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GOE 413 AIRFOIL (goe413-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 413 AIRFOIL (goe413-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.56 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe413-il-1000000-n5.txt
Download as CSV file: xf-goe413-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 413 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8468   0.10768   0.10512  -0.0374   1.0000   0.0318
 -17.250  -0.9074   0.09345   0.09065  -0.0465   1.0000   0.0322
 -17.000  -0.9345   0.08525   0.08230  -0.0518   1.0000   0.0324
 -16.750  -0.9556   0.07820   0.07513  -0.0566   1.0000   0.0325
 -16.500  -0.9736   0.07181   0.06863  -0.0609   1.0000   0.0326
 -16.250  -0.9908   0.06587   0.06259  -0.0651   1.0000   0.0327
 -16.000  -1.0072   0.06040   0.05691  -0.0689   0.9244   0.0328
 -15.750  -1.0231   0.05535   0.05163  -0.0719   0.8929   0.0328
 -15.250  -1.0427   0.04581   0.04179  -0.0790   0.8646   0.0329
 -15.000  -1.0481   0.04136   0.03718  -0.0827   0.8540   0.0330
 -14.750  -1.0512   0.03690   0.03260  -0.0870   0.8450   0.0331
 -14.500  -1.0487   0.03290   0.02846  -0.0915   0.8363   0.0333
 -14.250  -1.0404   0.02918   0.02461  -0.0969   0.8298   0.0334
 -14.000  -1.0268   0.02671   0.02202  -0.1009   0.8244   0.0335
 -13.750  -1.0081   0.02541   0.02063  -0.1022   0.8193   0.0336
 -13.250  -0.9653   0.02346   0.01853  -0.1036   0.8105   0.0339
 -13.000  -0.9422   0.02266   0.01768  -0.1041   0.8064   0.0341
 -12.750  -0.9184   0.02192   0.01689  -0.1045   0.8022   0.0342
 -12.500  -0.8941   0.02126   0.01615  -0.1049   0.7978   0.0344
 -12.250  -0.8693   0.02063   0.01546  -0.1051   0.7935   0.0346
 -12.000  -0.8438   0.02003   0.01481  -0.1054   0.7894   0.0348
 -11.750  -0.8179   0.01949   0.01422  -0.1057   0.7846   0.0350
 -11.500  -0.7918   0.01898   0.01365  -0.1059   0.7798   0.0352
 -11.250  -0.7655   0.01847   0.01308  -0.1061   0.7750   0.0355
 -11.000  -0.7388   0.01795   0.01250  -0.1063   0.7705   0.0357
 -10.750  -0.7121   0.01744   0.01194  -0.1065   0.7644   0.0359
 -10.500  -0.6852   0.01697   0.01140  -0.1067   0.7574   0.0361
 -10.250  -0.6579   0.01652   0.01088  -0.1069   0.7511   0.0363
 -10.000  -0.6304   0.01608   0.01039  -0.1071   0.7433   0.0365
  -9.750  -0.6029   0.01569   0.00992  -0.1072   0.7351   0.0367
  -9.500  -0.5750   0.01531   0.00947  -0.1074   0.7247   0.0368
  -9.250  -0.5471   0.01497   0.00905  -0.1075   0.7120   0.0369
  -9.000  -0.5195   0.01456   0.00855  -0.1077   0.6954   0.0371
  -8.750  -0.4920   0.01416   0.00806  -0.1078   0.6779   0.0374
  -8.500  -0.4639   0.01385   0.00767  -0.1080   0.6628   0.0377
  -8.250  -0.4355   0.01357   0.00733  -0.1081   0.6510   0.0379
  -8.000  -0.4070   0.01335   0.00705  -0.1083   0.6404   0.0382
  -7.750  -0.3781   0.01313   0.00678  -0.1085   0.6318   0.0385
  -7.500  -0.3493   0.01293   0.00653  -0.1086   0.6231   0.0388
  -7.250  -0.3204   0.01270   0.00626  -0.1088   0.6163   0.0391
  -7.000  -0.2913   0.01247   0.00599  -0.1090   0.6095   0.0394
  -6.750  -0.2623   0.01227   0.00573  -0.1092   0.6035   0.0397
  -6.500  -0.2331   0.01205   0.00548  -0.1094   0.5989   0.0400
  -6.250  -0.2037   0.01184   0.00524  -0.1096   0.5943   0.0403
