9790      0.1922
   0.9755      0.2023
   0.9718      0.2120
   0.9678      0.2215
   0.9636      0.2307
   0.9591      0.2395
   0.9544      0.2463
   0.9493      0.2550
   0.9439      0.2603
   0.9382      0.2667
   0.9322      0.2723
   0.9258      0.2780
   0.9191      0.2835
   0.9119      0.2888
   0.9044      0.2938
   0.8965      0.2984
   0.8881      0.3025
   0.8793      0.3055
   0.8700      0.3078
   0.8603      0.3079
   0.8501      0.3065
   0.8394      0.3026
   0.8283      0.2960
   0.8166      0.2856
   0.8045      0.2734
   0.7919      0.2575
   0.7788      0.2388
   0.7653      0.2164
   0.7512      0.1901
   0.7368      0.1600
   0.7218      0.1275
   0.7064      0.0942
   0.6906      0.0605
   0.6744      0.0251
   0.6578     -0.0095
   0.6408     -0.0442
   0.6235     -0.0783
   0.6060     -0.1127
   0.5881     -0.1467
   0.5700     -0.1798
   0.5518     -0.2119
   0.5334     -0.2414
   0.5150     -0.2672
   0.4964     -0.2881
   0.4779     -0.3059
   0.4595     -0.3204
   0.4411     -0.3313
   0.4229     -0.3407
   0.4048     -0.3483
   0.3870     -0.3527
   0.3694     -0.3542
   0.3522     -0.3543
   0.3353     -0.3513
   0.3187     -0.3447
   0.3026     -0.3370
   0.2869     -0.3282
   0.2716     -0.3171
   0.2568     -0.3024
   0.2425     -0.2854
   0.2287     -0.2679
   0.2153     -0.2511
   0.2025     -0.2350
   0.1902     -0.2185
   0.1784     -0.2024
   0.1670     -0.1869
   0.1562     -0.1717
   0.1459     -0.1564
   0.1361     -0.1411
   0.1267     -0.1259
   0.1178     -0.1113
   0.1093     -0.0971
   0.1013     -0.0834
   0.0937     -0.0700
   0.0865     -0.0571
   0.0797     -0.0441
   0.0733     -0.0317
   0.0672     -0.0201
   0.0615     -0.0076
   0.0561      0.0063
   0.0511      0.0211
   0.0464      0.0361
   0.0419      0.0519
   0.0378      0.0700
   0.0339      0.0894
   0.0302      0.1112
   0.0269      0.1385
   0.0237      0.1682
   0.0208      0.2009
   0.0181      0.2374
   0.0156      0.2769
   0.0134      0.3229
   0.0113      0.3724
   0.0094      0.4246
   0.0077      0.4799
   0.0062      0.5357
   0.0049      0.5938
   0.0037      0.6491
   0.0027      0.7000
   0.0019      0.7436
   0.0012      0.7773
   0.0007      0.8003
   0.0004      0.8083
   0.0001      0.8015
   0.0000      0.7831
   0.0000      0.7558
   0.0001      0.7210
   0.0002      0.6752
   0.0005      0.6152
   0.0008      0.5434
   0.0013      0.4632
   0.0019      0.3808
   0.0027      0.2926
   0.0037      0.2023
   0.0047      0.1140
   0.0060      0.0231
   0.0074     -0.0702
   0.0090     -0.1672
   0.0108     -0.2632
   0.0128     -0.3607
   0.0150     -0.4587
   0.0174     -0.5592
   0.0201     -0.6731
   0.0230     -0.8109
   0.0261     -0.9616
   0.0296     -1.0858
   0.0333     -1.1561
   0.0373     -1.1805
   0.0416     -1.1997
   0.0461     -1.2116
   0.0510     -1.2188
   0.0562     -1.2194
   0.0617     -1.2177
   0.0676     -1.2175
   0.0739     -1.2151
   0.0805     -1.2099
   0.0874     -1.2035
   0.0948     -1.1968
   0.1026     -1.1903
   0.1108     -1.1838
   0.1195     -1.1771
   0.1286     -1.1716
   0.1382     -1.1656
   0.1483     -1.1580
