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GOE 593 AIRFOIL (goe593-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 593 AIRFOIL (goe593-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.1 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe593-il-1000000-n5.txt
Download as CSV file: xf-goe593-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 593 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.0205   0.03915   0.03640  -0.0955   1.0000   0.0078
 -15.000  -1.0634   0.03488   0.03195  -0.0933   1.0000   0.0078
 -14.750  -1.0636   0.03196   0.02884  -0.0939   0.9975   0.0079
 -14.500  -1.0478   0.02961   0.02632  -0.0956   0.9951   0.0081
 -14.250  -1.0320   0.02767   0.02422  -0.0962   0.9927   0.0081
 -14.000  -1.0139   0.02608   0.02247  -0.0966   0.9899   0.0083
 -13.750  -0.9917   0.02473   0.02099  -0.0973   0.9878   0.0084
 -13.500  -0.9686   0.02321   0.01933  -0.0983   0.9860   0.0087
 -13.250  -0.9484   0.02204   0.01805  -0.0982   0.9827   0.0089
 -13.000  -0.9261   0.02098   0.01690  -0.0982   0.9792   0.0092
 -12.750  -0.9001   0.02004   0.01587  -0.0988   0.9769   0.0096
 -12.500  -0.8722   0.01916   0.01489  -0.0997   0.9753   0.0099
 -12.250  -0.8536   0.01845   0.01410  -0.0984   0.9691   0.0102
 -12.000  -0.8274   0.01775   0.01331  -0.0986   0.9659   0.0106
 -11.750  -0.7994   0.01706   0.01253  -0.0992   0.9638   0.0109
 -11.500  -0.7795   0.01639   0.01179  -0.0980   0.9567   0.0114
 -11.250  -0.7510   0.01575   0.01109  -0.0986   0.9534   0.0119
 -11.000  -0.7195   0.01517   0.01045  -0.0997   0.9510   0.0125
 -10.750  -0.6918   0.01467   0.00988  -0.1000   0.9455   0.0130
 -10.500  -0.6586   0.01416   0.00929  -0.1014   0.9418   0.0136
 -10.250  -0.6232   0.01363   0.00871  -0.1033   0.9386   0.0143
 -10.000  -0.5892   0.01323   0.00827  -0.1049   0.9341   0.0152
  -9.750  -0.5560   0.01284   0.00782  -0.1062   0.9282   0.0160
  -9.500  -0.5216   0.01249   0.00740  -0.1078   0.9226   0.0169
  -9.250  -0.4919   0.01215   0.00701  -0.1083   0.9155   0.0177
  -9.000  -0.4614   0.01190   0.00673  -0.1089   0.9085   0.0186
  -8.750  -0.4335   0.01167   0.00644  -0.1090   0.9013   0.0194
  -8.500  -0.4063   0.01144   0.00614  -0.1089   0.8938   0.0201
  -8.250  -0.3794   0.01123   0.00586  -0.1087   0.8873   0.0207
  -8.000  -0.3543   0.01096   0.00555  -0.1082   0.8798   0.0216
  -7.750  -0.3280   0.01076   0.00530  -0.1078   0.8727   0.0223
  -7.500  -0.3026   0.01058   0.00510  -0.1073   0.8653   0.0231
  -7.250  -0.2767   0.01041   0.00486  -0.1068   0.8581   0.0238
  -7.000  -0.2512   0.01024   0.00464  -0.1063   0.8507   0.0246
  -6.750  -0.2256   0.01009   0.00443  -0.1057   0.8426   0.0251
  -6.500  -0.2006   0.00988   0.00416  -0.1051   0.8345   0.0256
  -6.250  -0.1761   0.00964   0.00387  -0.1043   0.8260   0.0267
  -6.000  -0.1509   0.00946   0.00367  -0.1037   0.8171   0.0275
  -5.750  -0.1258   0.00931   0.00346  -0.1030   0.8075   0.0282
  -5.500  -0.1007   0.00918   0.00328  -0.1024   0.7971   0.0291
  -5.250  -0.0756   0.00904   0.00309  -0.1017   0.7870   0.0297
