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GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 738 AIRFOIL (goe738-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.59 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe738-il-1000000-n5.txt
Download as CSV file: xf-goe738-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 738 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.2043   0.09380   0.09057  -0.0190   1.0000   0.0238
 -19.250  -1.2434   0.08376   0.08038  -0.0251   1.0000   0.0239
 -19.000  -1.2812   0.07413   0.07058  -0.0309   1.0000   0.0240
 -18.750  -1.3126   0.06573   0.06202  -0.0360   1.0000   0.0240
 -18.500  -1.3366   0.05860   0.05473  -0.0402   1.0000   0.0240
 -18.250  -1.3515   0.05309   0.04911  -0.0433   1.0000   0.0243
 -18.000  -1.3637   0.04820   0.04410  -0.0459   1.0000   0.0244
 -17.750  -1.3722   0.04409   0.03988  -0.0478   1.0000   0.0245
 -17.500  -1.3753   0.04086   0.03656  -0.0490   1.0000   0.0247
 -17.250  -1.3785   0.03785   0.03345  -0.0498   1.0000   0.0249
 -17.000  -1.3782   0.03542   0.03093  -0.0500   1.0000   0.0251
 -16.750  -1.3764   0.03329   0.02872  -0.0499   1.0000   0.0252
 -16.500  -1.3724   0.03151   0.02687  -0.0494   1.0000   0.0255
 -16.250  -1.3671   0.02994   0.02523  -0.0487   1.0000   0.0258
 -16.000  -1.3625   0.02844   0.02365  -0.0477   1.0000   0.0259
 -15.750  -1.3559   0.02717   0.02231  -0.0464   1.0000   0.0261
 -15.500  -1.3487   0.02603   0.02110  -0.0450   1.0000   0.0263
 -15.250  -1.3399   0.02505   0.02006  -0.0435   1.0000   0.0264
 -14.750  -1.3262   0.02317   0.01806  -0.0392   0.9922   0.0269
 -14.500  -1.3025   0.02241   0.01701  -0.0400   0.8591   0.0273
 -14.250  -1.2946   0.02181   0.01628  -0.0373   0.8299   0.0275
 -14.000  -1.2845   0.02124   0.01560  -0.0349   0.8112   0.0279
 -13.750  -1.2730   0.02071   0.01499  -0.0325   0.7973   0.0281
 -13.500  -1.2608   0.02020   0.01440  -0.0301   0.7850   0.0284
 -13.250  -1.2473   0.01974   0.01387  -0.0278   0.7752   0.0287
 -12.750  -1.2156   0.01890   0.01289  -0.0240   0.7573   0.0294
 -12.500  -1.1971   0.01848   0.01239  -0.0225   0.7491   0.0297
 -12.250  -1.1776   0.01807   0.01192  -0.0211   0.7420   0.0300
 -12.000  -1.1573   0.01767   0.01146  -0.0199   0.7346   0.0303
 -11.750  -1.1365   0.01731   0.01101  -0.0187   0.7279   0.0305
 -11.500  -1.1158   0.01687   0.01053  -0.0175   0.7214   0.0309
 -11.250  -1.0948   0.01645   0.01007  -0.0164   0.7145   0.0314
 -11.000  -1.0728   0.01607   0.00965  -0.0153   0.7085   0.0320
 -10.750  -1.0501   0.01571   0.00926  -0.0144   0.7026   0.0325
 -10.500  -1.0270   0.01539   0.00889  -0.0135   0.6959   0.0330
 -10.250  -1.0035   0.01507   0.00852  -0.0127   0.6903   0.0335
 -10.000  -0.9795   0.01477   0.00818  -0.0119   0.6844   0.0340
  -9.750  -0.9553   0.01448   0.00785  -0.0112   0.6780   0.0345
  -9.500  -0.9308   0.01422   0.00753  -0.0105   0.6722   0.0349
  -9.250  -0.9065   0.01389   0.00717  -0.0097   0.6666   0.0357
  -9.000  -0.8819   0.01359   0.00685  -0.0091   0.6606   0.0365
  -8.500  -0.8315   0.01308   0.00629  -0.0079   0.6493   0.0383
  -8.250  -0.8058   0.01285   0.00603  -0.0073   0.6431   0.0392
  -8.000  -0.7801   0.01263   0.00576  -0.0068   0.6374   0.0401
  -7.750  -0.7544   0.01238   0.00550  -0.0062   0.6324   0.0413
  -7.500  -0.7285   0.01215   0.00526  -0.0057   0.6262   0.0427
  -7.250  -0.7023   0.01195   0.00503  -0.0053   0.6197   0.0440
