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



COARSE GRID SIZE            WB       WBF
----------------------------------------
              Zones:        12        12
        Field Nodes:   2387918   2395170
        Field Cells:   2256896   2263808
     Boundary Nodes:
     Boundary Faces:
   BL 1st-Cell Size:   0.00055   0.00055
 BL Max-Growth Rate:
           BL Cells:
      Miscellaneous:



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

WING/BODY

 GRID_SIZE      MACH     ALPHA
  2387918.      0.75     0.279

WING SECTION 1   Y/BO2 0.15  (Y = 0.08785 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.0002      0.8828
   0.0005      0.8481
   0.0008      0.8008
   0.0013      0.7267
   0.0020      0.6299
   0.0029      0.5221
   0.0042      0.3980
   0.0059      0.2564
   0.0080      0.1022
   0.0106     -0.0579
   0.0136     -0.2181
   0.0173     -0.3763
   0.0215     -0.5236
   0.0264     -0.6508
   0.0319     -0.7534
   0.0382     -0.8277
   0.0452     -0.8758
   0.0529     -0.9022
   0.0614     -0.9140
   0.0708     -0.9113
   0.0810     -0.9059
   0.0921     -0.8996
   0.1041     -0.8925
   0.1170     -0.8835
   0.1310     -0.8666
   0.1460     -0.8530
   0.1621     -0.8525
   0.1793     -0.8476
   0.1975     -0.8380
   0.2168     -0.8275
   0.2371     -0.8129
   0.2585     -0.7883
   0.2810     -0.7542
   0.3043     -0.7113
   0.3285     -0.6700
   0.3535     -0.6423
   0.3793     -0.6238
   0.4056     -0.6065
   0.4324     -0.5880
   0.4595     -0.5696
   0.4869     -0.5502
   0.5143     -0.5287
   0.5416     -0.5032
   0.5688     -0.4721
   0.5955     -0.4377
   0.6218     -0.4017
   0.6475     -0.3665
   0.6725     -0.3325
   0.6737     -0.3309
   0.6966     -0.2994
   0.7198     -0.2698
   0.7421     -0.2456
   0.7633     -0.2250
   0.7835     -0.2052
   0.8026     -0.1922
   0.8207     -0.1863
   0.8376     -0.1872
   0.8534     -0.1916
   0.8682     -0.1993
   0.8819     -0.2082
   0.8946     -0.2173
   0.9063     -0.2274
   0.9171     -0.2330
   0.9271     -0.2390
   0.9344     -0.2404
   0.9362     -0.2405
   0.9445     -0.2402
   0.9522     -0.2392
   0.9592     -0.2349
   0.9657     -0.2303
   0.9715     -0.1925
   0.9769     -0.1672
   0.9817     -0.1500
   0.9862     -0.1388
   0.9902     -0.1329
   0.9939     -0.1325
   0.9973     -0.1394
   0.9970     -0.0683
   0.9934     -0.0262
   0.9895      0.0091
   0.9851      0.0396
   0.9803      0.0661
   0.9750      0.0891
   0.9692      0.1084
   0.9629      0.1234
   0.9560      0.1373
   0.9485      0.1500
   0.9403      0.1626
   0.9313      0.1739
   0.9216      0.1834
   0.9111      0.1921
   0.8997      0.1963
   0.8874      0.2003
   0.8742      0.2005
   0.8600      0.1996
   0.8448      0.1960
   0.8286      0.1902
   0.8113      0.1832
   0.7931      0.1708
   0.7738      0.1509
   0.7537      0.1186
   0.7326      0.0775
   0.7107      0.0250
   0.6878     -0.0343
   0.6642     -0.0843
   0.6398     -0.1380
   0.6198     -0.1780
   0.6147     -0.1882
   0.5890     -0.2448
   0.5628     -0.2930
   0.5361     -0.3417
   0.5091     -0.3341
   0.4819     -0.3084
   0.4548     -0.2914
   0.4279     -0.2823
   0.4012     -0.2770
   0.3750     -0.2759
   0.3359     -0.2566
   0.3494     -0.2666
   0.3245     -0.2481
   0.3003     -0.2365
   0.2770     -0.2270
   0.2546     -0.2131
   0.2332     -0.1939
   0.2129     -0.1763
   0.1936     -0.1676
   0.1753     -0.1623
   0.1582     -0.1543
   0.1421     -0.1407
   0.1271     -0.1234
   0.1131     -0.1024