   0.1588     -1.1502
   0.1698     -1.1424
   0.1813     -1.1338
   0.1933     -1.1248
   0.2058     -1.1104
   0.2188     -1.0786
   0.2323     -0.9398
   0.2463     -0.7613
   0.2608     -0.5998
   0.2757     -0.6080
   0.2911     -0.6266
   0.3069     -0.6460
   0.3231     -0.6655
   0.3397     -0.6822
   0.3567     -0.6960
   0.3740     -0.7068
   0.3916     -0.7162
   0.4094     -0.7233
   0.4275     -0.7285
   0.4457     -0.7320
   0.4641     -0.7333
   0.4825     -0.7337
   0.5011     -0.7341
   0.5196     -0.7348
   0.5380     -0.7363
   0.5564     -0.7385
   0.5747     -0.7411
   0.5927     -0.7426
   0.6106     -0.7411
   0.6282     -0.7318
   0.6455     -0.7124
   0.6625     -0.6849
   0.6791     -0.6534
   0.6953     -0.6190
   0.7111     -0.5825
   0.7264     -0.5458
   0.7413     -0.5104
   0.7557     -0.4769
   0.7697     -0.4446
   0.7831     -0.4131
   0.7961     -0.3831
   0.8086     -0.3543
   0.8205     -0.3267
   0.8320     -0.3002
   0.8430     -0.2745
   0.8535     -0.2496
   0.8635     -0.2253
   0.8730     -0.2016
   0.8821     -0.1788
   0.8907     -0.1570
   0.8989     -0.1361
   0.9067     -0.1161
   0.9141     -0.0970
   0.9211     -0.0789
   0.9277     -0.0617
   0.9339     -0.0458
   0.9398     -0.0306
   0.9454     -0.0175
   0.9506     -0.0036
   0.9556      0.0057
   0.9602      0.0163
   0.9646      0.0216
   0.9687      0.0273
   0.9726      0.0333
   0.9762      0.0394
   0.9796      0.0453
   0.9828      0.0512
   0.9858      0.0569
   0.9886      0.0625
   0.9913      0.0679
   0.9938      0.0733
   0.9961      0.0785
   0.9982      0.0837

WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1026
   0.9960      0.1158
   0.9936      0.1283
   0.9911      0.1405
   0.9884      0.1521
   0.9855      0.1634
   0.9824      0.1743
   0.9791      0.1847
   0.9757      0.1949
   0.9719      0.2046
   0.9680      0.2141
   0.9638      0.2231
   0.9593      0.2315
   0.9546      0.2389
   0.9496      0.2482
   0.9442      0.2540
   0.9385      0.2606
   0.9325      0.2665
   0.9262      0.2725
   0.9195      0.2782
   0.9123      0.2838
   0.9048      0.2893
   0.8969      0.2942
   0.8886      0.2986
   0.8798      0.3017
   0.8705      0.3042
   0.8608      0.3046
   0.8507      0.3033
   0.8400      0.2996
   0.8289      0.2927
   0.8173      0.2829
   0.8051      0.2705
   0.7925      0.2556
   0.7795      0.2376
   0.7659      0.2160
   0.7519      0.1908
   0.7374      0.1625
   0.7225      0.1321
   0.7071      0.1008
   0.6913      0.0689
   0.6750      0.0360
   0.6585      0.0032
   0.6415     -0.0294
   0.6242     -0.0622
   0.6067     -0.0941
   0.5889     -0.1261
   0.5708     -0.1567
   0.5526     -0.1864
   0.5343     -0.2144
   0.5159     -0.2407
   0.4974     -0.2646
   0.4789     -0.2859
   0.4605     -0.3043
   0.4422     -0.3180
   0.4240     -0.3286
   0.4060     -0.3366
   0.3883     -0.3424
   0.3708     -0.3457
   0.3536     -0.3462
   0.3367     -0.3448
   0.3202     -0.3408
   0.3041     -0.3343
   0.2884     -0.3248
   0.2732     -0.3129
   0.2584     -0.2985
   0.2441     -0.2820
   0.2303     -0.2646
   0.2170     -0.2468