  -5.000  -0.0507   0.00893   0.00291  -0.1009   0.7761   0.0302
  -4.750  -0.0258   0.00883   0.00274  -0.1002   0.7645   0.0308
  -4.500  -0.0014   0.00867   0.00252  -0.0994   0.7520   0.0321
  -4.250   0.0228   0.00858   0.00237  -0.0985   0.7373   0.0331
  -4.000   0.0465   0.00852   0.00223  -0.0975   0.7194   0.0341
  -3.750   0.0706   0.00847   0.00210  -0.0966   0.7031   0.0352
  -3.500   0.0954   0.00842   0.00199  -0.0958   0.6897   0.0364
  -3.250   0.1205   0.00835   0.00188  -0.0951   0.6792   0.0382
  -3.000   0.1456   0.00827   0.00178  -0.0945   0.6690   0.0413
  -2.750   0.1712   0.00821   0.00169  -0.0939   0.6595   0.0446
  -2.500   0.1960   0.00814   0.00160  -0.0932   0.6491   0.0521
  -2.000   0.2456   0.00796   0.00148  -0.0918   0.6269   0.0855
  -1.750   0.2706   0.00793   0.00144  -0.0911   0.6164   0.0986
  -1.500   0.2959   0.00791   0.00141  -0.0905   0.6050   0.1084
  -1.250   0.3216   0.00789   0.00139  -0.0899   0.5955   0.1180
  -1.000   0.3467   0.00788   0.00136  -0.0893   0.5854   0.1282
  -0.750   0.3721   0.00787   0.00135  -0.0887   0.5740   0.1387
  -0.500   0.3973   0.00784   0.00133  -0.0881   0.5636   0.1563
  -0.250   0.4213   0.00776   0.00134  -0.0873   0.5516   0.1953
   0.000   0.4442   0.00766   0.00136  -0.0863   0.5360   0.2617
   0.250   0.4675   0.00759   0.00138  -0.0853   0.5205   0.3125
   0.500   0.4896   0.00749   0.00141  -0.0842   0.5030   0.3831
   0.750   0.5105   0.00734   0.00146  -0.0828   0.4856   0.4868
   1.000   0.5319   0.00729   0.00152  -0.0815   0.4670   0.5564
   1.250   0.5521   0.00721   0.00160  -0.0799   0.4491   0.6367
   1.500   0.5711   0.00714   0.00169  -0.0780   0.4315   0.7186
   1.750   0.5869   0.00700   0.00180  -0.0753   0.4148   0.8246
   2.000   0.6249   0.00702   0.00202  -0.0775   0.3947   0.9357
   2.250   0.6857   0.00731   0.00221  -0.0850   0.3736   0.9640
   2.500   0.7255   0.00753   0.00235  -0.0877   0.3588   0.9755
   2.750   0.7631   0.00775   0.00250  -0.0900   0.3460   0.9875
   3.250   0.8330   0.00813   0.00275  -0.0933   0.3240   0.9975
   3.500   0.8686   0.00832   0.00288  -0.0952   0.3143   0.9998
   3.750   0.8904   0.00848   0.00299  -0.0940   0.3046   1.0000
   4.000   0.9106   0.00862   0.00311  -0.0924   0.2963   1.0000
   4.250   0.9302   0.00880   0.00323  -0.0907   0.2876   1.0000
   4.500   0.9504   0.00895   0.00335  -0.0892   0.2786   1.0000
   4.750   0.9699   0.00914   0.00350  -0.0875   0.2693   1.0000
   5.000   0.9902   0.00930   0.00363  -0.0859   0.2614   1.0000
   5.250   1.0100   0.00949   0.00378  -0.0843   0.2543   1.0000
   5.500   1.0308   0.00963   0.00392  -0.0829   0.2489   1.0000
   5.750   1.0507   0.00982   0.00409  -0.0814   0.2422   1.0000
   6.000   1.0710   0.01000   0.00425  -0.0799   0.2357   1.0000
   6.250   1.0907   0.01021   0.00443  -0.0783   0.2283   1.0000
   6.500   1.1104   0.01041   0.00462  -0.0767   0.2220   1.0000
   6.750   1.1294   0.01059   0.00480  -0.0750   0.2164   1.0000
   7.000   1.1460   0.01084   0.00500  -0.0728   0.2081   1.0000
   7.250   1.1635   0.01106   0.00521  -0.0708   0.1996   1.0000