   0.1001     -0.0793
   0.0881     -0.0534
   0.0694      0.0011
   0.0771     -0.0242
   0.0670      0.0090
   0.0578      0.0475
   0.0494      0.0911
   0.0418      0.1418
   0.0350      0.1993
   0.0289      0.2643
   0.0235      0.3363
   0.0188      0.4135
   0.0147      0.4953
   0.0112      0.5797
   0.0083      0.6631
   0.0059      0.7420
   0.0040      0.8133
   0.0026      0.8721
   0.0015      0.9161
   0.0008      0.9449
   0.0004      0.9588
   0.0001      0.9565
   0.0000      0.9467
   0.0000      0.9307
   0.0002      0.8833
   0.0001      0.9092

WING SECTION 2   Y/BO2 0.239 (Y = 0.13987 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9971      0.1423
   0.9935      0.1496
   0.9896      0.1599
   0.9853      0.1725
   0.9805      0.1870
   0.9753      0.2032
   0.9696      0.2212
   0.9634      0.2412
   0.9565      0.2468
   0.9491      0.2517
   0.9410      0.2572
   0.9321      0.2618
   0.9225      0.2662
   0.9120      0.2693
   0.9007      0.2721
   0.8885      0.2728
   0.8754      0.2722
   0.8613      0.2693
   0.8461      0.2645
   0.8300      0.2559
   0.8128      0.2440
   0.7945      0.2265
   0.7753      0.2018
   0.7551      0.1688
   0.7339      0.1256
   0.7119      0.0736
   0.6889      0.0143
   0.6650     -0.0407
   0.6404     -0.1023
   0.6150     -0.1581
   0.5891     -0.2230
   0.5626     -0.2800
   0.5357     -0.3351
   0.5086     -0.3582
   0.4813     -0.3517
   0.4541     -0.3486
   0.4270     -0.3476
   0.4004     -0.3486
   0.3741     -0.3505
   0.3485     -0.3438
   0.3236     -0.3291
   0.2995     -0.3183
   0.2763     -0.3074
   0.2541     -0.2912
   0.2328     -0.2697
   0.2126     -0.2506
   0.1935     -0.2370
   0.1755     -0.2258
   0.1586     -0.2135
   0.1427     -0.1972
   0.1280     -0.1777
   0.1142     -0.1555
   0.1015     -0.1321
   0.0897     -0.1073
   0.0788     -0.0810
   0.0689     -0.0510
   0.0598     -0.0168
   0.0515      0.0204
   0.0440      0.0626
   0.0372      0.1107
   0.0311      0.1655
   0.0256      0.2275
   0.0208      0.2957
   0.0166      0.3691
   0.0129      0.4465
   0.0098      0.5266
   0.0072      0.6046
   0.0051      0.6782
   0.0034      0.7420
   0.0021      0.7918
   0.0012      0.8251
   0.0006      0.8437
   0.0002      0.8411
   0.0000      0.8271
   0.0000      0.8049
   0.0001      0.7748
   0.0002      0.7386
   0.0005      0.6907
   0.0009      0.6248
   0.0014      0.5297
   0.0022      0.4126
   0.0033      0.2892
   0.0048      0.1520
   0.0067     -0.0013
   0.0089     -0.1566
   0.0117     -0.3159
   0.0149     -0.4769
   0.0187     -0.6357
   0.0231     -0.7992
   0.0281     -0.9507
   0.0337     -1.0653
   0.0400     -1.1428
   0.0470     -1.1962
   0.0548     -1.2357
   0.0633     -1.2659
   0.0726     -1.2795
   0.0827     -1.2879
   0.0937     -1.2887
   0.1057     -1.2841
   0.1186     -1.2692
   0.1325     -1.2359
   0.1474     -1.1821
   0.1634     -1.1094
   0.1804     -1.0330
   0.1985     -0.9745
   0.2177     -0.9277
   0.2380     -0.8719
   0.2593     -0.7820
   0.2816     -0.6871
   0.3049     -0.6591
   0.3291     -0.6475
   0.3540     -0.6393
   0.3797     -0.6314
   0.4059     -0.6194
   0.4327     -0.6073
   0.4598     -0.5948
   0.4871     -0.5824
   0.5144     -0.5702
   0.5417     -0.5579
   0.5688     -0.5455
   0.5956     -0.5324
   0.6218     -0.5181
   0.6474     -0.5004
   0.6724     -0.4777
   0.6964     -0.4504
   0.7196     -0.4193
   0.7418     -0.3880
   0.7630     -0.3596
   0.7831     -0.3351
   0.8022     -0.3143