   0.2042     -0.2287
   0.1919     -0.2105
   0.1801     -0.1924
   0.1688     -0.1748
   0.1580     -0.1576
   0.1477     -0.1407
   0.1379     -0.1241
   0.1285     -0.1079
   0.1196     -0.0918
   0.1111     -0.0761
   0.1031     -0.0609
   0.0955     -0.0464
   0.0883     -0.0334
   0.0815     -0.0214
   0.0751     -0.0097
   0.0690      0.0025
   0.0633      0.0151
   0.0579      0.0278
   0.0528      0.0410
   0.0480      0.0537
   0.0436      0.0669
   0.0394      0.0819
   0.0354      0.0981
   0.0318      0.1163
   0.0283      0.1386
   0.0252      0.1633
   0.0222      0.1912
   0.0194      0.2227
   0.0169      0.2564
   0.0145      0.2968
   0.0124      0.3418
   0.0104      0.3908
   0.0086      0.4440
   0.0070      0.4991
   0.0056      0.5587
   0.0043      0.6177
   0.0032      0.6753
   0.0023      0.7281
   0.0015      0.7729
   0.0009      0.8059
   0.0005      0.8277
   0.0001      0.8298
   0.0000      0.8147
   0.0000      0.7880
   0.0000      0.7508
   0.0002      0.7022
   0.0004      0.6350
   0.0008      0.5560
   0.0013      0.4734
   0.0020      0.3901
   0.0029      0.3026
   0.0038      0.2136
   0.0050      0.1260
   0.0063      0.0362
   0.0078     -0.0543
   0.0094     -0.1503
   0.0112     -0.2479
   0.0132     -0.3481
   0.0155     -0.4428
   0.0179     -0.5386
   0.0206     -0.6651
   0.0235     -0.8242
   0.0266     -0.9807
   0.0301     -1.0968
   0.0338     -1.1569
   0.0378     -1.1743
   0.0421     -1.1865
   0.0467     -1.1904
   0.0503     -1.1885
   0.0516     -1.1877
   0.0568     -1.1839
   0.0623     -1.1791
   0.0682     -1.1731
   0.0745     -1.1659
   0.0811     -1.1561
   0.0881     -1.1439
   0.0954     -1.1331
   0.1032     -1.1258
   0.1115     -1.1198
   0.1202     -1.1136
   0.1293     -1.1076
   0.1389     -1.1017
   0.1489     -1.0956
   0.1595     -1.0888
   0.1705     -1.0815
   0.1820     -1.0728
   0.1940     -1.0634
   0.2066     -1.0378
   0.2196     -0.9973
   0.2331     -0.8599
   0.2471     -0.6711
   0.2616     -0.6198
   0.2765     -0.6387
   0.2919     -0.6586
   0.3078     -0.6792
   0.3240     -0.6979
   0.3407     -0.7139
   0.3577     -0.7271
   0.3750     -0.7375
   0.3926     -0.7463
   0.4105     -0.7524
   0.4286     -0.7578
   0.4468     -0.7614
   0.4652     -0.7628
   0.4837     -0.7640
   0.5023     -0.7661
   0.5208     -0.7692
   0.5393     -0.7735
   0.5477     -0.7758
   0.5577     -0.7787
   0.5760     -0.7841
   0.5941     -0.7857
   0.6119     -0.7836
   0.6295     -0.7741
   0.6468     -0.7510
   0.6638     -0.7134
   0.6804     -0.6776
   0.6966     -0.6421
   0.7124     -0.6053
   0.7277     -0.5683
   0.7426     -0.5317
   0.7570     -0.4959
   0.7709     -0.4612
   0.7843     -0.4279
   0.7972     -0.3960
   0.8096     -0.3653
   0.8216     -0.3358
   0.8330     -0.3073
   0.8439     -0.2802
   0.8544     -0.2543
   0.8643     -0.2295
   0.8738     -0.2059
   0.8829     -0.1835
   0.8915     -0.1621
   0.8996     -0.1418
   0.9074     -0.1225
   0.9147     -0.1043
   0.9217     -0.0872
   0.9282     -0.0711
   0.9345     -0.0562
   0.9403     -0.0420
   0.9459     -0.0298
   0.9511     -0.0168
