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GOE 436 AIRFOIL (goe436-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 436 AIRFOIL (goe436-il)
Reynolds number: 1,000,000
Max Cl/Cd: 118.34 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe436-il-1000000.txt
Download as CSV file: xf-goe436-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 436 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.0513   0.04006   0.03768  -0.0916   1.0000   0.0176
 -15.000  -1.0968   0.03482   0.03220  -0.0896   1.0000   0.0176
 -14.750  -1.1110   0.03203   0.02922  -0.0865   1.0000   0.0177
 -14.500  -1.1196   0.02965   0.02668  -0.0835   1.0000   0.0181
 -14.250  -1.1196   0.02794   0.02486  -0.0807   1.0000   0.0185
 -14.000  -1.1120   0.02681   0.02368  -0.0783   1.0000   0.0190
 -13.750  -1.1016   0.02591   0.02271  -0.0761   1.0000   0.0195
 -13.500  -1.0908   0.02501   0.02173  -0.0739   1.0000   0.0200
 -13.250  -1.0790   0.02416   0.02079  -0.0718   1.0000   0.0205
 -13.000  -1.0664   0.02335   0.01987  -0.0696   1.0000   0.0209
 -12.750  -1.0528   0.02261   0.01901  -0.0676   1.0000   0.0213
 -12.500  -1.0265   0.02148   0.01781  -0.0685   0.9987   0.0222
 -12.250  -0.9938   0.02117   0.01751  -0.0698   0.9973   0.0230
 -12.000  -0.9607   0.02079   0.01709  -0.0712   0.9958   0.0238
 -11.750  -0.9275   0.02024   0.01645  -0.0728   0.9945   0.0245
 -11.500  -0.8954   0.01974   0.01584  -0.0740   0.9930   0.0251
 -11.250  -0.8689   0.01864   0.01463  -0.0746   0.9904   0.0259
 -11.000  -0.8367   0.01837   0.01437  -0.0757   0.9884   0.0267
 -10.750  -0.8026   0.01833   0.01435  -0.0770   0.9868   0.0274
 -10.500  -0.7689   0.01807   0.01404  -0.0784   0.9853   0.0282
 -10.250  -0.7352   0.01765   0.01354  -0.0798   0.9841   0.0289
 -10.000  -0.7009   0.01726   0.01306  -0.0813   0.9831   0.0295
  -9.750  -0.6759   0.01624   0.01190  -0.0813   0.9790   0.0303
  -9.500  -0.6443   0.01588   0.01154  -0.0822   0.9764   0.0311
  -9.250  -0.6099   0.01578   0.01145  -0.0836   0.9745   0.0318
  -9.000  -0.5752   0.01560   0.01125  -0.0850   0.9730   0.0325
  -8.750  -0.5404   0.01533   0.01093  -0.0865   0.9717   0.0334
  -8.500  -0.5063   0.01494   0.01047  -0.0879   0.9702   0.0341
  -8.250  -0.4791   0.01464   0.01010  -0.0878   0.9639   0.0346
  -8.000  -0.4495   0.01359   0.00889  -0.0885   0.9586   0.0356
  -7.750  -0.4193   0.01315   0.00843  -0.0890   0.9523   0.0364
  -7.500  -0.3905   0.01296   0.00823  -0.0891   0.9443   0.0371
  -7.250  -0.3618   0.01274   0.00797  -0.0892   0.9363   0.0378
  -7.000  -0.3337   0.01246   0.00762  -0.0891   0.9268   0.0386
  -6.750  -0.3073   0.01213   0.00722  -0.0887   0.9164   0.0394
  -6.500  -0.2803   0.01185   0.00685  -0.0884   0.9056   0.0400
  -6.000  -0.2281   0.01117   0.00597  -0.0874   0.8824   0.0413
  -5.750  -0.2036   0.01055   0.00527  -0.0867   0.8719   0.0424
  -5.500  -0.1775   0.01033   0.00500  -0.0862   0.8611   0.0432