   0.8202     -0.2955
   0.8371     -0.2744
   0.8529     -0.2495
   0.8676     -0.2222
   0.8813     -0.1917
   0.8940     -0.1600
   0.9058     -0.1268
   0.9166     -0.0935
   0.9266     -0.0614
   0.9358     -0.0318
   0.9442     -0.0044
   0.9519      0.0189
   0.9590      0.0399
   0.9654      0.0582
   0.9713      0.0512
   0.9767      0.0488
   0.9816      0.0507
   0.9861      0.0564
   0.9902      0.0657
   0.9939      0.0786
   0.9973      0.0954

WING SECTION 3   Y/BO2 0.331 (Y = 0.19453 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9971      0.1413
   0.9937      0.1572
   0.9899      0.1727
   0.9857      0.1876
   0.9810      0.2018
   0.9760      0.2153
   0.9704      0.2281
   0.9644      0.2403
   0.9577      0.2492
   0.9504      0.2572
   0.9425      0.2655
   0.9338      0.2727
   0.9244      0.2800
   0.9142      0.2866
   0.9031      0.2926
   0.8911      0.2972
   0.8782      0.3010
   0.8643      0.3013
   0.8494      0.2990
   0.8334      0.2916
   0.8164      0.2788
   0.7983      0.2589
   0.7791      0.2347
   0.7590      0.2024
   0.7378      0.1615
   0.7156      0.1123
   0.6925      0.0589
   0.6684      0.0037
   0.6435     -0.0486
   0.6180     -0.1059
   0.5917     -0.1601
   0.5650     -0.2161
   0.5379     -0.2658
   0.5105     -0.3019
   0.4831     -0.3226
   0.4558     -0.3364
   0.4286     -0.3479
   0.4019     -0.3572
   0.3756     -0.3617
   0.3499     -0.3596
   0.3250     -0.3513
   0.3010     -0.3413
   0.2778     -0.3286
   0.2557     -0.3108
   0.2346     -0.2878
   0.2146     -0.2649
   0.1956     -0.2453
   0.1778     -0.2277
   0.1611     -0.2092
   0.1455     -0.1893
   0.1309     -0.1684
   0.1174     -0.1470
   0.1048     -0.1259
   0.0932     -0.1046
   0.0826     -0.0824
   0.0728     -0.0599
   0.0638     -0.0368
   0.0555     -0.0115
   0.0481      0.0173
   0.0413      0.0498
   0.0351      0.0866
   0.0296      0.1290
   0.0246      0.1787
   0.0202      0.2369
   0.0162      0.3020
   0.0128      0.3738
   0.0098      0.4506
   0.0073      0.5313
   0.0052      0.6111
   0.0035      0.6842
   0.0022      0.7458
   0.0012      0.7887
   0.0005      0.8118
   0.0002      0.8065
   0.0000      0.7839
   0.0000      0.7485
   0.0002      0.7016
   0.0004      0.6367
   0.0009      0.5450
   0.0017      0.4298
   0.0027      0.3008
   0.0041      0.1665
   0.0058      0.0257
   0.0080     -0.1216
   0.0106     -0.2692
   0.0136     -0.4206
   0.0171     -0.5751
   0.0211     -0.7412
   0.0257     -0.9280
   0.0309     -1.0794
   0.0367     -1.1616
   0.0431     -1.2035
   0.0503     -1.2368
   0.0581     -1.2523
   0.0666     -1.2643
   0.0760     -1.2678
   0.0861     -1.2699
   0.0972     -1.2666
   0.1091     -1.2626
   0.1220     -1.2566
   0.1359     -1.2479
   0.1508     -1.2369
   0.1668     -1.2224
   0.1838     -1.2072
   0.2019     -1.1653
   0.2211     -1.0555
   0.2414     -0.8289
   0.2627     -0.5955
   0.2850     -0.6080
   0.3082     -0.6323
   0.3324     -0.6531
   0.3573     -0.6716
   0.3829     -0.6812
   0.4092     -0.6883
   0.4359     -0.6902
   0.4629     -0.6879
   0.4902     -0.6840
   0.5175     -0.6798
   0.5447     -0.6759
   0.5717     -0.6717
   0.5983     -0.6647
   0.6244     -0.6498
   0.6499     -0.6252
   0.6747     -0.5910
   0.6986     -0.5479
   0.7216     -0.5010
   0.7436     -0.4549
   0.7646     -0.4122
   0.7846     -0.3726
   0.8034     -0.3357
   0.8212     -0.3007
   0.8379     -0.2669
   0.8536     -0.2333
   0.8682     -0.1999
   0.8818     -0.1665