   0.9560     -0.0081
   0.9606      0.0019
   0.9650      0.0100
   0.9690      0.0179
   0.9729      0.0252
   0.9765      0.0319
   0.9799      0.0383
   0.9831      0.0442
   0.9861      0.0497
   0.9889      0.0549
   0.9915      0.0597
   0.9939      0.0641
   0.9962      0.0680
   0.9984      0.0713

WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1045
   0.9960      0.1162
   0.9936      0.1274
   0.9911      0.1383
   0.9884      0.1487
   0.9855      0.1589
   0.9824      0.1686
   0.9791      0.1779
   0.9757      0.1869
   0.9719      0.1954
   0.9680      0.2035
   0.9638      0.2113
   0.9593      0.2188
   0.9546      0.2257
   0.9496      0.2339
   0.9442      0.2397
   0.9385      0.2461
   0.9325      0.2519
   0.9262      0.2579
   0.9194      0.2638
   0.9123      0.2696
   0.9048      0.2754
   0.8969      0.2808
   0.8886      0.2857
   0.8798      0.2899
   0.8705      0.2928
   0.8608      0.2950
   0.8507      0.2947
   0.8400      0.2927
   0.8289      0.2874
   0.8173      0.2800
   0.8051      0.2691
   0.7926      0.2571
   0.7795      0.2414
   0.7659      0.2230
   0.7519      0.2011
   0.7374      0.1766
   0.7225      0.1504
   0.7071      0.1232
   0.6913      0.0953
   0.6751      0.0667
   0.6585      0.0380
   0.6416      0.0097
   0.6243     -0.0191
   0.6068     -0.0472
   0.5890     -0.0752
   0.5709     -0.1022
   0.5527     -0.1285
   0.5344     -0.1536
   0.5160     -0.1774
   0.4975     -0.1995
   0.4791     -0.2198
   0.4606     -0.2374
   0.4423     -0.2518
   0.4242     -0.2631
   0.4062     -0.2728
   0.3884     -0.2800
   0.3709     -0.2858
   0.3537     -0.2894
   0.3368     -0.2903
   0.3203     -0.2889
   0.3042     -0.2850
   0.2886     -0.2788
   0.2733     -0.2693
   0.2586     -0.2579
   0.2443     -0.2441
   0.2305     -0.2287
   0.2172     -0.2129
   0.2044     -0.1966
   0.1921     -0.1799
   0.1803     -0.1633
   0.1690     -0.1468
   0.1582     -0.1305
   0.1478     -0.1146
   0.1380     -0.0988
   0.1286     -0.0832
   0.1197     -0.0677
   0.1113     -0.0526
   0.1032     -0.0378
   0.0956     -0.0237
   0.0884     -0.0110
   0.0816      0.0005
   0.0752      0.0119
   0.0691      0.0239
   0.0633      0.0361
   0.0580      0.0487
   0.0529      0.0615
   0.0481      0.0740
   0.0436      0.0872
   0.0394      0.1020
   0.0355      0.1181
   0.0318      0.1362
   0.0284      0.1585
   0.0252      0.1830
   0.0223      0.2111
   0.0195      0.2428
   0.0170      0.2767
   0.0146      0.3174
   0.0125      0.3625
   0.0105      0.4118
   0.0087      0.4655
   0.0071      0.5211
   0.0057      0.5812
   0.0044      0.6407
   0.0033      0.6990
   0.0023      0.7524
   0.0016      0.7977
   0.0010      0.8313
   0.0005      0.8535
   0.0002      0.8559
   0.0000      0.8407
   0.0000      0.8140
   0.0000      0.7762
   0.0002      0.7268
   0.0004      0.6599
   0.0008      0.5807
   0.0013      0.4965
   0.0020      0.4118
   0.0029      0.3236
   0.0038      0.2342
   0.0050      0.1453
   0.0063      0.0548
   0.0078     -0.0369
   0.0094     -0.1339
   0.0112     -0.2324
   0.0132     -0.3336
   0.0154     -0.4295
