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GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 626 AIRFOIL (goe626-il)
Reynolds number: 500,000
Max Cl/Cd: 90.44 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe626-il-500000.txt
Download as CSV file: xf-goe626-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 626 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.7240   0.09955   0.09598  -0.0709   1.0000   0.0333
 -17.000  -0.7360   0.09437   0.09072  -0.0736   1.0000   0.0335
 -16.750  -0.7510   0.08885   0.08508  -0.0766   1.0000   0.0335
 -16.500  -0.7618   0.08421   0.08035  -0.0789   1.0000   0.0336
 -16.250  -0.7669   0.08059   0.07667  -0.0804   1.0000   0.0339
 -16.000  -0.7715   0.07717   0.07319  -0.0818   1.0000   0.0340
 -15.750  -0.7759   0.07390   0.06986  -0.0830   1.0000   0.0342
 -15.500  -0.7799   0.07084   0.06673  -0.0839   1.0000   0.0343
 -15.250  -0.7835   0.06797   0.06381  -0.0846   1.0000   0.0344
 -15.000  -0.7866   0.06533   0.06112  -0.0851   1.0000   0.0346
 -14.750  -0.7896   0.06290   0.05865  -0.0852   1.0000   0.0348
 -14.500  -0.7936   0.06060   0.05631  -0.0851   1.0000   0.0349
 -14.250  -0.7993   0.05842   0.05409  -0.0846   1.0000   0.0350
 -14.000  -0.8060   0.05642   0.05205  -0.0837   1.0000   0.0352
 -13.750  -0.8149   0.05455   0.05016  -0.0824   1.0000   0.0353
 -13.500  -0.8272   0.05273   0.04833  -0.0806   1.0000   0.0354
 -13.250  -0.8236   0.05030   0.04584  -0.0825   0.9987   0.0356
 -13.000  -0.8061   0.04781   0.04328  -0.0864   0.9959   0.0359
 -12.750  -0.7887   0.04499   0.04038  -0.0913   0.9929   0.0362
 -12.500  -0.7742   0.04255   0.03787  -0.0948   0.9885   0.0364
 -12.250  -0.7560   0.04018   0.03543  -0.0988   0.9840   0.0366
 -12.000  -0.7327   0.03859   0.03384  -0.1020   0.9810   0.0369
 -11.750  -0.7174   0.03671   0.03196  -0.1042   0.9741   0.0373
 -11.500  -0.6931   0.03428   0.02952  -0.1092   0.9700   0.0378
 -11.250  -0.6639   0.03154   0.02675  -0.1156   0.9677   0.0381
 -11.000  -0.6453   0.02870   0.02384  -0.1200   0.9607   0.0385
 -10.750  -0.6152   0.02582   0.02087  -0.1259   0.9570   0.0390
 -10.500  -0.5806   0.02325   0.01819  -0.1315   0.9550   0.0397
 -10.250  -0.5451   0.02159   0.01644  -0.1356   0.9535   0.0403
 -10.000  -0.5079   0.02024   0.01499  -0.1394   0.9524   0.0410
  -9.750  -0.4867   0.01930   0.01397  -0.1394   0.9457   0.0414
  -9.500  -0.4554   0.01795   0.01256  -0.1418   0.9424   0.0422
  -9.250  -0.4221   0.01684   0.01138  -0.1441   0.9400   0.0432
  -9.000  -0.3871   0.01593   0.01041  -0.1463   0.9379   0.0443
  -8.750  -0.3571   0.01523   0.00964  -0.1472   0.9340   0.0454
  -8.500  -0.3313   0.01466   0.00900  -0.1471   0.9279   0.0466
  -8.250  -0.2991   0.01391   0.00820  -0.1484   0.9236   0.0491
  -8.000  -0.2643   0.01318   0.00746  -0.1501   0.9197   0.0546
  -7.750  -0.2417   0.01253   0.00689  -0.1493   0.9114   0.0712
  -7.500  -0.2118   0.01189   0.00627  -0.1499   0.9055   0.0900
  -7.250  -0.1820   0.01126   0.00569  -0.1506   0.9000   0.1093