  -7.000  -0.6757   0.01177   0.00481  -0.0048   0.6142   0.0452
  -6.750  -0.6495   0.01155   0.00459  -0.0044   0.6085   0.0469
  -6.500  -0.6230   0.01136   0.00438  -0.0040   0.6024   0.0488
  -6.250  -0.5962   0.01119   0.00419  -0.0036   0.5967   0.0505
  -6.000  -0.5694   0.01102   0.00400  -0.0032   0.5904   0.0524
  -5.750  -0.5427   0.01084   0.00382  -0.0028   0.5838   0.0550
  -5.500  -0.5156   0.01069   0.00365  -0.0025   0.5786   0.0573
  -5.250  -0.4885   0.01053   0.00349  -0.0021   0.5729   0.0596
  -5.000  -0.4616   0.01038   0.00333  -0.0018   0.5667   0.0624
  -4.750  -0.4342   0.01025   0.00318  -0.0015   0.5611   0.0650
  -4.500  -0.4070   0.01010   0.00303  -0.0012   0.5548   0.0681
  -4.250  -0.3798   0.00997   0.00289  -0.0009   0.5485   0.0719
  -4.000  -0.3523   0.00984   0.00276  -0.0006   0.5433   0.0755
  -3.750  -0.3251   0.00969   0.00263  -0.0003   0.5380   0.0811
  -3.500  -0.2978   0.00955   0.00250   0.0000   0.5323   0.0875
  -3.250  -0.2708   0.00939   0.00237   0.0003   0.5269   0.0983
  -3.000  -0.2440   0.00920   0.00226   0.0006   0.5203   0.1170
  -2.750  -0.2169   0.00909   0.00217   0.0009   0.5112   0.1327
  -2.500  -0.1895   0.00897   0.00209   0.0012   0.5039   0.1450
  -2.250  -0.1618   0.00887   0.00201   0.0014   0.4976   0.1549
  -2.000  -0.1339   0.00882   0.00195   0.0016   0.4924   0.1628
  -1.750  -0.1062   0.00871   0.00189   0.0018   0.4875   0.1734
  -1.500  -0.0783   0.00864   0.00183   0.0020   0.4808   0.1835
  -1.250  -0.0507   0.00858   0.00178   0.0022   0.4743   0.1954
  -1.000  -0.0231   0.00847   0.00173   0.0024   0.4690   0.2131
  -0.750   0.0043   0.00838   0.00169   0.0026   0.4625   0.2331
  -0.500   0.0313   0.00827   0.00165   0.0029   0.4556   0.2600
  -0.250   0.0583   0.00813   0.00162   0.0032   0.4488   0.2929
   0.000   0.0850   0.00800   0.00159   0.0036   0.4415   0.3293
   0.250   0.1117   0.00785   0.00156   0.0039   0.4357   0.3697
   0.500   0.1379   0.00767   0.00154   0.0043   0.4304   0.4201
   0.750   0.1635   0.00748   0.00153   0.0048   0.4251   0.4808
   1.000   0.1898   0.00735   0.00154   0.0053   0.4205   0.5282
   1.250   0.2167   0.00725   0.00155   0.0056   0.4156   0.5647
   1.500   0.2436   0.00720   0.00157   0.0060   0.4101   0.5945
   1.750   0.2706   0.00717   0.00160   0.0063   0.4047   0.6218
   2.000   0.2976   0.00712   0.00164   0.0066   0.3998   0.6490
   2.250   0.3246   0.00709   0.00168   0.0070   0.3938   0.6765
   2.500   0.3507   0.00708   0.00173   0.0075   0.3875   0.7082
   2.750   0.3774   0.00706   0.00179   0.0079   0.3802   0.7352
   3.000   0.4030   0.00708   0.00186   0.0085   0.3703   0.7667
   3.250   0.4285   0.00707   0.00194   0.0091   0.3597   0.8003
   3.500   0.4538   0.00707   0.00203   0.0098   0.3500   0.8344
   3.750   0.4796   0.00709   0.00214   0.0105   0.3387   0.8742
   4.000   0.5103   0.00720   0.00229   0.0100   0.3205   0.9095
   4.250   0.5472   0.00750   0.00250   0.0080   0.2921   0.9307
   4.500   0.5855   0.00779   0.00271   0.0057   0.2728   0.9425
   4.750   0.6214   0.00808   0.00291   0.0038   0.2551   0.9514
   5.000   0.6576   0.00835   0.00311   0.0020   0.2417   0.9568
   5.250   0.6916   0.00855   0.00328   0.0007   0.2339   0.9621
   5.750   0.7532   0.00899   0.00364  -0.0007   0.2200   0.9720
   6.000   0.7844   0.00919   0.00382  -0.0014   0.2143   0.9761
   6.250   0.8117   0.00942   0.00402  -0.0014   0.2086   0.9812