   0.8944     -0.1344
   0.9061     -0.1039
   0.9169     -0.0749
   0.9268     -0.0478
   0.9359     -0.0234
   0.9443     -0.0009
   0.9520      0.0179
   0.9591      0.0351
   0.9655      0.0492
   0.9714      0.0563
   0.9768      0.0637
   0.9817      0.0710
   0.9861      0.0784
   0.9902      0.0856
   0.9939      0.0927
   0.9972      0.0996

WING SECTION 4   Y/BO2 0.377 (Y = 0.22156 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9971      0.1210
   0.9937      0.1389
   0.9899      0.1563
   0.9857      0.1731
   0.9811      0.1891
   0.9761      0.2043
   0.9706      0.2187
   0.9645      0.2322
   0.9579      0.2436
   0.9507      0.2531
   0.9428      0.2632
   0.9341      0.2716
   0.9248      0.2803
   0.9146      0.2883
   0.9036      0.2961
   0.8917      0.3022
   0.8788      0.3079
   0.8650      0.3099
   0.8501      0.3080
   0.8342      0.3011
   0.8173      0.2852
   0.7993      0.2659
   0.7802      0.2390
   0.7602      0.2066
   0.7391      0.1652
   0.7170      0.1181
   0.6940      0.0684
   0.6678      0.0111
   0.6701      0.0155
   0.6453     -0.0332
   0.6199     -0.0854
   0.5938     -0.1346
   0.5672     -0.1844
   0.5402     -0.2296
   0.5130     -0.2690
   0.4857     -0.2988
   0.4585     -0.3211
   0.4315     -0.3372
   0.4048     -0.3491
   0.3786     -0.3550
   0.3531     -0.3547
   0.3283     -0.3497
   0.3043     -0.3395
   0.2812     -0.3264
   0.2591     -0.3070
   0.2381     -0.2825
   0.2181     -0.2579
   0.1992     -0.2339
   0.1814     -0.2108
   0.1647     -0.1877
   0.1491     -0.1654
   0.1345     -0.1431
   0.1210     -0.1210
   0.1084     -0.1001
   0.0968     -0.0805
   0.0861     -0.0613
   0.0828     -0.0552
   0.0763     -0.0429
   0.0672     -0.0257
   0.0589     -0.0065
   0.0513      0.0141
   0.0445      0.0364
   0.0382      0.0612
   0.0325      0.0904
   0.0274      0.1269
   0.0228      0.1712
   0.0187      0.2219
   0.0150      0.2822
   0.0118      0.3524
   0.0091      0.4297
   0.0067      0.5119
   0.0047      0.5968
   0.0031      0.6779
   0.0018      0.7450
   0.0009      0.7947
   0.0003      0.8138
   0.0001      0.7998
   0.0000      0.7627
   0.0001      0.7082
   0.0004      0.6285
   0.0010      0.5205
   0.0019      0.3991
   0.0030      0.2699
   0.0046      0.1364
   0.0064      0.0031
   0.0087     -0.1362
   0.0113     -0.2786
   0.0144     -0.4227
   0.0180     -0.5755
   0.0220     -0.7581
   0.0267     -0.9547
   0.0319     -1.1092
   0.0377     -1.1605
   0.0442     -1.1889
   0.0513     -1.2020
   0.0591     -1.2061
   0.0676     -1.2051
   0.0769     -1.1999
   0.0871     -1.1920
   0.0981     -1.1827
   0.1100     -1.1739
   0.1228     -1.1650
   0.1367     -1.1555
   0.1515     -1.1448
   0.1674     -1.1317
   0.1844     -1.1189
   0.2025     -1.0833
   0.2216     -1.0109
   0.2418     -0.8110
   0.2631     -0.5923
   0.2854     -0.6303
   0.3086     -0.6638
   0.3327     -0.6920
   0.3576     -0.7118
   0.3832     -0.7264
   0.4094     -0.7355
   0.4361     -0.7425
   0.4631     -0.7434
   0.4903     -0.7430
   0.5176     -0.7430
   0.5448     -0.7441
   0.5718     -0.7466
   0.5984     -0.7471
   0.6245     -0.7385
   0.6500     -0.7107
   0.6747     -0.6650
   0.6986     -0.6143
   0.7216     -0.5605
   0.7436     -0.5079
   0.7646     -0.4590
   0.7845     -0.4123
   0.8034     -0.3685
   0.8211     -0.3273
   0.8378     -0.2885
   0.8535     -0.2516
   0.8681     -0.2159
   0.8816     -0.1819
   0.8942     -0.1499
   0.9059     -0.1200
   0.9167     -0.0921