   7.500   1.1810   0.01130   0.00543  -0.0689   0.1924   1.0000
   7.750   1.1984   0.01157   0.00567  -0.0669   0.1832   1.0000
   8.000   1.2155   0.01187   0.00594  -0.0650   0.1722   1.0000
   8.250   1.2314   0.01224   0.00625  -0.0629   0.1585   1.0000
   8.500   1.2443   0.01277   0.00667  -0.0604   0.1382   1.0000
   9.000   1.2604   0.01439   0.00795  -0.0540   0.0817   1.0000
   9.250   1.2737   0.01498   0.00848  -0.0517   0.0702   1.0000
   9.500   1.2884   0.01551   0.00899  -0.0497   0.0626   1.0000
   9.750   1.3029   0.01607   0.00952  -0.0478   0.0568   1.0000
  10.000   1.3197   0.01651   0.00998  -0.0463   0.0539   1.0000
  10.250   1.3358   0.01700   0.01048  -0.0447   0.0510   1.0000
  10.500   1.3505   0.01757   0.01106  -0.0430   0.0479   1.0000
  10.750   1.3661   0.01811   0.01163  -0.0414   0.0454   1.0000
  11.000   1.3824   0.01863   0.01218  -0.0400   0.0439   1.0000
  11.250   1.3972   0.01923   0.01280  -0.0385   0.0416   1.0000
  11.500   1.4105   0.01995   0.01352  -0.0369   0.0389   1.0000
  11.750   1.4251   0.02060   0.01421  -0.0355   0.0373   1.0000
  12.000   1.4393   0.02129   0.01494  -0.0341   0.0353   1.0000
  12.250   1.4516   0.02212   0.01578  -0.0325   0.0326   1.0000
  12.500   1.4634   0.02301   0.01668  -0.0310   0.0296   1.0000
  12.750   1.4740   0.02400   0.01768  -0.0295   0.0265   1.0000
  13.000   1.4841   0.02504   0.01875  -0.0280   0.0234   1.0000
  13.250   1.4905   0.02639   0.02010  -0.0263   0.0189   1.0000
  13.500   1.4967   0.02780   0.02152  -0.0247   0.0161   1.0000
  13.750   1.5030   0.02926   0.02302  -0.0233   0.0143   1.0000
  14.000   1.5100   0.03071   0.02452  -0.0220   0.0132   1.0000
  14.250   1.5154   0.03233   0.02619  -0.0208   0.0121   1.0000
  14.500   1.5199   0.03410   0.02802  -0.0196   0.0112   1.0000
  14.750   1.5252   0.03585   0.02984  -0.0187   0.0106   1.0000
  15.000   1.5299   0.03772   0.03179  -0.0178   0.0102   1.0000
  15.250   1.5330   0.03980   0.03393  -0.0171   0.0096   1.0000
  15.500   1.5351   0.04205   0.03625  -0.0164   0.0092   1.0000
  15.750   1.5359   0.04451   0.03878  -0.0159   0.0088   1.0000
  16.000   1.5358   0.04714   0.04149  -0.0155   0.0085   1.0000
  16.250   1.5364   0.04975   0.04418  -0.0153   0.0081   1.0000
  16.500   1.5354   0.05264   0.04715  -0.0151   0.0078   1.0000
  16.750   1.5338   0.05565   0.05026  -0.0152   0.0076   1.0000
  17.000   1.5305   0.05895   0.05364  -0.0154   0.0074   1.0000
  17.250   1.5259   0.06248   0.05726  -0.0157   0.0073   1.0000
  17.500   1.5193   0.06637   0.06125  -0.0162   0.0071   1.0000
  17.750   1.5115   0.07052   0.06549  -0.0169   0.0069   1.0000
  18.000   1.5008   0.07512   0.07019  -0.0179   0.0066   1.0000
  18.250   1.4903   0.07982   0.07500  -0.0190   0.0065   1.0000
  18.500   1.4813   0.08438   0.07966  -0.0201   0.0065   1.0000
  18.750   1.4715   0.08913   0.08452  -0.0215   0.0064   1.0000
  19.000   1.4603   0.09410   0.08960  -0.0229   0.0063   1.0000
  19.250   1.4487   0.09921   0.09480  -0.0245   0.0062   1.0000
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