   6.500   0.8456   0.00961   0.00420  -0.0028   0.2035   0.9830
   6.750   0.8788   0.00980   0.00437  -0.0040   0.1986   0.9852
   7.000   0.9108   0.01004   0.00458  -0.0050   0.1931   0.9877
   7.250   0.9422   0.01025   0.00478  -0.0059   0.1886   0.9904
   7.500   0.9730   0.01047   0.00499  -0.0066   0.1828   0.9929
   7.750   1.0070   0.01076   0.00523  -0.0082   0.1733   0.9947
   8.000   1.0395   0.01114   0.00552  -0.0096   0.1571   0.9967
   8.250   1.0696   0.01172   0.00595  -0.0108   0.1339   0.9985
   8.500   1.0998   0.01225   0.00638  -0.0119   0.1191   0.9999
   8.750   1.1192   0.01270   0.00678  -0.0107   0.1101   1.0000
   9.000   1.1383   0.01306   0.00713  -0.0093   0.1042   1.0000
   9.250   1.1556   0.01350   0.00753  -0.0078   0.0980   1.0000
   9.500   1.1737   0.01387   0.00790  -0.0063   0.0920   1.0000
   9.750   1.1889   0.01438   0.00836  -0.0045   0.0838   1.0000
  10.000   1.2017   0.01496   0.00889  -0.0023   0.0743   1.0000
  10.250   1.2138   0.01554   0.00943  -0.0001   0.0680   1.0000
  10.500   1.2263   0.01606   0.00994   0.0021   0.0648   1.0000
  10.750   1.2327   0.01661   0.01050   0.0052   0.0624   1.0000
  11.000   1.2348   0.01727   0.01118   0.0087   0.0605   1.0000
  11.250   1.2429   0.01801   0.01196   0.0108   0.0595   1.0000
  11.500   1.2529   0.01886   0.01284   0.0122   0.0584   1.0000
  11.750   1.2636   0.01979   0.01380   0.0134   0.0573   1.0000
  12.000   1.2732   0.02090   0.01493   0.0145   0.0558   1.0000
  12.250   1.2830   0.02206   0.01612   0.0154   0.0546   1.0000
  12.500   1.2925   0.02330   0.01738   0.0162   0.0531   1.0000
  12.750   1.3041   0.02442   0.01854   0.0168   0.0527   1.0000
  13.000   1.3155   0.02559   0.01976   0.0174   0.0520   1.0000
  13.250   1.3256   0.02689   0.02110   0.0179   0.0511   1.0000
  13.500   1.3350   0.02827   0.02252   0.0184   0.0505   1.0000
  13.750   1.3431   0.02979   0.02408   0.0188   0.0496   1.0000
  14.000   1.3497   0.03147   0.02580   0.0192   0.0488   1.0000
  14.250   1.3569   0.03312   0.02750   0.0196   0.0484   1.0000
  14.500   1.3617   0.03503   0.02944   0.0198   0.0475   1.0000
  14.750   1.3648   0.03712   0.03158   0.0201   0.0466   1.0000
  15.000   1.3728   0.03878   0.03330   0.0202   0.0460   1.0000
  15.250   1.3778   0.04077   0.03535   0.0203   0.0459   1.0000
  15.500   1.3838   0.04271   0.03735   0.0203   0.0455   1.0000
  15.750   1.3885   0.04486   0.03955   0.0202   0.0451   1.0000
  16.000   1.3928   0.04709   0.04184   0.0200   0.0443   1.0000
  16.250   1.3966   0.04939   0.04420   0.0198   0.0440   1.0000
  16.500   1.3990   0.05189   0.04676   0.0194   0.0433   1.0000
  16.750   1.4001   0.05459   0.04950   0.0190   0.0425   1.0000
  17.000   1.4007   0.05736   0.05232   0.0186   0.0417   1.0000
  17.250   1.3998   0.06036   0.05537   0.0180   0.0410   1.0000
  17.500   1.3991   0.06339   0.05847   0.0173   0.0406   1.0000
  17.750   1.4018   0.06602   0.06116   0.0168   0.0401   1.0000
  18.000   1.4022   0.06895   0.06416   0.0161   0.0394   1.0000
  18.250   1.4016   0.07206   0.06733   0.0153   0.0390   1.0000
  18.500   1.4011   0.07516   0.07049   0.0145   0.0380   1.0000
  18.750   1.3978   0.07869   0.07409   0.0135   0.0373   1.0000
  19.000   1.3935   0.08236   0.07781   0.0124   0.0363   1.0000
  19.250   1.3883   0.08620   0.08170   0.0112   0.0356   1.0000
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