   0.9267     -0.0662
   0.9358     -0.0430
   0.9442     -0.0213
   0.9519     -0.0038
   0.9590      0.0131
   0.9655      0.0265
   0.9714      0.0337
   0.9768      0.0414
   0.9817      0.0492
   0.9861      0.0567
   0.9902      0.0638
   0.9939      0.0705
   0.9972      0.0768

WING SECTION 5   Y/BO2 0.411 (Y = 0.24037 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9972      0.1097
   0.9937      0.1291
   0.9900      0.1475
   0.9858      0.1649
   0.9812      0.1812
   0.9762      0.1965
   0.9707      0.2109
   0.9647      0.2241
   0.9581      0.2365
   0.9509      0.2472
   0.9430      0.2571
   0.9345      0.2663
   0.9251      0.2750
   0.9150      0.2835
   0.9040      0.2916
   0.8921      0.2983
   0.8793      0.3039
   0.8655      0.3067
   0.8507      0.3049
   0.8348      0.2976
   0.8179      0.2820
   0.7999      0.2630
   0.7809      0.2375
   0.7608      0.2065
   0.7397      0.1674
   0.7176      0.1233
   0.6946      0.0766
   0.6707      0.0270
   0.6460     -0.0200
   0.6206     -0.0686
   0.5945     -0.1156
   0.5680     -0.1614
   0.5411     -0.2044
   0.5139     -0.2434
   0.4867     -0.2773
   0.4596     -0.3061
   0.4326     -0.3246
   0.4060     -0.3383
   0.3799     -0.3460
   0.3545     -0.3473
   0.3297     -0.3443
   0.3058     -0.3366
   0.2828     -0.3223
   0.2607     -0.3034
   0.2397     -0.2792
   0.2198     -0.2538
   0.2009     -0.2273
   0.1832     -0.2010
   0.1665     -0.1751
   0.1509     -0.1503
   0.1364     -0.1258
   0.1228     -0.1024
   0.1103     -0.0796
   0.0987     -0.0581
   0.0879     -0.0385
   0.0781     -0.0210
   0.0690     -0.0035
   0.0607      0.0152
   0.0531      0.0334
   0.0461      0.0522
   0.0398      0.0728
   0.0341      0.0972
   0.0289      0.1270
   0.0242      0.1639
   0.0200      0.2069
   0.0163      0.2593
   0.0129      0.3221
   0.0100      0.3948
   0.0075      0.4756
   0.0054      0.5621
   0.0036      0.6502
   0.0022      0.7309
   0.0012      0.7936
   0.0004      0.8339
   0.0000      0.8287
   0.0000      0.7924
   0.0001      0.7359
   0.0004      0.6491
   0.0010      0.5323
   0.0019      0.4086
   0.0032      0.2805
   0.0048      0.1488
   0.0067      0.0171
   0.0090     -0.1195
   0.0117     -0.2633
   0.0149     -0.4078
   0.0184     -0.5595
   0.0225     -0.7592
   0.0272     -0.9671
   0.0324     -1.1138
   0.0383     -1.1502
   0.0447     -1.1728
   0.0519     -1.1713
   0.0597     -1.1673
   0.0682     -1.1597
   0.0775     -1.1485
   0.0877     -1.1340
   0.0987     -1.1199
   0.1106     -1.1096
   0.1235     -1.0998
   0.1373     -1.0908
   0.1522     -1.0810
   0.1681     -1.0697
   0.1851     -1.0544
   0.2032     -1.0207
   0.2224     -0.9292
   0.2426     -0.7155
   0.2639     -0.6177
   0.2862     -0.6638
   0.3095     -0.6968
   0.3336     -0.7219
   0.3586     -0.7407
   0.3842     -0.7527
   0.4105     -0.7630
   0.4372     -0.7688
   0.4643     -0.7702
   0.4915     -0.7714
   0.5189     -0.7744
   0.5461     -0.7790
   0.5731     -0.7840
   0.5997     -0.7848
   0.6259     -0.7759
   0.6513     -0.7454
   0.6761     -0.6931
   0.7000     -0.6390
   0.7229     -0.5834
   0.7449     -0.5287
   0.7658     -0.4766
   0.7857     -0.4266
   0.8045     -0.3804
   0.8222     -0.3363
   0.8388     -0.2953
   0.8544     -0.2564
   0.8689     -0.2199
   0.8824     -0.1859
   0.8950     -0.1542
   0.9066     -0.1250
   0.9173     -0.0981
   0.9272     -0.0736
   0.9363     -0.0516
   0.9447     -0.0313
   0.9524     -0.0146
