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GOE 575 AIRFOIL (goe575-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 575 AIRFOIL (goe575-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.33 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe575-il-1000000.txt
Download as CSV file: xf-goe575-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 575 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.0221   0.07818   0.07575  -0.0625   0.9996   0.0248
 -16.500  -1.1945   0.04443   0.04139  -0.0880   0.9993   0.0243
 -16.250  -1.2166   0.04040   0.03718  -0.0879   0.9988   0.0244
 -16.000  -1.2271   0.03798   0.03463  -0.0860   0.9979   0.0246
 -15.750  -1.2351   0.03596   0.03245  -0.0835   0.9968   0.0248
 -15.500  -1.2240   0.03522   0.03162  -0.0821   0.9960   0.0251
 -15.250  -1.2193   0.03415   0.03042  -0.0800   0.9953   0.0253
 -15.000  -1.2169   0.03311   0.02924  -0.0776   0.9946   0.0255
 -14.750  -1.2288   0.03185   0.02789  -0.0718   0.9941   0.0259
 -14.500  -1.2324   0.03101   0.02703  -0.0665   0.9933   0.0262
 -14.250  -1.2273   0.03009   0.02603  -0.0631   0.9904   0.0264
 -14.000  -1.2036   0.03026   0.02623  -0.0625   0.9891   0.0268
 -13.750  -1.1882   0.02977   0.02568  -0.0609   0.9876   0.0271
 -13.500  -1.1631   0.02994   0.02583  -0.0606   0.9868   0.0276
 -13.250  -1.1496   0.02934   0.02509  -0.0588   0.9859   0.0278
 -13.000  -1.1462   0.02881   0.02453  -0.0539   0.9809   0.0283
 -12.750  -1.1290   0.02837   0.02400  -0.0523   0.9788   0.0286
 -12.500  -1.1092   0.02802   0.02356  -0.0510   0.9775   0.0290
 -12.250  -1.0968   0.02744   0.02287  -0.0482   0.9731   0.0292
 -12.000  -1.0875   0.02657   0.02187  -0.0449   0.9704   0.0296
 -11.750  -1.0712   0.02569   0.02091  -0.0430   0.9688   0.0299
 -11.500  -1.0449   0.02573   0.02098  -0.0429   0.9679   0.0306
 -11.250  -1.0200   0.02541   0.02063  -0.0425   0.9672   0.0309
 -11.000  -1.0126   0.02488   0.02004  -0.0383   0.9625   0.0312
 -10.750  -0.9888   0.02484   0.01999  -0.0374   0.9602   0.0317
 -10.500  -0.9638   0.02443   0.01951  -0.0369   0.9587   0.0323
 -10.250  -0.9383   0.02378   0.01877  -0.0366   0.9576   0.0325
 -10.000  -0.9096   0.02381   0.01874  -0.0368   0.9569   0.0333
  -9.750  -0.9006   0.02315   0.01800  -0.0328   0.9526   0.0335
  -9.500  -0.8805   0.02292   0.01769  -0.0311   0.9499   0.0338
  -9.250  -0.8591   0.02171   0.01638  -0.0300   0.9485   0.0346
  -9.000  -0.8324   0.02114   0.01578  -0.0299   0.9474   0.0350
  -8.750  -0.8031   0.02082   0.01545  -0.0302   0.9466   0.0355
  -8.500  -0.7725   0.02055   0.01516  -0.0307   0.9460   0.0360
  -8.250  -0.7615   0.02027   0.01485  -0.0270   0.9411   0.0365
  -8.000  -0.7370   0.01984   0.01437  -0.0261   0.9386   0.0370
  -7.750  -0.7091   0.01946   0.01394  -0.0260   0.9372   0.0376
  -7.500  -0.6784   0.01908   0.01351  -0.0265   0.9361   0.0382
  -7.250  -0.6481   0.01863   0.01300  -0.0269   0.9353   0.0386
  -7.000  -0.6159   0.01822   0.01255  -0.0277   0.9346   0.0388
  -6.750  -0.5833   0.01726   0.01154  -0.0288   0.9341   0.0397
  -6.500  -0.5747   0.01685   0.01111  -0.0245   0.9281   0.0400
  -6.250  -0.5475   0.01648   0.01076  -0.0242   0.9262   0.0409
  -6.000  -0.5153   0.01604   0.01031  -0.0250   0.9247   0.0414