  -5.250  -0.1514   0.01016   0.00478  -0.0857   0.8500   0.0440
  -5.000  -0.1251   0.01002   0.00459  -0.0852   0.8398   0.0449
  -4.750  -0.0987   0.00987   0.00438  -0.0847   0.8308   0.0459
  -4.500  -0.0723   0.00969   0.00415  -0.0843   0.8221   0.0468
  -4.250  -0.0459   0.00956   0.00395  -0.0838   0.8130   0.0475
  -4.000  -0.0192   0.00945   0.00380  -0.0834   0.8031   0.0479
  -3.750   0.0048   0.00889   0.00318  -0.0825   0.7938   0.0497
  -3.500   0.0309   0.00871   0.00298  -0.0820   0.7836   0.0509
  -3.250   0.0575   0.00861   0.00286  -0.0816   0.7729   0.0523
  -3.000   0.0838   0.00852   0.00273  -0.0811   0.7604   0.0536
  -2.750   0.1098   0.00842   0.00257  -0.0805   0.7453   0.0548
  -2.500   0.1357   0.00835   0.00244  -0.0799   0.7267   0.0558
  -2.250   0.1613   0.00835   0.00234  -0.0792   0.7040   0.0565
  -2.000   0.1850   0.00810   0.00199  -0.0782   0.6810   0.0591
  -1.750   0.2100   0.00808   0.00190  -0.0775   0.6586   0.0611
  -1.250   0.2609   0.00811   0.00177  -0.0762   0.6211   0.0648
  -1.000   0.2868   0.00814   0.00173  -0.0757   0.6035   0.0662
  -0.750   0.3124   0.00808   0.00161  -0.0751   0.5862   0.0689
  -0.500   0.3381   0.00806   0.00154  -0.0745   0.5673   0.0728
  -0.250   0.3636   0.00811   0.00151  -0.0739   0.5439   0.0763
   0.000   0.3888   0.00820   0.00150  -0.0732   0.5140   0.0786
   0.250   0.4129   0.00827   0.00147  -0.0724   0.4812   0.0871
   0.500   0.4375   0.00837   0.00148  -0.0717   0.4554   0.0983
   0.750   0.4620   0.00835   0.00152  -0.0710   0.4364   0.1413
   1.000   0.4843   0.00799   0.00157  -0.0700   0.4233   0.3135
   1.250   0.5029   0.00738   0.00165  -0.0684   0.4128   0.5841
   1.500   0.5174   0.00677   0.00175  -0.0655   0.4048   0.8244
   1.750   0.5753   0.00672   0.00196  -0.0718   0.3941   0.9693
   2.250   0.6905   0.00709   0.00215  -0.0847   0.3713   0.9999
   2.500   0.7140   0.00721   0.00221  -0.0838   0.3642   1.0000
   2.750   0.7374   0.00729   0.00227  -0.0828   0.3592   1.0000
   3.000   0.7603   0.00740   0.00234  -0.0817   0.3532   1.0000
   3.250   0.7835   0.00752   0.00242  -0.0807   0.3468   1.0000
   3.500   0.8069   0.00762   0.00249  -0.0797   0.3398   1.0000
   3.750   0.8298   0.00777   0.00259  -0.0786   0.3331   1.0000
   4.000   0.8538   0.00785   0.00267  -0.0778   0.3279   1.0000
   4.250   0.8771   0.00799   0.00277  -0.0768   0.3211   1.0000
   4.500   0.9007   0.00811   0.00288  -0.0759   0.3159   1.0000
   4.750   0.9247   0.00822   0.00298  -0.0750   0.3111   1.0000
   5.000   0.9482   0.00836   0.00309  -0.0741   0.3060   1.0000
   5.250   0.9718   0.00850   0.00322  -0.0732   0.3010   1.0000
   5.500   0.9960   0.00861   0.00334  -0.0724   0.2960   1.0000
   5.750   1.0194   0.00876   0.00347  -0.0715   0.2899   1.0000
   6.000   1.0432   0.00890   0.00360  -0.0707   0.2838   1.0000
   6.250   1.0669   0.00905   0.00375  -0.0698   0.2769   1.0000
   6.500   1.0901   0.00923   0.00390  -0.0689   0.2695   1.0000