   0.9594      0.0012
   0.9658      0.0140
   0.9717      0.0241
   0.9770      0.0335
   0.9819      0.0419
   0.9864      0.0494
   0.9904      0.0559
   0.9941      0.0616
   0.9974      0.0662

WING SECTION 6   Y/BO2 0.514 (Y = 0.30090 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9972      0.1075
   0.9937      0.1254
   0.9900      0.1424
   0.9858      0.1584
   0.9812      0.1733
   0.9974      0.0687
   0.9793      0.1788
   0.9762      0.1872
   0.9707      0.2001
   0.9647      0.2122
   0.9581      0.2233
   0.9509      0.2325
   0.9430      0.2425
   0.9345      0.2509
   0.9251      0.2597
   0.9150      0.2683
   0.9040      0.2765
   0.8921      0.2845
   0.8793      0.2901
   0.8655      0.2954
   0.8507      0.2952
   0.8348      0.2903
   0.8179      0.2780
   0.7999      0.2614
   0.7809      0.2400
   0.7608      0.2132
   0.7397      0.1794
   0.7177      0.1413
   0.6947      0.1005
   0.6708      0.0573
   0.6461      0.0161
   0.6206     -0.0261
   0.5946     -0.0676
   0.5681     -0.1073
   0.5412     -0.1458
   0.5140     -0.1810
   0.4868     -0.2131
   0.4597     -0.2398
   0.4327     -0.2599
   0.4062     -0.2751
   0.3801     -0.2854
   0.3546     -0.2917
   0.3298     -0.2920
   0.3059     -0.2876
   0.2829     -0.2774
   0.2609     -0.2626
   0.2399     -0.2423
   0.2199     -0.2200
   0.2011     -0.1959
   0.1833     -0.1718
   0.1666     -0.1477
   0.1510     -0.1240
   0.1365     -0.1011
   0.1229     -0.0787
   0.1104     -0.0566
   0.0988     -0.0351
   0.0880     -0.0164
   0.0782      0.0005
   0.0691      0.0178
   0.0608      0.0357
   0.0531      0.0537
   0.0462      0.0725
   0.0399      0.0928
   0.0341      0.1171
   0.0289      0.1468
   0.0243      0.1836
   0.0201      0.2270
   0.0163      0.2797
   0.0130      0.3426
   0.0101      0.4156
   0.0076      0.4972
   0.0054      0.5840
   0.0037      0.6729
   0.0023      0.7545
   0.0012      0.8178
   0.0005      0.8588
   0.0001      0.8541
   0.0000      0.8180
   0.0001      0.7609
   0.0004      0.6739
   0.0010      0.5570
   0.0020      0.4310
   0.0032      0.3018
   0.0048      0.1691
   0.0067      0.0364
   0.0090     -0.1026
   0.0117     -0.2472
   0.0148     -0.3934
   0.0184     -0.5467
   0.0225     -0.7455
   0.0271     -0.9633
   0.0324     -1.0946
   0.0382     -1.1506
   0.0447     -1.1606
   0.0518     -1.1624
   0.0596     -1.1550
   0.0682     -1.1443
   0.0775     -1.1288
   0.0876     -1.1077
   0.0986     -1.0860
   0.1105     -1.0657
   0.1234     -1.0426
   0.1372     -1.0155
   0.1521     -0.9766
   0.1680     -0.9245
   0.1850     -0.8179
   0.2031     -0.7120
   0.2223     -0.7163
   0.2425     -0.7604
   0.2638     -0.7885
   0.2861     -0.8052
   0.3094     -0.8130
   0.3335     -0.8162
   0.3584     -0.8154
   0.3841     -0.8116
   0.4103     -0.8060
   0.4371     -0.8006
   0.4641     -0.7958
   0.4914     -0.7912
   0.5187     -0.7851
   0.5460     -0.7706
   0.5730     -0.7351
   0.5996     -0.6943
   0.6257     -0.6711
   0.6512     -0.6488
   0.6760     -0.6077
   0.6998     -0.5591
   0.7228     -0.5066
   0.7448     -0.4547
   0.7657     -0.4037
   0.7856     -0.3562
   0.8044     -0.3115
   0.8221     -0.2701
   0.8387     -0.2316
   0.8543     -0.1958
   0.8688     -0.1630
   0.8824     -0.1329
   0.8949     -0.1053
   0.9065     -0.0801
   0.9173     -0.0575
   0.9272     -0.0370
   0.9363     -0.0193
   0.9447     -0.0029
   0.9524      0.0101
   0.9594      0.0224
   0.9658      0.0323
   0.9717      0.0381