  -5.750  -0.4826   0.01560   0.00986  -0.0258   0.9237   0.0422
  -5.500  -0.4472   0.01515   0.00939  -0.0273   0.9228   0.0430
  -5.250  -0.4094   0.01463   0.00886  -0.0292   0.9219   0.0436
  -5.000  -0.3910   0.01427   0.00848  -0.0268   0.9160   0.0439
  -4.750  -0.3609   0.01395   0.00814  -0.0270   0.9129   0.0445
  -4.500  -0.3261   0.01319   0.00737  -0.0284   0.9113   0.0456
  -4.250  -0.2909   0.01262   0.00681  -0.0298   0.9097   0.0464
  -4.000  -0.2566   0.01216   0.00636  -0.0310   0.9086   0.0472
  -3.750  -0.2318   0.01184   0.00604  -0.0301   0.9038   0.0482
  -3.500  -0.2049   0.01152   0.00572  -0.0297   0.8986   0.0488
  -3.250  -0.1691   0.01111   0.00530  -0.0312   0.8950   0.0497
  -3.000  -0.1284   0.01072   0.00491  -0.0338   0.8927   0.0508
  -2.750  -0.1060   0.01051   0.00469  -0.0324   0.8814   0.0511
  -2.500  -0.0563   0.00993   0.00410  -0.0371   0.8770   0.0528
  -2.250  -0.0162   0.00953   0.00369  -0.0396   0.8619   0.0548
  -2.000   0.0328   0.00917   0.00327  -0.0442   0.8395   0.0564
  -1.750   0.0859   0.00893   0.00284  -0.0497   0.7917   0.0585
  -1.500   0.1049   0.00905   0.00272  -0.0475   0.7384   0.0615
  -1.250   0.1236   0.00910   0.00266  -0.0453   0.7103   0.0653
  -1.000   0.1448   0.00905   0.00263  -0.0438   0.6888   0.0887
  -0.750   0.1668   0.00901   0.00263  -0.0424   0.6706   0.1179
  -0.500   0.1869   0.00905   0.00265  -0.0406   0.6499   0.1346
   0.000   0.2284   0.00915   0.00268  -0.0373   0.6106   0.1570
   0.250   0.2489   0.00921   0.00271  -0.0356   0.5870   0.1700
   0.500   0.2709   0.00926   0.00273  -0.0342   0.5695   0.1808
   0.750   0.2923   0.00933   0.00276  -0.0328   0.5483   0.1954
   1.000   0.3144   0.00939   0.00279  -0.0314   0.5290   0.2089
   1.250   0.3371   0.00945   0.00282  -0.0303   0.5104   0.2246
   1.500   0.3616   0.00944   0.00287  -0.0296   0.4911   0.2642
   1.750   0.3935   0.00920   0.00297  -0.0309   0.4712   0.4061
   2.000   0.5558   0.01012   0.00532  -0.0616   0.4286   0.9636
   2.250   0.6086   0.01087   0.00596  -0.0670   0.4088   0.9734
   2.500   0.6906   0.01127   0.00621  -0.0791   0.3871   0.9809
   2.750   0.7626   0.01129   0.00612  -0.0890   0.3700   0.9883
   3.000   0.8147   0.01135   0.00607  -0.0944   0.3535   0.9948
   3.250   0.8734   0.01092   0.00554  -0.1015   0.3393   0.9999
   3.500   0.8962   0.01100   0.00558  -0.1004   0.3309   1.0000
   3.750   0.9174   0.01113   0.00566  -0.0990   0.3216   1.0000
   4.000   0.9386   0.01125   0.00574  -0.0977   0.3127   1.0000
   4.250   0.9597   0.01137   0.00583  -0.0963   0.3059   1.0000
   4.500   0.9811   0.01148   0.00592  -0.0949   0.2986   1.0000
   4.750   1.0015   0.01164   0.00603  -0.0934   0.2903   1.0000
   5.000   1.0224   0.01175   0.00613  -0.0920   0.2819   1.0000
   5.250   1.0423   0.01193   0.00625  -0.0903   0.2722   1.0000
   5.500   1.0629   0.01206   0.00637  -0.0888   0.2649   1.0000
   5.750   1.0824   0.01226   0.00651  -0.0872   0.2523   1.0000
   6.000   1.1015   0.01249   0.00667  -0.0854   0.2393   1.0000
   6.250   1.1209   0.01269   0.00683  -0.0838   0.2276   1.0000
   6.500   1.1398   0.01292   0.00701  -0.0820   0.2148   1.0000
   6.750   1.1581   0.01319   0.00722  -0.0801   0.2021   1.0000