   6.750   1.1131   0.00941   0.00406  -0.0679   0.2600   1.0000
   7.000   1.1361   0.00960   0.00423  -0.0670   0.2505   1.0000
   7.250   1.1579   0.00987   0.00443  -0.0659   0.2349   1.0000
   7.500   1.1774   0.01027   0.00470  -0.0644   0.2099   1.0000
   7.750   1.1937   0.01089   0.00511  -0.0624   0.1746   1.0000
   8.000   1.2088   0.01159   0.00561  -0.0603   0.1424   1.0000
   8.250   1.2246   0.01223   0.00610  -0.0583   0.1170   1.0000
   8.500   1.2397   0.01291   0.00661  -0.0561   0.0895   1.0000
   8.750   1.2524   0.01371   0.00723  -0.0537   0.0640   1.0000
   9.000   1.2708   0.01412   0.00764  -0.0521   0.0589   1.0000
   9.250   1.2891   0.01452   0.00805  -0.0505   0.0565   1.0000
   9.500   1.3050   0.01495   0.00849  -0.0484   0.0542   1.0000
   9.750   1.3195   0.01540   0.00896  -0.0461   0.0517   1.0000
  10.000   1.3356   0.01576   0.00937  -0.0442   0.0503   1.0000
  10.250   1.3529   0.01609   0.00973  -0.0424   0.0492   1.0000
  10.500   1.3691   0.01647   0.01016  -0.0406   0.0476   1.0000
  10.750   1.3842   0.01693   0.01064  -0.0387   0.0460   1.0000
  11.000   1.3976   0.01749   0.01122  -0.0366   0.0438   1.0000
  11.250   1.4118   0.01802   0.01179  -0.0347   0.0420   1.0000
  11.500   1.4296   0.01837   0.01218  -0.0333   0.0405   1.0000
  11.750   1.4446   0.01888   0.01270  -0.0317   0.0378   1.0000
  12.000   1.4580   0.01949   0.01331  -0.0299   0.0343   1.0000
  12.250   1.4702   0.02019   0.01398  -0.0280   0.0291   1.0000
  12.500   1.4790   0.02112   0.01487  -0.0259   0.0229   1.0000
  12.750   1.4863   0.02218   0.01593  -0.0237   0.0198   1.0000
  13.000   1.4936   0.02331   0.01710  -0.0217   0.0180   1.0000
  13.250   1.4984   0.02467   0.01849  -0.0197   0.0166   1.0000
  13.500   1.5065   0.02586   0.01977  -0.0182   0.0159   1.0000
  13.750   1.5123   0.02729   0.02126  -0.0166   0.0151   1.0000
  14.000   1.5171   0.02888   0.02291  -0.0153   0.0147   1.0000
  14.250   1.5177   0.03090   0.02500  -0.0138   0.0139   1.0000
  14.500   1.5175   0.03313   0.02732  -0.0127   0.0135   1.0000
  14.750   1.5217   0.03506   0.02934  -0.0119   0.0132   1.0000
  15.000   1.5234   0.03731   0.03167  -0.0113   0.0128   1.0000
  15.250   1.5238   0.03982   0.03427  -0.0109   0.0125   1.0000
  15.500   1.5219   0.04273   0.03728  -0.0108   0.0123   1.0000
  15.750   1.5181   0.04596   0.04061  -0.0109   0.0120   1.0000
  16.000   1.5130   0.04949   0.04423  -0.0113   0.0118   1.0000
  16.250   1.5066   0.05328   0.04812  -0.0118   0.0117   1.0000
  16.500   1.4956   0.05777   0.05272  -0.0127   0.0115   1.0000
  16.750   1.4815   0.06286   0.05793  -0.0139   0.0112   1.0000
  17.000   1.4653   0.06837   0.06356  -0.0153   0.0111   1.0000
  17.250   1.4497   0.07387   0.06917  -0.0169   0.0109   1.0000
  17.500   1.4353   0.07930   0.07470  -0.0184   0.0108   1.0000
  17.750   1.4248   0.08416   0.07967  -0.0198   0.0108   1.0000
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