   0.0179     -0.5262
   0.0205     -0.6534
   0.0234     -0.8132
   0.0266     -0.9707
   0.0300     -1.0875
   0.0338     -1.1485
   0.0378     -1.1662
   0.0421     -1.1790
   0.0467     -1.1829
   0.0515     -1.1800
   0.0567     -1.1758
   0.0623     -1.1701
   0.0682     -1.1625
   0.0744     -1.1531
   0.0810     -1.1399
   0.0880     -1.1234
   0.0954     -1.1076
   0.1032     -1.0951
   0.1114     -1.0830
   0.1201     -1.0699
   0.1292     -1.0551
   0.1388     -1.0367
   0.1488     -1.0152
   0.1594     -0.9881
   0.1704     -0.9474
   0.1819     -0.8767
   0.1939     -0.7762
   0.2065     -0.6934
   0.2195     -0.7109
   0.2330     -0.7416
   0.2470     -0.7620
   0.2615     -0.7769
   0.2764     -0.7875
   0.2918     -0.7956
   0.3077     -0.8022
   0.3239     -0.8073
   0.3405     -0.8110
   0.3575     -0.8138
   0.3749     -0.8146
   0.3925     -0.8134
   0.4103     -0.8105
   0.4284     -0.8068
   0.4467     -0.8030
   0.4651     -0.7992
   0.4836     -0.7959
   0.5021     -0.7924
   0.5207     -0.7868
   0.5392     -0.7746
   0.5576     -0.7479
   0.5759     -0.7156
   0.5939     -0.6956
   0.6118     -0.6837
   0.6294     -0.6737
   0.6467     -0.6549
   0.6637     -0.6288
   0.6803     -0.5997
   0.6965     -0.5660
   0.7123     -0.5307
   0.7276     -0.4947
   0.7425     -0.4591
   0.7569     -0.4242
   0.7708     -0.3905
   0.7842     -0.3582
   0.7971     -0.3275
   0.8096     -0.2983
   0.8215     -0.2705
   0.8329     -0.2440
   0.8438     -0.2189
   0.8543     -0.1952
   0.8643     -0.1727
   0.8738     -0.1516
   0.8828     -0.1316
   0.8914     -0.1128
   0.8996     -0.0951
   0.9073     -0.0786
   0.9147     -0.0632
   0.9216     -0.0488
   0.9282     -0.0355
   0.9344     -0.0234
   0.9403     -0.0119
   0.9458     -0.0022
   0.9510      0.0082
   0.9560      0.0148
   0.9606      0.0225
   0.9649      0.0273
   0.9690      0.0321
   0.9729      0.0369
   0.9765      0.0416
   0.9799      0.0463
   0.9831      0.0509
   0.9860      0.0555
   0.9888      0.0599
   0.9915      0.0642
   0.9939      0.0684
   0.9962      0.0723
   0.9984      0.0756

WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1103
   0.9960      0.1214
   0.9936      0.1321
   0.9911      0.1425
   0.9884      0.1525
   0.9855      0.1623
   0.9824      0.1718
   0.9791      0.1809
   0.9757      0.1896
   0.9719      0.1980
   0.9680      0.2061
   0.9638      0.2139
   0.9593      0.2215
   0.9546      0.2283
   0.9495      0.2360
   0.9442      0.2418
   0.9385      0.2481
   0.9325      0.2540
   0.9262      0.2599
   0.9194      0.2658
   0.9123      0.2715
   0.9048      0.2771
   0.8969      0.2825
   0.8886      0.2873
   0.8798      0.2915
   0.8705      0.2944
   0.8608      0.2965
   0.8507      0.2962
   0.8400      0.2942
   0.8289      0.2890
   0.8173      0.2818
   0.8051      0.2710
   0.7926      0.2592
   0.7795      0.2441
   0.7659      0.2260
   0.7519      0.2041
   0.7375      0.1800
   0.7225      0.1549
   0.7072      0.1285
   0.6914      0.1008
   0.6752      0.0728
   0.6586      0.0447
   0.6416      0.0171
   0.6244     -0.0108
   0.6068     -0.0379