  -6.000  -0.1744   0.01165   0.00501  -0.1097   0.5891   0.0406
  -5.750  -0.1451   0.01148   0.00479  -0.1099   0.5836   0.0409
  -5.500  -0.1156   0.01132   0.00459  -0.1101   0.5793   0.0411
  -5.250  -0.0859   0.01115   0.00441  -0.1103   0.5756   0.0413
  -5.000  -0.0564   0.01092   0.00415  -0.1106   0.5713   0.0417
  -4.750  -0.0269   0.01073   0.00394  -0.1108   0.5666   0.0422
  -4.250   0.0324   0.01047   0.00364  -0.1112   0.5585   0.0431
  -4.000   0.0622   0.01034   0.00350  -0.1114   0.5547   0.0436
  -3.750   0.0919   0.01022   0.00337  -0.1116   0.5501   0.0441
  -3.500   0.1215   0.01012   0.00324  -0.1118   0.5452   0.0446
  -3.250   0.1512   0.01004   0.00312  -0.1120   0.5401   0.0451
  -3.000   0.1811   0.00993   0.00301  -0.1122   0.5355   0.0455
  -2.750   0.2108   0.00985   0.00291  -0.1124   0.5305   0.0459
  -2.500   0.2405   0.00977   0.00280  -0.1126   0.5259   0.0464
  -2.250   0.2702   0.00967   0.00268  -0.1128   0.5215   0.0472
  -2.000   0.3001   0.00957   0.00259  -0.1130   0.5183   0.0479
  -1.750   0.3300   0.00950   0.00251  -0.1133   0.5140   0.0486
  -1.500   0.3597   0.00945   0.00245  -0.1134   0.5098   0.0495
  -1.250   0.3893   0.00942   0.00240  -0.1136   0.5053   0.0505
  -1.000   0.4190   0.00939   0.00236  -0.1138   0.5012   0.0512
  -0.750   0.4489   0.00931   0.00229  -0.1140   0.4973   0.0524
  -0.500   0.4787   0.00927   0.00225  -0.1142   0.4932   0.0538
  -0.250   0.5083   0.00925   0.00222  -0.1144   0.4885   0.0553
   0.250   0.5675   0.00920   0.00218  -0.1148   0.4796   0.0611
   0.500   0.5975   0.00892   0.00211  -0.1152   0.4751   0.1318
   0.750   0.6270   0.00887   0.00213  -0.1155   0.4694   0.1562
   1.000   0.6563   0.00886   0.00216  -0.1157   0.4626   0.1741
   1.250   0.6857   0.00886   0.00219  -0.1158   0.4550   0.1894
   1.500   0.7148   0.00889   0.00223  -0.1160   0.4483   0.2058
   1.750   0.7442   0.00889   0.00228  -0.1162   0.4403   0.2250
   2.000   0.7728   0.00895   0.00235  -0.1163   0.4286   0.2510
   2.250   0.8020   0.00894   0.00242  -0.1165   0.4197   0.2858
   2.500   0.8307   0.00900   0.00252  -0.1166   0.4109   0.3124
   2.750   0.8595   0.00906   0.00261  -0.1168   0.4013   0.3340
   3.000   0.8878   0.00918   0.00272  -0.1168   0.3900   0.3553
   3.500   0.9434   0.00949   0.00301  -0.1168   0.3611   0.4017
   3.750   0.9711   0.00963   0.00317  -0.1168   0.3470   0.4340
   4.000   0.9989   0.00975   0.00336  -0.1168   0.3356   0.4783
   4.250   1.0261   0.00993   0.00356  -0.1168   0.3237   0.5176
   4.500   1.0538   0.01009   0.00374  -0.1168   0.3131   0.5453
   4.750   1.0808   0.01029   0.00394  -0.1166   0.3026   0.5699
   5.000   1.1076   0.01051   0.00416  -0.1165   0.2909   0.5965
   5.250   1.1342   0.01071   0.00439  -0.1164   0.2772   0.6329
   5.500   1.1604   0.01085   0.00468  -0.1162   0.2641   0.7134
   5.750   1.1851   0.01103   0.00499  -0.1157   0.2496   0.8029
   6.000   1.2057   0.01121   0.00531  -0.1143   0.2340   0.8921
   6.250   1.2253   0.01150   0.00559  -0.1127   0.2158   1.0000
   6.500   1.2473   0.01210   0.00602  -0.1120   0.1927   1.0000
   6.750   1.2665   0.01287   0.00660  -0.1108   0.1619   1.0000
   7.000   1.2690   0.01479   0.00802  -0.1076   0.0816   1.0000
