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GOE 701 AIRFOIL (goe701-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 701 AIRFOIL (goe701-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.32 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe701-il-1000000-n5.txt
Download as CSV file: xf-goe701-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 701 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6630   0.09863   0.09642  -0.0630   1.0000   0.0196
 -15.250  -1.0313   0.02863   0.02517  -0.1227   0.9838   0.0146
 -15.000  -1.0238   0.02598   0.02235  -0.1229   0.9797   0.0152
 -14.750  -1.0079   0.02419   0.02042  -0.1232   0.9764   0.0160
 -14.500  -0.9867   0.02274   0.01886  -0.1239   0.9742   0.0168
 -14.250  -0.9632   0.02132   0.01733  -0.1248   0.9726   0.0179
 -14.000  -0.9365   0.02012   0.01604  -0.1261   0.9714   0.0195
 -13.750  -0.9174   0.01926   0.01510  -0.1253   0.9670   0.0208
 -13.500  -0.8939   0.01841   0.01419  -0.1253   0.9636   0.0223
 -13.250  -0.8664   0.01771   0.01341  -0.1259   0.9611   0.0237
 -13.000  -0.8376   0.01701   0.01266  -0.1268   0.9588   0.0250
 -12.750  -0.8134   0.01646   0.01205  -0.1265   0.9550   0.0262
 -12.500  -0.7898   0.01599   0.01152  -0.1260   0.9502   0.0273
 -12.250  -0.7623   0.01553   0.01098  -0.1262   0.9462   0.0282
 -12.000  -0.7342   0.01501   0.01042  -0.1266   0.9426   0.0293
 -11.750  -0.7122   0.01464   0.01001  -0.1256   0.9366   0.0304
 -11.500  -0.6862   0.01428   0.00959  -0.1254   0.9311   0.0314
 -11.250  -0.6593   0.01393   0.00916  -0.1253   0.9260   0.0322
 -11.000  -0.6353   0.01363   0.00879  -0.1246   0.9187   0.0327
 -10.750  -0.6096   0.01323   0.00833  -0.1243   0.9118   0.0337
 -10.500  -0.5852   0.01291   0.00797  -0.1237   0.9035   0.0345
 -10.250  -0.5591   0.01264   0.00764  -0.1233   0.8950   0.0355
 -10.000  -0.5341   0.01238   0.00732  -0.1227   0.8851   0.0363
  -9.750  -0.5085   0.01216   0.00701  -0.1222   0.8754   0.0372
  -9.500  -0.4832   0.01195   0.00672  -0.1217   0.8647   0.0378
  -9.250  -0.4584   0.01171   0.00639  -0.1210   0.8542   0.0385
  -9.000  -0.4339   0.01145   0.00608  -0.1203   0.8444   0.0398
  -8.750  -0.4088   0.01127   0.00585  -0.1197   0.8342   0.0410
  -8.500  -0.3836   0.01108   0.00559  -0.1190   0.8252   0.0417
  -8.000  -0.3332   0.01071   0.00508  -0.1178   0.8081   0.0430
  -7.750  -0.3079   0.01056   0.00486  -0.1171   0.7998   0.0436
  -7.500  -0.2819   0.01041   0.00464  -0.1166   0.7927   0.0441
  -7.250  -0.2569   0.01019   0.00436  -0.1160   0.7849   0.0449
  -7.000  -0.2315   0.00998   0.00410  -0.1154   0.7785   0.0460
  -6.750  -0.2057   0.00980   0.00389  -0.1148   0.7714   0.0469
  -6.500  -0.1801   0.00965   0.00369  -0.1142   0.7649   0.0478
  -6.250  -0.1537   0.00950   0.00351  -0.1138   0.7586   0.0488
  -6.000  -0.1276   0.00938   0.00334  -0.1133   0.7519   0.0498
  -5.750  -0.1014   0.00927   0.00318  -0.1128   0.7460   0.0507
  -5.500  -0.0748   0.00916   0.00303  -0.1124   0.7398   0.0513
  -5.250  -0.0490   0.00901   0.00284  -0.1118   0.7334   0.0528
  -5.000  -0.0228   0.00887   0.00268  -0.1114   0.7278   0.0545