  -7.000  -0.1572   0.01070   0.00521  -0.1501   0.8921   0.1338
  -6.750  -0.1271   0.01021   0.00478  -0.1507   0.8859   0.1620
  -6.500  -0.1001   0.00994   0.00458  -0.1504   0.8782   0.1834
  -6.250  -0.0714   0.00981   0.00446  -0.1503   0.8703   0.2002
  -6.000  -0.0416   0.00977   0.00440  -0.1503   0.8626   0.2128
  -5.750  -0.0139   0.00974   0.00431  -0.1499   0.8532   0.2213
  -5.500   0.0158   0.00978   0.00432  -0.1498   0.8444   0.2285
  -5.250   0.0436   0.00981   0.00426  -0.1494   0.8334   0.2344
  -5.000   0.0717   0.00981   0.00422  -0.1491   0.8225   0.2390
  -4.750   0.1002   0.00991   0.00426  -0.1488   0.8103   0.2437
  -4.500   0.1273   0.00997   0.00426  -0.1482   0.7959   0.2479
  -4.250   0.1546   0.01006   0.00422  -0.1476   0.7800   0.2513
  -4.000   0.1812   0.01004   0.00415  -0.1470   0.7617   0.2550
  -3.750   0.2074   0.01016   0.00419  -0.1463   0.7402   0.2583
  -3.250   0.2585   0.01054   0.00431  -0.1446   0.6924   0.2659
  -3.000   0.2842   0.01074   0.00434  -0.1438   0.6731   0.2684
  -2.750   0.3096   0.01072   0.00423  -0.1431   0.6574   0.2718
  -2.500   0.3356   0.01089   0.00436  -0.1424   0.6436   0.2751
  -2.250   0.3623   0.01105   0.00447  -0.1419   0.6318   0.2784
  -2.000   0.3887   0.01117   0.00450  -0.1413   0.6211   0.2810
  -1.750   0.4159   0.01124   0.00450  -0.1409   0.6116   0.2835
  -1.250   0.4696   0.01130   0.00443  -0.1400   0.5938   0.2883
  -1.000   0.4958   0.01127   0.00435  -0.1395   0.5846   0.2903
  -0.750   0.5226   0.01125   0.00433  -0.1391   0.5753   0.2922
  -0.500   0.5485   0.01131   0.00433  -0.1385   0.5651   0.2942
  -0.250   0.5753   0.01131   0.00433  -0.1380   0.5559   0.2961
   0.000   0.6015   0.01135   0.00430  -0.1374   0.5467   0.2979
   0.250   0.6280   0.01136   0.00429  -0.1369   0.5376   0.2996
   0.500   0.6537   0.01142   0.00428  -0.1363   0.5271   0.3015
   0.750   0.6798   0.01146   0.00429  -0.1357   0.5165   0.3033
   1.250   0.7311   0.01150   0.00423  -0.1344   0.4964   0.3063
   1.500   0.7559   0.01151   0.00419  -0.1337   0.4872   0.3084
   1.750   0.7821   0.01152   0.00422  -0.1332   0.4785   0.3102
   2.000   0.8068   0.01162   0.00427  -0.1324   0.4699   0.3122
   2.250   0.8328   0.01168   0.00435  -0.1318   0.4620   0.3144
   2.500   0.8577   0.01179   0.00442  -0.1311   0.4541   0.3166
   2.750   0.8829   0.01189   0.00450  -0.1304   0.4465   0.3186
   3.000   0.9079   0.01199   0.00458  -0.1297   0.4384   0.3205
   3.250   0.9321   0.01215   0.00468  -0.1288   0.4308   0.3221
   3.500   0.9574   0.01225   0.00477  -0.1281   0.4231   0.3235
   3.750   0.9808   0.01233   0.00483  -0.1272   0.4153   0.3263
   4.000   1.0057   0.01239   0.00493  -0.1264   0.4088   0.3289
   4.250   1.0297   0.01250   0.00505  -0.1256   0.4016   0.3314
   4.500   1.0526   0.01268   0.00520  -0.1245   0.3946   0.3342
   4.750   1.0771   0.01277   0.00532  -0.1237   0.3876   0.3373
   5.000   1.1000   0.01293   0.00546  -0.1227   0.3810   0.3399
   5.250   1.1226   0.01310   0.00562  -0.1215   0.3752   0.3421
   5.500   1.1453   0.01316   0.00573  -0.1204   0.3685   0.3456