   0.5890     -0.0649
   0.5710     -0.0908
   0.5528     -0.1159
   0.5345     -0.1399
   0.5321     -0.1428
   0.5161     -0.1626
   0.4976     -0.1837
   0.4792     -0.2030
   0.4608     -0.2194
   0.4424     -0.2324
   0.4243     -0.2427
   0.4063     -0.2512
   0.3885     -0.2579
   0.3710     -0.2626
   0.3538     -0.2656
   0.3370     -0.2658
   0.3205     -0.2641
   0.3044     -0.2597
   0.2887     -0.2533
   0.2735     -0.2439
   0.2587     -0.2325
   0.2444     -0.2189
   0.2306     -0.2039
   0.2173     -0.1881
   0.2045     -0.1722
   0.1922     -0.1557
   0.1804     -0.1393
   0.1691     -0.1232
   0.1582     -0.1072
   0.1479     -0.0915
   0.1381     -0.0760
   0.1287     -0.0606
   0.1198     -0.0455
   0.1113     -0.0305
   0.1033     -0.0158
   0.0957     -0.0018
   0.0885      0.0108
   0.0816      0.0223
   0.0752      0.0337
   0.0691      0.0455
   0.0634      0.0579
   0.0580      0.0704
   0.0529      0.0834
   0.0482      0.0960
   0.0437      0.1091
   0.0395      0.1241
   0.0355      0.1403
   0.0319      0.1585
   0.0284      0.1806
   0.0253      0.2052
   0.0223      0.2331
   0.0195      0.2648
   0.0170      0.2987
   0.0146      0.3390
   0.0125      0.3838
   0.0105      0.4325
   0.0087      0.4855
   0.0071      0.5403
   0.0056      0.5994
   0.0044      0.6578
   0.0033      0.7146
   0.0023      0.7664
   0.0016      0.8100
   0.0009      0.8415
   0.0005      0.8616
   0.0002      0.8618
   0.0000      0.8447
  -0.0001      0.8167
   0.0000      0.7773
   0.0001      0.7261
   0.0004      0.6583
   0.0008      0.5789
   0.0013      0.4935
   0.0020      0.4076
   0.0028      0.3188
   0.0038      0.2291
   0.0049      0.1405
   0.0062      0.0493
   0.0077     -0.0424
   0.0093     -0.1394
   0.0111     -0.2378
   0.0131     -0.3389
   0.0153     -0.4347
   0.0178     -0.5315
   0.0204     -0.6583
   0.0233     -0.8173
   0.0265     -0.9748
   0.0299     -1.0924
   0.0337     -1.1546
   0.0377     -1.1739
   0.0419     -1.1870
   0.0465     -1.1915
   0.0514     -1.1883
   0.0566     -1.1839
   0.0621     -1.1781
   0.0680     -1.1705
   0.0742     -1.1610
   0.0808     -1.1472
   0.0878     -1.1298
   0.0952     -1.1126
   0.1030     -1.0986
   0.1112     -1.0853
   0.1199     -1.0702
   0.1290     -1.0517
   0.1386     -1.0260
   0.1487     -0.9826
   0.1592     -0.9134
   0.1702     -0.8225
   0.1817     -0.7621
   0.1938     -0.7813
   0.2063     -0.8035
   0.2193     -0.8175
   0.2328     -0.8276
   0.2468     -0.8343
   0.2613     -0.8398
   0.2762     -0.8422
   0.2916     -0.8403
   0.3075     -0.8351
   0.3237     -0.8268
   0.3403     -0.8157
   0.3573     -0.8023
   0.3747     -0.7854
   0.3923     -0.7631
   0.4101     -0.7410
   0.4282     -0.7274
   0.4465     -0.7231
   0.4649     -0.7214
   0.4834     -0.7213
   0.5020     -0.7211
   0.5205     -0.7186
   0.5390     -0.7127
   0.5574     -0.7015
   0.5757     -0.6883
   0.5938     -0.6750
   0.6116     -0.6599
   0.6292     -0.6448
   0.6465     -0.6272
   0.6635     -0.6035
   0.6801     -0.5754
   0.6963     -0.5438
   0.7121     -0.5100
   0.7274     -0.4754
   0.7423     -0.4410
