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GOE 424 AIRFOIL (goe424-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 424 AIRFOIL (goe424-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.15 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe424-il-1000000.txt
Download as CSV file: xf-goe424-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 424 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8208   0.09476   0.09208  -0.0771   1.0000   0.0185
 -19.250  -0.8582   0.08499   0.08214  -0.0828   1.0000   0.0186
 -19.000  -0.8826   0.07764   0.07466  -0.0871   1.0000   0.0187
 -18.750  -0.8985   0.07181   0.06873  -0.0905   1.0000   0.0189
 -18.500  -0.9093   0.06684   0.06367  -0.0934   1.0000   0.0190
 -18.250  -0.9166   0.06251   0.05927  -0.0958   1.0000   0.0192
 -18.000  -0.9204   0.05878   0.05547  -0.0979   1.0000   0.0193
 -17.750  -0.9227   0.05535   0.05199  -0.0996   1.0000   0.0195
 -17.500  -0.9242   0.05221   0.04878  -0.1011   1.0000   0.0197
 -17.250  -0.9258   0.04933   0.04584  -0.1022   1.0000   0.0199
 -17.000  -0.9289   0.04663   0.04307  -0.1028   1.0000   0.0200
 -16.750  -0.9345   0.04418   0.04056  -0.1026   1.0000   0.0202
 -16.500  -0.9427   0.04199   0.03830  -0.1015   1.0000   0.0204
 -16.250  -0.9464   0.03984   0.03607  -0.1010   0.9996   0.0206
 -16.000  -0.9320   0.03746   0.03359  -0.1036   0.9980   0.0209
 -15.750  -0.9159   0.03528   0.03130  -0.1061   0.9961   0.0212
 -15.500  -0.8965   0.03338   0.02929  -0.1087   0.9944   0.0215
 -15.250  -0.8816   0.03106   0.02685  -0.1111   0.9927   0.0218
 -15.000  -0.8663   0.02924   0.02499  -0.1127   0.9892   0.0222
 -14.750  -0.8457   0.02803   0.02376  -0.1142   0.9857   0.0225
 -14.500  -0.8231   0.02701   0.02270  -0.1156   0.9823   0.0228
 -14.250  -0.8060   0.02612   0.02178  -0.1158   0.9763   0.0231
 -14.000  -0.7892   0.02531   0.02092  -0.1157   0.9699   0.0235
 -13.750  -0.7757   0.02456   0.02012  -0.1147   0.9621   0.0238
 -13.500  -0.7631   0.02383   0.01930  -0.1134   0.9541   0.0242
 -13.250  -0.7502   0.02313   0.01852  -0.1121   0.9451   0.0246
 -13.000  -0.7366   0.02250   0.01780  -0.1106   0.9362   0.0249
 -12.750  -0.7217   0.02195   0.01715  -0.1092   0.9254   0.0252
 -12.500  -0.7114   0.02076   0.01586  -0.1074   0.9140   0.0257
 -12.250  -0.6955   0.02022   0.01528  -0.1060   0.9006   0.0261
 -12.000  -0.6783   0.01985   0.01484  -0.1047   0.8835   0.0264
 -11.750  -0.6607   0.01955   0.01445  -0.1032   0.8626   0.0267
 -11.500  -0.6440   0.01932   0.01409  -0.1016   0.8397   0.0271
 -11.250  -0.6251   0.01910   0.01373  -0.1003   0.8172   0.0276
 -11.000  -0.6051   0.01883   0.01333  -0.0992   0.7942   0.0281
 -10.750  -0.5848   0.01857   0.01291  -0.0982   0.7697   0.0286
 -10.500  -0.5640   0.01834   0.01251  -0.0971   0.7408   0.0290
 -10.250  -0.5447   0.01788   0.01185  -0.0960   0.7060   0.0294
 -10.000  -0.5261   0.01735   0.01117  -0.0948   0.6723   0.0300
  -9.750  -0.5045   0.01719   0.01090  -0.0939   0.6473   0.0304
  -9.500  -0.4817   0.01708   0.01070  -0.0932   0.6302   0.0309
  -9.250  -0.4583   0.01694   0.01048  -0.0926   0.6176   0.0314
  -9.000  -0.4351   0.01674   0.01019  -0.0919   0.6071   0.0320
  -8.750  -0.4114   0.01645   0.00983  -0.0914   0.5987   0.0326
  -8.500  -0.3879   0.01621   0.00949  -0.0907   0.5905   0.0331
  -8.250  -0.3630   0.01600   0.00923  -0.0903   0.5847   0.0336
  -8.000  -0.3416   0.01534   0.00852  -0.0894   0.5787   0.0343