  -4.750   0.0036   0.00875   0.00255  -0.1109   0.7216   0.0562
  -4.500   0.0297   0.00866   0.00242  -0.1104   0.7155   0.0578
  -4.250   0.0564   0.00857   0.00230  -0.1100   0.7100   0.0593
  -4.000   0.0827   0.00846   0.00219  -0.1096   0.7036   0.0626
  -3.750   0.1086   0.00837   0.00209  -0.1090   0.6976   0.0665
  -3.500   0.1354   0.00827   0.00200  -0.1086   0.6916   0.0713
  -3.250   0.1615   0.00820   0.00194  -0.1082   0.6850   0.0777
  -3.000   0.1878   0.00814   0.00189  -0.1077   0.6791   0.0839
  -2.750   0.2144   0.00810   0.00184  -0.1073   0.6717   0.0888
  -2.500   0.2402   0.00808   0.00179  -0.1067   0.6628   0.0923
  -2.250   0.2664   0.00804   0.00175  -0.1062   0.6541   0.0965
  -2.000   0.2922   0.00803   0.00171  -0.1056   0.6453   0.0996
  -1.750   0.3179   0.00804   0.00168  -0.1050   0.6344   0.1016
  -1.500   0.3437   0.00805   0.00164  -0.1044   0.6234   0.1029
  -1.250   0.3689   0.00806   0.00161  -0.1037   0.6124   0.1056
  -1.000   0.3936   0.00808   0.00159  -0.1029   0.5991   0.1091
  -0.750   0.4185   0.00810   0.00158  -0.1022   0.5850   0.1120
  -0.500   0.4431   0.00815   0.00157  -0.1014   0.5701   0.1145
  -0.250   0.4680   0.00819   0.00158  -0.1007   0.5568   0.1167
   0.000   0.4928   0.00824   0.00158  -0.0999   0.5451   0.1200
   0.250   0.5174   0.00828   0.00160  -0.0992   0.5342   0.1251
   0.500   0.5427   0.00830   0.00162  -0.0985   0.5241   0.1299
   0.750   0.5674   0.00835   0.00165  -0.0978   0.5137   0.1355
   1.000   0.5917   0.00839   0.00169  -0.0970   0.5026   0.1461
   1.250   0.6161   0.00843   0.00174  -0.0962   0.4913   0.1587
   1.500   0.6398   0.00851   0.00180  -0.0953   0.4774   0.1706
   1.750   0.6633   0.00860   0.00187  -0.0943   0.4641   0.1815
   2.000   0.6865   0.00870   0.00194  -0.0933   0.4496   0.1924
   2.250   0.7096   0.00881   0.00202  -0.0923   0.4357   0.2012
   2.500   0.7326   0.00892   0.00211  -0.0912   0.4214   0.2111
   2.750   0.7550   0.00904   0.00220  -0.0901   0.4061   0.2219
   3.000   0.7765   0.00919   0.00231  -0.0888   0.3887   0.2351
   3.250   0.7966   0.00937   0.00245  -0.0872   0.3681   0.2551
   3.500   0.8163   0.00949   0.00260  -0.0856   0.3491   0.2970
   3.750   0.8348   0.00959   0.00276  -0.0838   0.3314   0.3592
   4.000   0.8513   0.00965   0.00292  -0.0815   0.3147   0.4324
   4.500   0.9747   0.00962   0.00391  -0.0974   0.2609   0.9981
   4.750   1.0050   0.00993   0.00413  -0.0982   0.2465   1.0000
   5.000   1.0221   0.01013   0.00429  -0.0960   0.2392   1.0000
   5.250   1.0391   0.01031   0.00445  -0.0938   0.2324   1.0000
   5.500   1.0523   0.01054   0.00462  -0.0908   0.2235   1.0000
   5.750   1.0672   0.01073   0.00478  -0.0882   0.2166   1.0000
   6.000   1.0819   0.01097   0.00498  -0.0855   0.2091   1.0000
   6.250   1.0995   0.01115   0.00516  -0.0835   0.2045   1.0000
   6.500   1.1174   0.01135   0.00535  -0.0816   0.2005   1.0000
   6.750   1.1344   0.01160   0.00557  -0.0795   0.1953   1.0000
   7.000   1.1532   0.01181   0.00578  -0.0779   0.1912   1.0000
   7.250   1.1720   0.01204   0.00600  -0.0762   0.1871   1.0000