   7.000   1.1758   0.01349   0.00744  -0.0782   0.1896   1.0000
   7.250   1.1935   0.01378   0.00768  -0.0762   0.1802   1.0000
   7.500   1.2121   0.01400   0.00790  -0.0744   0.1747   1.0000
   7.750   1.2303   0.01424   0.00812  -0.0726   0.1693   1.0000
   8.000   1.2472   0.01455   0.00840  -0.0705   0.1624   1.0000
   8.250   1.2655   0.01476   0.00863  -0.0687   0.1589   1.0000
   8.500   1.2828   0.01501   0.00888  -0.0667   0.1545   1.0000
   8.750   1.2992   0.01532   0.00918  -0.0645   0.1494   1.0000
   9.000   1.3166   0.01558   0.00945  -0.0626   0.1454   1.0000
   9.250   1.3337   0.01585   0.00972  -0.0606   0.1395   1.0000
   9.500   1.3493   0.01621   0.01006  -0.0585   0.1332   1.0000
   9.750   1.3660   0.01651   0.01036  -0.0564   0.1257   1.0000
  10.000   1.3791   0.01697   0.01075  -0.0539   0.1138   1.0000
  10.250   1.3891   0.01758   0.01126  -0.0508   0.0979   1.0000
  10.500   1.3961   0.01836   0.01192  -0.0472   0.0810   1.0000
  10.750   1.4065   0.01895   0.01248  -0.0443   0.0748   1.0000
  11.000   1.4164   0.01956   0.01308  -0.0412   0.0700   1.0000
  11.250   1.4277   0.02010   0.01363  -0.0386   0.0679   1.0000
  11.500   1.4382   0.02069   0.01424  -0.0357   0.0651   1.0000
  11.750   1.4508   0.02116   0.01476  -0.0333   0.0638   1.0000
  12.000   1.4622   0.02171   0.01536  -0.0308   0.0628   1.0000
  12.250   1.4719   0.02235   0.01602  -0.0281   0.0617   1.0000
  12.500   1.4820   0.02299   0.01670  -0.0254   0.0604   1.0000
  12.750   1.4895   0.02378   0.01752  -0.0225   0.0591   1.0000
  13.000   1.4958   0.02466   0.01845  -0.0195   0.0579   1.0000
  13.250   1.5028   0.02552   0.01938  -0.0167   0.0572   1.0000
  13.500   1.5146   0.02614   0.02005  -0.0147   0.0566   1.0000
  13.750   1.5231   0.02696   0.02093  -0.0123   0.0563   1.0000
  14.000   1.5304   0.02788   0.02192  -0.0099   0.0558   1.0000
  14.250   1.5395   0.02874   0.02283  -0.0078   0.0545   1.0000
  14.500   1.5461   0.02978   0.02392  -0.0055   0.0538   1.0000
  14.750   1.5511   0.03098   0.02517  -0.0032   0.0532   1.0000
  15.000   1.5553   0.03228   0.02653  -0.0009   0.0528   1.0000
  15.250   1.5580   0.03375   0.02804   0.0012   0.0511   1.0000
  15.500   1.5569   0.03561   0.02998   0.0035   0.0507   1.0000
  15.750   1.5559   0.03756   0.03200   0.0055   0.0498   1.0000
  16.000   1.5582   0.03935   0.03388   0.0070   0.0497   1.0000
  16.250   1.5656   0.04074   0.03534   0.0081   0.0491   1.0000
  16.500   1.5727   0.04220   0.03687   0.0091   0.0483   1.0000
  16.750   1.5755   0.04411   0.03886   0.0101   0.0479   1.0000
  17.000   1.5763   0.04628   0.04110   0.0110   0.0471   1.0000
  17.250   1.5753   0.04870   0.04360   0.0118   0.0465   1.0000
  17.500   1.5758   0.05104   0.04597   0.0124   0.0453   1.0000
  17.750   1.5743   0.05364   0.04866   0.0129   0.0447   1.0000
  18.000   1.5640   0.05734   0.05243   0.0132   0.0437   1.0000
  18.250   1.5595   0.06043   0.05561   0.0133   0.0430   1.0000
  18.500   1.5613   0.06283   0.05810   0.0134   0.0424   1.0000
  18.750   1.5587   0.06579   0.06115   0.0133   0.0416   1.0000
  19.000   1.5537   0.06912   0.06457   0.0131   0.0409   1.0000
  19.250   1.5473   0.07269   0.06820   0.0126   0.0397   1.0000
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