   0.9770      0.0439
   0.9819      0.0495
   0.9863      0.0550
   0.9904      0.0601
   0.9971      0.0683
   0.9941      0.0647

WING SECTION 7   Y/BO2 0.638 (Y = 0.37319 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9972      0.1110
   0.9937      0.1278
   0.9899      0.1439
   0.9858      0.1593
   0.9812      0.1738
   0.9762      0.1874
   0.9707      0.2005
   0.9647      0.2135
   0.9581      0.2243
   0.9509      0.2335
   0.9430      0.2435
   0.9345      0.2518
   0.9251      0.2606
   0.9150      0.2691
   0.9040      0.2773
   0.8921      0.2851
   0.8793      0.2907
   0.8655      0.2961
   0.8507      0.2959
   0.8348      0.2910
   0.8179      0.2789
   0.7999      0.2626
   0.7809      0.2415
   0.7608      0.2148
   0.7398      0.1817
   0.7177      0.1448
   0.6947      0.1047
   0.6708      0.0621
   0.6461      0.0219
   0.6207     -0.0192
   0.5947     -0.0594
   0.5682     -0.0976
   0.5413     -0.1345
   0.5141     -0.1681
   0.4869     -0.1990
   0.4598     -0.2236
   0.4329     -0.2426
   0.4063     -0.2553
   0.3802     -0.2652
   0.3547     -0.2698
   0.3300     -0.2693
   0.3060     -0.2646
   0.2830     -0.2538
   0.2610     -0.2395
   0.2400     -0.2193
   0.2200     -0.1969
   0.2012     -0.1733
   0.1834     -0.1493
   0.1667     -0.1255
   0.1511     -0.1026
   0.1366     -0.0800
   0.1230     -0.0576
   0.1105     -0.0352
   0.0988     -0.0143
   0.0881      0.0043
   0.0782      0.0212
   0.0691      0.0383
   0.0608      0.0562
   0.0532      0.0747
   0.0462      0.0931
   0.0399      0.1140
   0.0342      0.1381
   0.0290      0.1680
   0.0243      0.2049
   0.0201      0.2478
   0.0163      0.3005
   0.0130      0.3630
   0.0101      0.4352
   0.0076      0.5157
   0.0054      0.6015
   0.0037      0.6890
   0.0022      0.7687
   0.0012      0.8299
   0.0004      0.8675
   0.0001      0.8602
  -0.0001      0.8220
   0.0000      0.7626
   0.0004      0.6739
   0.0010      0.5567
   0.0019      0.4292
   0.0031      0.2989
   0.0047      0.1654
   0.0067      0.0323
   0.0089     -0.1063
   0.0116     -0.2508
   0.0147     -0.3965
   0.0183     -0.5492
   0.0224     -0.7498
   0.0270     -0.9610
   0.0323     -1.1046
   0.0381     -1.1523
   0.0446     -1.1651
   0.0517     -1.1675
   0.0595     -1.1593
   0.0680     -1.1490
   0.0773     -1.1334
   0.0875     -1.1104
   0.0984     -1.0865
   0.1104     -1.0638
   0.1232     -1.0307
   0.1371     -0.9881
   0.1519     -0.9108
   0.1679     -0.7844
   0.1849     -0.7769
   0.2029     -0.8077
   0.2221     -0.8280
   0.2423     -0.8427
   0.2636     -0.8465
   0.2859     -0.8418
   0.3092     -0.8288
   0.3333     -0.8087
   0.3582     -0.7852
   0.3839     -0.7626
   0.4101     -0.7440
   0.4369     -0.7319
   0.4639     -0.7247
   0.4912     -0.7194
   0.5185     -0.7148
   0.5458     -0.7077
   0.5728     -0.6933
   0.5994     -0.6708
   0.6256     -0.6481
   0.6510     -0.6216
   0.6758     -0.5832
   0.6997     -0.5372
   0.7227     -0.4866
   0.7446     -0.4365
   0.7656     -0.3872
   0.7855     -0.3412
   0.8043     -0.2976
   0.8220     -0.2573
   0.8386     -0.2199
   0.8542     -0.1850
   0.8687     -0.1531
   0.8823     -0.1237
   0.8948     -0.0967
   0.9065     -0.0721
   0.9172     -0.0500
   0.9271     -0.0300
   0.9363     -0.0125
   0.9446      0.0036
   0.9523      0.0163
   0.9593      0.0285
   0.9658      0.0381
   0.9717      0.0435
   0.9770      0.0489
   0.9819      0.0544
   0.9863      0.0598
   0.9904      0.0650
   0.9940      0.0698