   7.500   1.1900   0.01230   0.00625  -0.0745   0.1824   1.0000
   7.750   1.2082   0.01258   0.00653  -0.0728   0.1780   1.0000
   8.000   1.2271   0.01284   0.00679  -0.0713   0.1735   1.0000
   8.250   1.2446   0.01316   0.00709  -0.0696   0.1675   1.0000
   8.500   1.2623   0.01350   0.00741  -0.0679   0.1617   1.0000
   8.750   1.2790   0.01388   0.00777  -0.0662   0.1537   1.0000
   9.000   1.2956   0.01429   0.00815  -0.0645   0.1461   1.0000
   9.250   1.3097   0.01483   0.00862  -0.0624   0.1346   1.0000
   9.500   1.3233   0.01542   0.00915  -0.0604   0.1237   1.0000
   9.750   1.3359   0.01607   0.00974  -0.0583   0.1121   1.0000
  10.000   1.3462   0.01687   0.01046  -0.0559   0.0979   1.0000
  10.250   1.3581   0.01761   0.01116  -0.0538   0.0888   1.0000
  10.500   1.3706   0.01834   0.01186  -0.0520   0.0808   1.0000
  10.750   1.3829   0.01912   0.01262  -0.0501   0.0732   1.0000
  11.000   1.3837   0.02062   0.01396  -0.0470   0.0481   1.0000
  11.250   1.3851   0.02216   0.01542  -0.0442   0.0315   1.0000
  11.500   1.3961   0.02313   0.01640  -0.0425   0.0284   1.0000
  11.750   1.4074   0.02410   0.01740  -0.0410   0.0263   1.0000
  12.000   1.4205   0.02498   0.01831  -0.0397   0.0252   1.0000
  12.250   1.4320   0.02599   0.01936  -0.0383   0.0238   1.0000
  12.500   1.4422   0.02712   0.02051  -0.0369   0.0224   1.0000
  12.750   1.4535   0.02818   0.02162  -0.0357   0.0215   1.0000
  13.000   1.4649   0.02926   0.02274  -0.0345   0.0206   1.0000
  13.250   1.4753   0.03046   0.02397  -0.0334   0.0196   1.0000
  13.500   1.4843   0.03178   0.02533  -0.0322   0.0186   1.0000
  13.750   1.4929   0.03316   0.02675  -0.0310   0.0178   1.0000
  14.000   1.5023   0.03452   0.02816  -0.0301   0.0170   1.0000
  14.250   1.5110   0.03596   0.02965  -0.0291   0.0163   1.0000
  14.500   1.5182   0.03757   0.03130  -0.0281   0.0155   1.0000
  14.750   1.5244   0.03930   0.03307  -0.0272   0.0148   1.0000
  15.000   1.5308   0.04106   0.03488  -0.0264   0.0143   1.0000
  15.250   1.5371   0.04284   0.03672  -0.0257   0.0136   1.0000
  15.500   1.5423   0.04480   0.03873  -0.0250   0.0130   1.0000
  15.750   1.5466   0.04689   0.04087  -0.0244   0.0126   1.0000
  16.000   1.5494   0.04916   0.04320  -0.0238   0.0121   1.0000
  16.250   1.5513   0.05158   0.04568  -0.0233   0.0117   1.0000
  16.500   1.5541   0.05397   0.04814  -0.0230   0.0113   1.0000
  16.750   1.5558   0.05652   0.05077  -0.0227   0.0110   1.0000
  17.000   1.5563   0.05927   0.05359  -0.0226   0.0107   1.0000
  17.250   1.5556   0.06219   0.05658  -0.0225   0.0104   1.0000
  17.500   1.5539   0.06530   0.05976  -0.0226   0.0100   1.0000
  17.750   1.5507   0.06865   0.06319  -0.0227   0.0098   1.0000
  18.000   1.5464   0.07221   0.06683  -0.0231   0.0096   1.0000
  18.250   1.5397   0.07614   0.07085  -0.0235   0.0093   1.0000
  18.500   1.5335   0.08006   0.07486  -0.0241   0.0091   1.0000
  18.750   1.5269   0.08410   0.07900  -0.0248   0.0090   1.0000
  19.000   1.5183   0.08851   0.08350  -0.0257   0.0089   1.0000
  19.250   1.5099   0.09290   0.08799  -0.0267   0.0087   1.0000
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