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GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 628 AIRFOIL (goe628-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.79 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe628-il-1000000-n5.txt
Download as CSV file: xf-goe628-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 628 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7469   0.11104   0.10838  -0.0628   1.0000   0.0206
 -18.750  -0.7891   0.10073   0.09794  -0.0690   1.0000   0.0214
 -18.500  -0.8127   0.09373   0.09085  -0.0732   1.0000   0.0218
 -18.250  -0.8380   0.08668   0.08373  -0.0774   1.0000   0.0228
 -18.000  -0.8632   0.07987   0.07685  -0.0814   1.0000   0.0240
 -17.750  -0.8817   0.07424   0.07116  -0.0847   1.0000   0.0249
 -17.500  -0.8974   0.06920   0.06606  -0.0875   1.0000   0.0258
 -17.250  -0.9154   0.06407   0.06088  -0.0903   1.0000   0.0265
 -17.000  -0.9354   0.05903   0.05577  -0.0929   1.0000   0.0271
 -16.750  -0.9600   0.05393   0.05061  -0.0954   1.0000   0.0277
 -16.500  -0.9891   0.04873   0.04533  -0.0976   1.0000   0.0283
 -16.000  -1.0373   0.03528   0.03165  -0.1106   0.9911   0.0288
 -15.750  -1.0459   0.02589   0.02197  -0.1252   0.9799   0.0294
 -15.500  -1.0269   0.02429   0.02032  -0.1269   0.9728   0.0305
 -15.250  -0.9980   0.02315   0.01911  -0.1291   0.9689   0.0316
 -15.000  -0.9685   0.02212   0.01801  -0.1313   0.9648   0.0326
 -14.750  -0.9383   0.02118   0.01698  -0.1333   0.9592   0.0332
 -14.500  -0.9044   0.02042   0.01619  -0.1356   0.9542   0.0340
 -14.250  -0.8725   0.01980   0.01553  -0.1372   0.9470   0.0347
 -14.000  -0.8412   0.01925   0.01492  -0.1385   0.9384   0.0354
 -13.750  -0.8143   0.01875   0.01434  -0.1390   0.9280   0.0360
 -13.500  -0.7885   0.01830   0.01380  -0.1390   0.9169   0.0367
 -13.250  -0.7665   0.01787   0.01328  -0.1384   0.9041   0.0371
 -13.000  -0.7445   0.01747   0.01278  -0.1376   0.8925   0.0374
 -12.750  -0.7242   0.01700   0.01223  -0.1366   0.8789   0.0378
 -12.500  -0.7035   0.01660   0.01175  -0.1356   0.8639   0.0382
 -12.250  -0.6813   0.01630   0.01138  -0.1346   0.8480   0.0386
 -12.000  -0.6587   0.01605   0.01105  -0.1337   0.8300   0.0391
 -11.750  -0.6363   0.01584   0.01073  -0.1326   0.8092   0.0396
 -11.500  -0.6137   0.01566   0.01044  -0.1316   0.7884   0.0401
 -11.000  -0.5691   0.01515   0.00971  -0.1295   0.7530   0.0409
 -10.750  -0.5454   0.01490   0.00937  -0.1287   0.7406   0.0412
 -10.250  -0.4966   0.01445   0.00876  -0.1273   0.7205   0.0419
 -10.000  -0.4725   0.01420   0.00842  -0.1266   0.7115   0.0423
  -9.750  -0.4485   0.01383   0.00801  -0.1259   0.7049   0.0429
  -9.500  -0.4233   0.01358   0.00773  -0.1253   0.6979   0.0434
  -9.250  -0.3985   0.01333   0.00742  -0.1246   0.6908   0.0437
  -9.000  -0.3727   0.01308   0.00713  -0.1241   0.6850   0.0440
  -8.750  -0.3470   0.01284   0.00685  -0.1236   0.6790   0.0443
  -8.500  -0.3215   0.01261   0.00656  -0.1230   0.6728   0.0446
  -8.250  -0.2955   0.01237   0.00627  -0.1225   0.6672   0.0449
  -8.000  -0.2693   0.01214   0.00600  -0.1220   0.6614   0.0452
  -7.750  -0.2432   0.01193   0.00574  -0.1215   0.6553   0.0455
  -7.500  -0.2171   0.01173   0.00549  -0.1210   0.6490   0.0458
  -7.250  -0.1905   0.01153   0.00525  -0.1206   0.6412   0.0461