   0.9974      0.0740

WING SECTION 8   Y/BO2 0.847 (Y = 0.49602 m)
     X/C     CP          CF            CFX           CFY           CFZ
   0.9972      0.1209
   0.9937      0.1360
   0.9899      0.1501
   0.9858      0.1632
   0.9812      0.1751
   0.9762      0.1858
   0.9707      0.1950
   0.9647      0.2025
   0.9581      0.2132
   0.9509      0.2236
   0.9430      0.2330
   0.9344      0.2421
   0.9251      0.2508
   0.9150      0.2593
   0.9040      0.2673
   0.8921      0.2748
   0.8793      0.2801
   0.8655      0.2849
   0.8507      0.2844
   0.8348      0.2793
   0.8179      0.2671
   0.7999      0.2508
   0.7809      0.2299
   0.7609      0.2039
   0.7399      0.1717
   0.7178      0.1354
   0.6949      0.0958
   0.6710      0.0538
   0.6463      0.0131
   0.6209     -0.0277
   0.5949     -0.0682
   0.5684     -0.1065
   0.5416     -0.1437
   0.5144     -0.1772
   0.4873     -0.2086
   0.4601     -0.2327
   0.4332     -0.2525
   0.4066     -0.2644
   0.3806     -0.2755
   0.3551     -0.2791
   0.3303     -0.2782
   0.3064     -0.2736
   0.2834     -0.2623
   0.2614     -0.2473
   0.2403     -0.2269
   0.2204     -0.2045
   0.2015     -0.1808
   0.1838     -0.1567
   0.1671     -0.1328
   0.1515     -0.1090
   0.1369     -0.0860
   0.1233     -0.0634
   0.1108     -0.0411
   0.0991     -0.0203
   0.0884     -0.0018
   0.0785      0.0151
   0.0694      0.0326
   0.0611      0.0503
   0.0534      0.0689
   0.0465      0.0874
   0.0401      0.1084
   0.0344      0.1326
   0.0292      0.1627
   0.0245      0.1991
   0.0203      0.2409
   0.0165      0.2933
   0.0132      0.3565
   0.0103      0.4297
   0.0077      0.5108
   0.0056      0.5967
   0.0038      0.6851
   0.0024      0.7662
   0.0013      0.8287
   0.0006      0.8687
   0.0001      0.8635
   0.0000      0.8274
   0.0001      0.7691
   0.0004      0.6814
   0.0010      0.5676
   0.0019      0.4407
   0.0032      0.3101
   0.0047      0.1775
   0.0066      0.0446
   0.0089     -0.0941
   0.0116     -0.2383
   0.0147     -0.3850
   0.0183     -0.5400
   0.0223     -0.7326
   0.0269     -0.9462
   0.0321     -1.0850
   0.0380     -1.1340
   0.0444     -1.1426
   0.0515     -1.1464
   0.0593     -1.1404
   0.0679     -1.1257
   0.0772     -1.1049
   0.0873     -1.0821
   0.0983     -1.0564
   0.1102     -1.0174
   0.1230     -0.9657
   0.1368     -0.8716
   0.1517     -0.7457
   0.1676     -0.7481
   0.1846     -0.7711
   0.2027     -0.7834
   0.2218     -0.7755
   0.2420     -0.7574
   0.2633     -0.7460
   0.2856     -0.7426
   0.3088     -0.7350
   0.3330     -0.7210
   0.3579     -0.7055
   0.3836     -0.6933
   0.4098     -0.6839
   0.4365     -0.6750
   0.4636     -0.6659
   0.4909     -0.6573
   0.5182     -0.6492
   0.5454     -0.6403
   0.5725     -0.6286
   0.5991     -0.6123
   0.6252     -0.5931
   0.6507     -0.5688
   0.6755     -0.5348
   0.6994     -0.4928
   0.7224     -0.4471
   0.7444     -0.4006
   0.7653     -0.3557
   0.7852     -0.3110
   0.8040     -0.2695
   0.8218     -0.2312
   0.8384     -0.1961
   0.8540     -0.1623
   0.8686     -0.1311
   0.8821     -0.1025
   0.8947     -0.0765
   0.9063     -0.0527
   0.9171     -0.0312
   0.9270     -0.0118
   0.9362      0.0057
   0.9446      0.0212
   0.9522      0.0348
   0.9593      0.0467
   0.9657      0.0569
   0.9716      0.0624
   0.9770      0.0680
   0.9819      0.0736
   0.9863      0.0790
   0.9903      0.0842
   0.9940      0.0888
   0.9974      0.0927



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)