   5.750   1.1659   0.01331   0.00589  -0.1190   0.3621   0.3493
   6.000   1.1875   0.01345   0.00607  -0.1177   0.3564   0.3529
   6.250   1.2094   0.01359   0.00623  -0.1164   0.3499   0.3568
   6.500   1.2287   0.01383   0.00644  -0.1148   0.3428   0.3605
   6.750   1.2506   0.01397   0.00664  -0.1136   0.3364   0.3655
   7.000   1.2711   0.01416   0.00688  -0.1122   0.3291   0.3711
   7.250   1.2906   0.01441   0.00713  -0.1106   0.3222   0.3778
   7.500   1.3113   0.01460   0.00739  -0.1093   0.3143   0.3860
   7.750   1.3291   0.01490   0.00769  -0.1075   0.3060   0.3965
   8.000   1.3490   0.01512   0.00799  -0.1061   0.2965   0.4115
   8.250   1.3661   0.01543   0.00835  -0.1043   0.2862   0.4364
   8.500   1.3817   0.01577   0.00878  -0.1023   0.2734   0.4905
   8.750   1.4009   0.01549   0.00935  -0.1012   0.2569   1.0000
   9.000   1.4144   0.01609   0.00985  -0.0990   0.2386   1.0000
   9.250   1.4253   0.01683   0.01047  -0.0965   0.2180   1.0000
   9.500   1.4352   0.01764   0.01117  -0.0939   0.2009   1.0000
   9.750   1.4455   0.01845   0.01190  -0.0915   0.1890   1.0000
  10.250   1.4678   0.02005   0.01343  -0.0871   0.1730   1.0000
  10.500   1.4780   0.02093   0.01429  -0.0850   0.1673   1.0000
  10.750   1.4901   0.02174   0.01511  -0.0831   0.1626   1.0000
  11.000   1.5025   0.02255   0.01594  -0.0813   0.1578   1.0000
  11.250   1.5112   0.02360   0.01698  -0.0792   0.1527   1.0000
  11.500   1.5226   0.02453   0.01794  -0.0775   0.1475   1.0000
  11.750   1.5330   0.02554   0.01897  -0.0758   0.1413   1.0000
  12.000   1.5405   0.02679   0.02021  -0.0739   0.1349   1.0000
  12.250   1.5496   0.02798   0.02140  -0.0723   0.1257   1.0000
  12.500   1.5541   0.02953   0.02291  -0.0705   0.1123   1.0000
  12.750   1.5502   0.03179   0.02504  -0.0683   0.0921   1.0000
  13.000   1.5460   0.03424   0.02743  -0.0664   0.0825   1.0000
  13.250   1.5443   0.03661   0.02981  -0.0648   0.0776   1.0000
  13.500   1.5432   0.03907   0.03229  -0.0636   0.0748   1.0000
  13.750   1.5418   0.04169   0.03496  -0.0626   0.0726   1.0000
  14.000   1.5436   0.04412   0.03747  -0.0618   0.0712   1.0000
  14.250   1.5441   0.04677   0.04019  -0.0613   0.0699   1.0000
  14.500   1.5437   0.04963   0.04312  -0.0609   0.0690   1.0000
  14.750   1.5412   0.05279   0.04636  -0.0606   0.0680   1.0000
  15.000   1.5380   0.05611   0.04975  -0.0605   0.0671   1.0000
  15.250   1.5330   0.05973   0.05344  -0.0605   0.0663   1.0000
  15.500   1.5283   0.06340   0.05718  -0.0607   0.0656   1.0000
  15.750   1.5210   0.06748   0.06133  -0.0610   0.0648   1.0000
  16.000   1.5196   0.07087   0.06481  -0.0614   0.0645   1.0000
  16.250   1.5186   0.07427   0.06830  -0.0618   0.0640   1.0000
  16.500   1.5173   0.07778   0.07190  -0.0623   0.0635   1.0000
  16.750   1.5162   0.08129   0.07550  -0.0630   0.0628   1.0000
  17.000   1.5149   0.08488   0.07917  -0.0637   0.0624   1.0000
  17.250   1.5132   0.08859   0.08295  -0.0645   0.0620   1.0000
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