   7.250   1.2876   0.01546   0.00860  -0.1063   0.0687   1.0000
   7.500   1.3089   0.01590   0.00902  -0.1055   0.0649   1.0000
   7.750   1.3280   0.01637   0.00947  -0.1042   0.0622   1.0000
   8.000   1.3466   0.01683   0.00993  -0.1029   0.0603   1.0000
   8.250   1.3654   0.01731   0.01041  -0.1017   0.0591   1.0000
   8.500   1.3836   0.01784   0.01095  -0.1006   0.0581   1.0000
   8.750   1.4012   0.01844   0.01155  -0.0994   0.0571   1.0000
   9.000   1.4181   0.01909   0.01221  -0.0983   0.0562   1.0000
   9.250   1.4345   0.01983   0.01295  -0.0971   0.0553   1.0000
   9.500   1.4502   0.02062   0.01376  -0.0960   0.0544   1.0000
   9.750   1.4661   0.02145   0.01461  -0.0950   0.0539   1.0000
  10.000   1.4822   0.02227   0.01546  -0.0941   0.0535   1.0000
  10.250   1.4979   0.02315   0.01636  -0.0932   0.0532   1.0000
  10.500   1.5128   0.02411   0.01735  -0.0923   0.0528   1.0000
  10.750   1.5270   0.02513   0.01841  -0.0914   0.0525   1.0000
  11.000   1.5406   0.02622   0.01952  -0.0904   0.0521   1.0000
  11.250   1.5532   0.02741   0.02075  -0.0895   0.0517   1.0000
  11.500   1.5651   0.02867   0.02204  -0.0885   0.0513   1.0000
  11.750   1.5761   0.03001   0.02342  -0.0876   0.0509   1.0000
  12.000   1.5861   0.03149   0.02493  -0.0867   0.0505   1.0000
  12.250   1.5954   0.03305   0.02653  -0.0858   0.0502   1.0000
  12.500   1.6037   0.03470   0.02822  -0.0849   0.0499   1.0000
  12.750   1.6110   0.03650   0.03007  -0.0840   0.0496   1.0000
  13.000   1.6173   0.03844   0.03206  -0.0832   0.0493   1.0000
  13.250   1.6225   0.04052   0.03418  -0.0825   0.0490   1.0000
  13.500   1.6269   0.04272   0.03644  -0.0818   0.0487   1.0000
  13.750   1.6305   0.04510   0.03888  -0.0812   0.0484   1.0000
  14.000   1.6333   0.04761   0.04145  -0.0807   0.0481   1.0000
  14.250   1.6343   0.05034   0.04425  -0.0802   0.0478   1.0000
  14.500   1.6378   0.05285   0.04682  -0.0798   0.0478   1.0000
  14.750   1.6414   0.05534   0.04938  -0.0794   0.0477   1.0000
  15.000   1.6439   0.05801   0.05211  -0.0791   0.0475   1.0000
  15.250   1.6468   0.06062   0.05478  -0.0788   0.0474   1.0000
  15.500   1.6496   0.06326   0.05748  -0.0786   0.0471   1.0000
  15.750   1.6510   0.06611   0.06040  -0.0784   0.0469   1.0000
  16.000   1.6535   0.06883   0.06318  -0.0783   0.0466   1.0000
  16.250   1.6535   0.07189   0.06631  -0.0782   0.0463   1.0000
  16.500   1.6545   0.07481   0.06929  -0.0782   0.0460   1.0000
  16.750   1.6538   0.07802   0.07256  -0.0782   0.0457   1.0000
  17.000   1.6537   0.08115   0.07576  -0.0783   0.0455   1.0000
  17.250   1.6519   0.08455   0.07922  -0.0785   0.0452   1.0000
  17.500   1.6499   0.08796   0.08270  -0.0787   0.0450   1.0000
  17.750   1.6480   0.09138   0.08619  -0.0789   0.0448   1.0000
  18.000   1.6450   0.09500   0.08988  -0.0793   0.0446   1.0000
  18.250   1.6435   0.09843   0.09337  -0.0797   0.0443   1.0000
  18.500   1.6398   0.10219   0.09719  -0.0803   0.0441   1.0000
  18.750   1.6377   0.10569   0.10075  -0.0808   0.0439   1.0000
  19.000   1.6333   0.10960   0.10472  -0.0815   0.0436   1.0000
  19.250   1.6310   0.11317   0.10836  -0.0822   0.0434   1.0000
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