   0.7567     -0.4072
   0.7706     -0.3745
   0.7841     -0.3432
   0.7970     -0.3133
   0.8094     -0.2850
   0.8214     -0.2579
   0.8328     -0.2322
   0.8437     -0.2077
   0.8542     -0.1846
   0.8642     -0.1627
   0.8737     -0.1420
   0.8827     -0.1225
   0.8976     -0.0909
   0.8913     -0.1041
   0.8995     -0.0868
   0.9073     -0.0706
   0.9146     -0.0555
   0.9216     -0.0414
   0.9282     -0.0283
   0.9344     -0.0164
   0.9402     -0.0051
   0.9458      0.0046
   0.9510      0.0147
   0.9559      0.0216
   0.9605      0.0293
   0.9649      0.0339
   0.9690      0.0386
   0.9728      0.0433
   0.9765      0.0479
   0.9799      0.0525
   0.9830      0.0571
   0.9860      0.0616
   0.9888      0.0660
   0.9915      0.0704
   0.9939      0.0746
   0.9962      0.0786
   0.9984      0.0822

WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9982      0.1269
   0.9960      0.1373
   0.9936      0.1470
   0.9911      0.1564
   0.9884      0.1655
   0.9855      0.1741
   0.9824      0.1824
   0.9791      0.1902
   0.9756      0.1977
   0.9719      0.2048
   0.9680      0.2115
   0.9638      0.2178
   0.9593      0.2239
   0.9546      0.2300
   0.9495      0.2369
   0.9442      0.2421
   0.9385      0.2478
   0.9325      0.2530
   0.9261      0.2584
   0.9194      0.2636
   0.9123      0.2687
   0.9048      0.2736
   0.8969      0.2782
   0.8885      0.2824
   0.8798      0.2858
   0.8705      0.2883
   0.8608      0.2895
   0.8507      0.2888
   0.8400      0.2864
   0.8289      0.2808
   0.8173      0.2735
   0.8052      0.2628
   0.7926      0.2512
   0.7795      0.2362
   0.7660      0.2184
   0.7520      0.1973
   0.7376      0.1739
   0.7226      0.1490
   0.7073      0.1229
   0.6915      0.0958
   0.6753      0.0680
   0.6588      0.0399
   0.6418      0.0122
   0.6246     -0.0158
   0.6071     -0.0430
   0.5893     -0.0701
   0.5713     -0.0961
   0.5531     -0.1214
   0.5348     -0.1455
   0.5164     -0.1683
   0.4979     -0.1895
   0.4795     -0.2089
   0.4611     -0.2254
   0.4428     -0.2383
   0.4246     -0.2487
   0.4066     -0.2573
   0.3889     -0.2639
   0.3714     -0.2689
   0.3542     -0.2715
   0.3373     -0.2716
   0.3208     -0.2697
   0.3047     -0.2651
   0.2891     -0.2585
   0.2738     -0.2489
   0.2591     -0.2373
   0.2448     -0.2236
   0.2310     -0.2085
   0.2176     -0.1926
   0.2048     -0.1765
   0.1925     -0.1598
   0.1807     -0.1433
   0.1694     -0.1270
   0.1586     -0.1109
   0.1482     -0.0950
   0.1384     -0.0794
   0.1290     -0.0639
   0.1201     -0.0486
   0.1116     -0.0335
   0.1036     -0.0188
   0.0960     -0.0047
   0.0888      0.0079
   0.0819      0.0195
   0.0755      0.0309
   0.0694      0.0430
   0.0637      0.0552
   0.0583      0.0680
   0.0532      0.0810
   0.0484      0.0938
   0.0439      0.1072
   0.0397      0.1222
   0.0358      0.1386
   0.0321      0.1570
   0.0287      0.1795
   0.0255      0.2041
   0.0225      0.2304
   0.0197      0.2611
   0.0172      0.2945
   0.0148      0.3353
   0.0127      0.3813
   0.0107      0.4308
   0.0089      0.4839
   0.0072      0.5386
   0.0058      0.5976
   0.0045      0.6563