  -7.750  -0.3181   0.01507   0.00822  -0.0888   0.5726   0.0349
  -7.500  -0.2931   0.01483   0.00797  -0.0884   0.5684   0.0355
  -7.250  -0.2682   0.01461   0.00771  -0.0880   0.5636   0.0361
  -7.000  -0.2437   0.01439   0.00744  -0.0875   0.5588   0.0367
  -6.750  -0.2190   0.01420   0.00720  -0.0870   0.5542   0.0374
  -6.500  -0.1932   0.01400   0.00698  -0.0867   0.5512   0.0381
  -6.250  -0.1672   0.01385   0.00678  -0.0864   0.5478   0.0386
  -6.000  -0.1455   0.01331   0.00622  -0.0855   0.5445   0.0393
  -5.750  -0.1221   0.01300   0.00589  -0.0848   0.5411   0.0400
  -5.500  -0.0977   0.01283   0.00569  -0.0842   0.5371   0.0407
  -5.250  -0.0716   0.01264   0.00550  -0.0840   0.5350   0.0416
  -5.000  -0.0456   0.01247   0.00532  -0.0837   0.5326   0.0425
  -4.750  -0.0198   0.01228   0.00511  -0.0834   0.5299   0.0432
  -4.500   0.0061   0.01214   0.00494  -0.0831   0.5270   0.0439
  -4.250   0.0323   0.01205   0.00482  -0.0828   0.5242   0.0444
  -4.000   0.0545   0.01167   0.00439  -0.0819   0.5213   0.0456
  -3.750   0.0801   0.01152   0.00423  -0.0815   0.5187   0.0468
  -3.500   0.1067   0.01137   0.00409  -0.0814   0.5171   0.0480
  -3.250   0.1334   0.01124   0.00395  -0.0812   0.5153   0.0491
  -3.000   0.1602   0.01113   0.00382  -0.0810   0.5132   0.0501
  -2.750   0.1872   0.01105   0.00373  -0.0809   0.5109   0.0508
  -2.500   0.2125   0.01083   0.00348  -0.0805   0.5087   0.0528
  -2.250   0.2387   0.01074   0.00337  -0.0803   0.5064   0.0546
  -2.000   0.2652   0.01070   0.00330  -0.0801   0.5038   0.0565
  -1.750   0.2922   0.01068   0.00326  -0.0800   0.5015   0.0579
  -1.500   0.3192   0.01055   0.00315  -0.0799   0.5003   0.0612
  -1.250   0.3464   0.01046   0.00306  -0.0799   0.4986   0.0648
  -1.000   0.3729   0.01031   0.00299  -0.0798   0.4968   0.0840
  -0.750   0.3897   0.00926   0.00277  -0.0783   0.4951   0.3402
  -0.500   0.4141   0.00896   0.00276  -0.0779   0.4934   0.4299
  -0.250   0.4396   0.00879   0.00277  -0.0776   0.4915   0.4864
   0.000   0.4653   0.00867   0.00280  -0.0773   0.4895   0.5388
   0.250   0.4915   0.00864   0.00285  -0.0772   0.4871   0.5782
   0.500   0.5184   0.00866   0.00294  -0.0771   0.4846   0.6092
   0.750   0.5458   0.00861   0.00297  -0.0772   0.4834   0.6343
   1.000   0.5729   0.00857   0.00301  -0.0771   0.4820   0.6591
   1.250   0.5999   0.00853   0.00306  -0.0771   0.4803   0.6875
   1.500   0.6267   0.00849   0.00311  -0.0770   0.4785   0.7154
   1.750   0.6537   0.00848   0.00317  -0.0770   0.4766   0.7392
   2.000   0.6804   0.00847   0.00323  -0.0769   0.4746   0.7648
   2.250   0.7066   0.00848   0.00331  -0.0766   0.4726   0.7916
   2.500   0.7327   0.00854   0.00341  -0.0764   0.4699   0.8181
   2.750   0.7584   0.00858   0.00354  -0.0761   0.4672   0.8487
   3.000   0.7840   0.00855   0.00360  -0.0757   0.4650   0.8744
   3.250   0.8097   0.00855   0.00366  -0.0753   0.4621   0.8942
   3.500   0.8353   0.00858   0.00373  -0.0749   0.4593   0.9113
   3.750   0.8606   0.00865   0.00382  -0.0745   0.4568   0.9268
   4.000   0.8861   0.00875   0.00393  -0.0741   0.4544   0.9421
   4.250   0.9130   0.00892   0.00408  -0.0741   0.4516   0.9565
   4.500   0.9424   0.00902   0.00420  -0.0746   0.4500   0.9684
   4.750   0.9752   0.00911   0.00432  -0.0759   0.4481   0.9765
   5.000   1.0088   0.00921   0.00443  -0.0775   0.4457   0.9826
   5.250   1.0448   0.00932   0.00455  -0.0796   0.4429   0.9865