  -7.000  -0.1646   0.01138   0.00502  -0.1200   0.6320   0.0464
  -6.750  -0.1378   0.01122   0.00480  -0.1196   0.6228   0.0467
  -6.250  -0.0847   0.01094   0.00441  -0.1186   0.6043   0.0471
  -6.000  -0.0582   0.01078   0.00419  -0.1182   0.5970   0.0475
  -5.750  -0.0317   0.01058   0.00395  -0.1177   0.5909   0.0480
  -5.500  -0.0047   0.01042   0.00376  -0.1173   0.5836   0.0485
  -5.250   0.0218   0.01030   0.00359  -0.1168   0.5757   0.0490
  -5.000   0.0491   0.01018   0.00344  -0.1165   0.5688   0.0496
  -4.750   0.0763   0.01008   0.00331  -0.1161   0.5617   0.0502
  -4.500   0.1033   0.01000   0.00318  -0.1157   0.5549   0.0508
  -4.250   0.1307   0.00991   0.00306  -0.1154   0.5473   0.0513
  -4.000   0.1574   0.00986   0.00295  -0.1149   0.5387   0.0519
  -3.750   0.1848   0.00979   0.00285  -0.1146   0.5309   0.0524
  -3.500   0.2119   0.00974   0.00276  -0.1142   0.5230   0.0529
  -3.250   0.2390   0.00967   0.00266  -0.1138   0.5160   0.0538
  -3.000   0.2661   0.00960   0.00256  -0.1134   0.5082   0.0549
  -2.750   0.2928   0.00957   0.00249  -0.1129   0.4999   0.0560
  -2.500   0.3199   0.00953   0.00242  -0.1126   0.4905   0.0573
  -2.250   0.3465   0.00954   0.00238  -0.1121   0.4809   0.0585
  -2.000   0.3734   0.00952   0.00233  -0.1117   0.4715   0.0605
  -1.750   0.3998   0.00950   0.00229  -0.1112   0.4627   0.0647
  -1.500   0.4255   0.00931   0.00220  -0.1107   0.4533   0.1009
  -1.250   0.4511   0.00922   0.00216  -0.1101   0.4441   0.1292
  -1.000   0.4766   0.00913   0.00214  -0.1096   0.4331   0.1599
  -0.750   0.5021   0.00911   0.00215  -0.1090   0.4212   0.1871
  -0.500   0.5275   0.00915   0.00219  -0.1083   0.4094   0.2049
  -0.250   0.5534   0.00920   0.00223  -0.1078   0.3982   0.2179
   0.000   0.5791   0.00927   0.00229  -0.1072   0.3885   0.2304
   0.250   0.6046   0.00934   0.00235  -0.1066   0.3780   0.2427
   0.500   0.6305   0.00942   0.00241  -0.1061   0.3695   0.2517
   0.750   0.6556   0.00951   0.00249  -0.1054   0.3601   0.2646
   1.000   0.6812   0.00959   0.00257  -0.1048   0.3525   0.2763
   1.250   0.7063   0.00970   0.00266  -0.1042   0.3439   0.2867
   1.500   0.7315   0.00979   0.00275  -0.1035   0.3373   0.2951
   1.750   0.7570   0.00988   0.00283  -0.1029   0.3317   0.3029
   2.000   0.7821   0.00999   0.00292  -0.1023   0.3262   0.3084
   2.250   0.8069   0.01009   0.00303  -0.1016   0.3214   0.3165
   2.500   0.8323   0.01017   0.00312  -0.1010   0.3176   0.3244
   2.750   0.8571   0.01026   0.00322  -0.1003   0.3131   0.3337
   3.000   0.8810   0.01039   0.00334  -0.0994   0.3081   0.3408
   3.250   0.9052   0.01052   0.00345  -0.0986   0.3041   0.3469
   3.500   0.9298   0.01059   0.00356  -0.0979   0.3014   0.3540
   3.750   0.9540   0.01069   0.00367  -0.0971   0.2985   0.3609
   4.000   0.9777   0.01081   0.00379  -0.0962   0.2953   0.3666
   4.250   1.0002   0.01093   0.00392  -0.0951   0.2921   0.3743
   4.500   1.0210   0.01107   0.00406  -0.0937   0.2885   0.3825
   4.750   1.0426   0.01116   0.00418  -0.0924   0.2860   0.3901
   5.000   1.0643   0.01125   0.00431  -0.0912   0.2836   0.3991
   5.250   1.0858   0.01137   0.00445  -0.0899   0.2812   0.4071
   5.500   1.1066   0.01151   0.00462  -0.0886   0.2787   0.4185
   5.750   1.1270   0.01167   0.00480  -0.0871   0.2761   0.4300
   6.000   1.1470   0.01184   0.00500  -0.0857   0.2733   0.4443