   0.0034      0.7137
   0.0025      0.7662
   0.0017      0.8104
   0.0010      0.8425
   0.0006      0.8633
   0.0003      0.8642
   0.0001      0.8478
   0.0000      0.8207
   0.0001      0.7815
   0.0002      0.7297
   0.0004      0.6635
   0.0008      0.5863
   0.0013      0.5012
   0.0020      0.4145
   0.0028      0.3255
   0.0038      0.2364
   0.0049      0.1478
   0.0062      0.0565
   0.0077     -0.0351
   0.0093     -0.1317
   0.0111     -0.2293
   0.0131     -0.3299
   0.0153     -0.4286
   0.0177     -0.5288
   0.0204     -0.6506
   0.0232     -0.8013
   0.0264     -0.9544
   0.0298     -1.0834
   0.0336     -1.1460
   0.0375     -1.1632
   0.0418     -1.1713
   0.0464     -1.1766
   0.0513     -1.1756
   0.0565     -1.1711
   0.0620     -1.1638
   0.0679     -1.1527
   0.0741     -1.1392
   0.0807     -1.1259
   0.0877     -1.1126
   0.0950     -1.0982
   0.1028     -1.0821
   0.1110     -1.0629
   0.1197     -1.0411
   0.1288     -1.0063
   0.1384     -0.9572
   0.1484     -0.8753
   0.1590     -0.7569
   0.1700     -0.7201
   0.1815     -0.7421
   0.1935     -0.7540
   0.2060     -0.7624
   0.2190     -0.7645
   0.2325     -0.7607
   0.2465     -0.7547
   0.2610     -0.7523
   0.2759     -0.7531
   0.2913     -0.7517
   0.3072     -0.7453
   0.3234     -0.7340
   0.3400     -0.7204
   0.3570     -0.7094
   0.3743     -0.7020
   0.3919     -0.6959
   0.4098     -0.6895
   0.4279     -0.6827
   0.4462     -0.6758
   0.4646     -0.6693
   0.4831     -0.6633
   0.5016     -0.6577
   0.5202     -0.6522
   0.5387     -0.6465
   0.5571     -0.6398
   0.5753     -0.6308
   0.5934     -0.6193
   0.6113     -0.6068
   0.6289     -0.5943
   0.6462     -0.5785
   0.6632     -0.5570
   0.6798     -0.5318
   0.6960     -0.5041
   0.7118     -0.4734
   0.7272     -0.4414
   0.7421     -0.4095
   0.7565     -0.3778
   0.7704     -0.3467
   0.7838     -0.3169
   0.7968     -0.2886
   0.8092     -0.2618
   0.8212     -0.2366
   0.8326     -0.2124
   0.8436     -0.1889
   0.8540     -0.1664
   0.8640     -0.1451
   0.8735     -0.1250
   0.8826     -0.1061
   0.8912     -0.0883
   0.8994     -0.0716
   0.9071     -0.0559
   0.9145     -0.0412
   0.9215     -0.0274
   0.9281     -0.0146
   0.9343     -0.0028
   0.9402      0.0084
   0.9457      0.0182
   0.9509      0.0282
   0.9558      0.0355
   0.9605      0.0434
   0.9648      0.0487
   0.9689      0.0539
   0.9728      0.0590
   0.9764      0.0641
   0.9798      0.0691
   0.9830      0.0740
   0.9860      0.0787
   0.9888      0.0834
   0.9914      0.0878
   0.9939      0.0921
   0.9962      0.0961
   0.9984      0.0996



WING/BODY/FX2B-FAIRING

 GRID_SIZE      MACH     ALPHA
 ????????.      0.75     ?.???

WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????

WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m)
     X/C     CP          CF            CFX           CFY           CFZ
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????
 ???.????    ???.????    ???.??????    ???.??????    ???.??????    ???.??????



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

* BO2              Semispan   (585.647 mm)