   5.500   1.0804   0.00947   0.00467  -0.0816   0.4401   0.9903
   5.750   1.1162   0.00965   0.00483  -0.0837   0.4370   0.9935
   6.000   1.1551   0.00983   0.00500  -0.0866   0.4340   0.9958
   6.250   1.1946   0.00993   0.00513  -0.0895   0.4310   0.9983
   6.500   1.2268   0.01002   0.00525  -0.0908   0.4275   1.0000
   6.750   1.2304   0.01003   0.00526  -0.0861   0.4245   1.0000
   7.000   1.2388   0.01011   0.00532  -0.0825   0.4214   1.0000
   7.250   1.2535   0.01024   0.00544  -0.0802   0.4179   1.0000
   7.500   1.2744   0.01030   0.00555  -0.0791   0.4143   1.0000
   7.750   1.2949   0.01043   0.00568  -0.0781   0.4097   1.0000
   8.000   1.3142   0.01062   0.00586  -0.0768   0.4051   1.0000
   8.250   1.3359   0.01080   0.00604  -0.0761   0.4010   1.0000
   8.500   1.3588   0.01095   0.00622  -0.0756   0.3963   1.0000
   8.750   1.3792   0.01118   0.00645  -0.0747   0.3907   1.0000
   9.000   1.3999   0.01143   0.00670  -0.0739   0.3848   1.0000
   9.250   1.4208   0.01169   0.00696  -0.0732   0.3773   1.0000
   9.500   1.4391   0.01204   0.00729  -0.0720   0.3694   1.0000
   9.750   1.4566   0.01245   0.00767  -0.0708   0.3587   1.0000
  10.000   1.4730   0.01291   0.00810  -0.0695   0.3467   1.0000
  10.250   1.4877   0.01347   0.00862  -0.0680   0.3347   1.0000
  10.500   1.5006   0.01414   0.00924  -0.0663   0.3225   1.0000
  10.750   1.5121   0.01489   0.00995  -0.0644   0.3102   1.0000
  11.000   1.5253   0.01560   0.01063  -0.0629   0.2993   1.0000
  11.250   1.5371   0.01640   0.01141  -0.0613   0.2894   1.0000
  11.500   1.5457   0.01740   0.01237  -0.0594   0.2787   1.0000
  11.750   1.5553   0.01839   0.01335  -0.0577   0.2682   1.0000
  12.000   1.5639   0.01949   0.01444  -0.0561   0.2591   1.0000
  12.250   1.5698   0.02080   0.01573  -0.0543   0.2503   1.0000
  12.500   1.5795   0.02194   0.01688  -0.0530   0.2435   1.0000
  12.750   1.5843   0.02345   0.01839  -0.0514   0.2362   1.0000
  13.000   1.5916   0.02486   0.01983  -0.0502   0.2297   1.0000
  13.250   1.5947   0.02663   0.02161  -0.0487   0.2227   1.0000
  13.500   1.5980   0.02848   0.02347  -0.0475   0.2162   1.0000
  13.750   1.6001   0.03052   0.02552  -0.0463   0.2095   1.0000
  14.000   1.5988   0.03291   0.02793  -0.0451   0.2036   1.0000
  14.250   1.6024   0.03495   0.03002  -0.0443   0.1982   1.0000
  14.500   1.5987   0.03772   0.03281  -0.0432   0.1924   1.0000
  14.750   1.5991   0.04017   0.03530  -0.0425   0.1876   1.0000
  15.000   1.5991   0.04268   0.03786  -0.0418   0.1824   1.0000
  15.250   1.5920   0.04589   0.04108  -0.0409   0.1767   1.0000
  15.500   1.5907   0.04857   0.04380  -0.0403   0.1710   1.0000
  15.750   1.5817   0.05203   0.04727  -0.0395   0.1638   1.0000
  16.000   1.5761   0.05517   0.05044  -0.0389   0.1568   1.0000
  16.250   1.5642   0.05900   0.05425  -0.0382   0.1487   1.0000
  16.500   1.5559   0.06250   0.05775  -0.0377   0.1397   1.0000
  16.750   1.5456   0.06623   0.06147  -0.0372   0.1315   1.0000
  17.000   1.5321   0.07037   0.06560  -0.0367   0.1229   1.0000
  17.250   1.5216   0.07426   0.06949  -0.0364   0.1149   1.0000
  17.500   1.5137   0.07789   0.07312  -0.0362   0.1076   1.0000
  18.000   1.4964   0.08543   0.08065  -0.0361   0.0934   1.0000
  18.250   1.4852   0.08962   0.08483  -0.0362   0.0843   1.0000
  18.500   1.4610   0.09537   0.09047  -0.0363   0.0657   1.0000
  18.750   1.4338   0.10162   0.09662  -0.0367   0.0495   1.0000
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