   6.250   1.1663   0.01202   0.00523  -0.0841   0.2704   0.4610
   6.750   1.2074   0.01223   0.00563  -0.0815   0.2666   0.5262
   7.250   1.2892   0.01196   0.00633  -0.0878   0.2610   1.0000
   7.500   1.3089   0.01221   0.00658  -0.0864   0.2585   1.0000
   7.750   1.3275   0.01251   0.00686  -0.0849   0.2549   1.0000
   8.000   1.3481   0.01275   0.00710  -0.0838   0.2527   1.0000
   8.250   1.3688   0.01299   0.00736  -0.0827   0.2501   1.0000
   8.500   1.3886   0.01328   0.00764  -0.0815   0.2464   1.0000
   8.750   1.4072   0.01362   0.00797  -0.0801   0.2427   1.0000
   9.000   1.4252   0.01400   0.00834  -0.0788   0.2394   1.0000
   9.250   1.4447   0.01433   0.00869  -0.0777   0.2370   1.0000
   9.500   1.4645   0.01465   0.00903  -0.0766   0.2350   1.0000
   9.750   1.4840   0.01500   0.00940  -0.0756   0.2329   1.0000
  10.000   1.5028   0.01539   0.00981  -0.0745   0.2304   1.0000
  10.250   1.5208   0.01584   0.01027  -0.0734   0.2279   1.0000
  10.500   1.5381   0.01634   0.01078  -0.0722   0.2252   1.0000
  10.750   1.5548   0.01689   0.01133  -0.0710   0.2224   1.0000
  11.000   1.5737   0.01733   0.01181  -0.0701   0.2202   1.0000
  11.250   1.5915   0.01785   0.01236  -0.0692   0.2180   1.0000
  11.500   1.6085   0.01842   0.01296  -0.0682   0.2149   1.0000
  11.750   1.6239   0.01910   0.01365  -0.0671   0.2119   1.0000
  12.000   1.6384   0.01986   0.01442  -0.0659   0.2088   1.0000
  12.250   1.6541   0.02057   0.01515  -0.0650   0.2055   1.0000
  12.500   1.6690   0.02133   0.01594  -0.0640   0.2011   1.0000
  12.750   1.6791   0.02243   0.01702  -0.0627   0.1949   1.0000
  13.000   1.6919   0.02339   0.01800  -0.0616   0.1902   1.0000
  13.250   1.7025   0.02453   0.01914  -0.0605   0.1841   1.0000
  13.500   1.7102   0.02590   0.02050  -0.0593   0.1775   1.0000
  13.750   1.7177   0.02734   0.02194  -0.0581   0.1702   1.0000
  14.000   1.7241   0.02891   0.02351  -0.0570   0.1647   1.0000
  14.250   1.7296   0.03058   0.02518  -0.0559   0.1575   1.0000
  14.500   1.7339   0.03240   0.02701  -0.0549   0.1521   1.0000
  14.750   1.7374   0.03431   0.02893  -0.0539   0.1452   1.0000
  15.000   1.7362   0.03669   0.03130  -0.0528   0.1374   1.0000
  15.250   1.7370   0.03894   0.03356  -0.0519   0.1319   1.0000
  15.500   1.7354   0.04147   0.03610  -0.0510   0.1261   1.0000
  15.750   1.7330   0.04413   0.03878  -0.0503   0.1203   1.0000
  16.000   1.7317   0.04673   0.04141  -0.0496   0.1166   1.0000
  16.250   1.7314   0.04927   0.04399  -0.0491   0.1125   1.0000
  16.500   1.7293   0.05208   0.04685  -0.0486   0.1094   1.0000
  16.750   1.7227   0.05541   0.05022  -0.0482   0.1051   1.0000
  17.000   1.7222   0.05812   0.05299  -0.0480   0.1029   1.0000
  17.250   1.7178   0.06131   0.05622  -0.0478   0.0997   1.0000
  17.500   1.7058   0.06542   0.06036  -0.0477   0.0952   1.0000
  17.750   1.7036   0.06848   0.06350  -0.0477   0.0939   1.0000
  18.000   1.6947   0.07233   0.06741  -0.0478   0.0903   1.0000
  18.250   1.6782   0.07717   0.07228  -0.0481   0.0860   1.0000
  18.500   1.6704   0.08103   0.07622  -0.0484   0.0833   1.0000
  18.750   1.6603   0.08518   0.08043  -0.0488   0.0805   1.0000
  19.000   1.6446   0.09010   0.08540  -0.0494   0.0775   1.0000
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