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GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 735 AIRFOIL (goe735-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.29 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe735-il-1000000-n5.txt
Download as CSV file: xf-goe735-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 735 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9685   0.09799   0.09488  -0.0399   1.0000   0.0283
 -19.500  -1.0758   0.07901   0.07557  -0.0514   1.0000   0.0280
 -19.250  -1.1656   0.06273   0.05896  -0.0616   1.0000   0.0277
 -18.750  -1.2271   0.04650   0.04234  -0.0728   0.9597   0.0281
 -18.500  -1.1821   0.04106   0.03651  -0.0866   0.8691   0.0287
 -18.250  -1.1936   0.03803   0.03322  -0.0866   0.8248   0.0288
 -17.750  -1.2046   0.03316   0.02805  -0.0858   0.7900   0.0292
 -17.500  -1.2045   0.03139   0.02616  -0.0850   0.7797   0.0297
 -17.250  -1.2035   0.02979   0.02446  -0.0838   0.7700   0.0299
 -17.000  -1.2003   0.02844   0.02301  -0.0824   0.7620   0.0301
 -16.750  -1.1983   0.02708   0.02157  -0.0807   0.7541   0.0305
 -16.500  -1.1953   0.02588   0.02028  -0.0788   0.7465   0.0309
 -16.250  -1.1904   0.02481   0.01914  -0.0769   0.7404   0.0312
 -16.000  -1.1838   0.02388   0.01814  -0.0749   0.7336   0.0316
 -15.750  -1.1759   0.02305   0.01725  -0.0728   0.7268   0.0322
 -15.500  -1.1665   0.02231   0.01645  -0.0707   0.7212   0.0326
 -15.250  -1.1559   0.02164   0.01572  -0.0687   0.7157   0.0332
 -15.000  -1.1441   0.02104   0.01506  -0.0666   0.7094   0.0337
 -14.500  -1.1201   0.01988   0.01378  -0.0624   0.6985   0.0347
 -14.250  -1.1072   0.01933   0.01319  -0.0602   0.6928   0.0354
 -14.000  -1.0937   0.01882   0.01263  -0.0581   0.6868   0.0363
 -13.750  -1.0786   0.01838   0.01214  -0.0561   0.6816   0.0371
 -13.500  -1.0627   0.01796   0.01167  -0.0542   0.6766   0.0379
 -13.250  -1.0468   0.01753   0.01120  -0.0522   0.6699   0.0387
 -13.000  -1.0311   0.01710   0.01073  -0.0501   0.6638   0.0398
 -12.750  -1.0142   0.01671   0.01031  -0.0482   0.6581   0.0409
 -12.500  -0.9965   0.01635   0.00991  -0.0464   0.6518   0.0421
 -12.250  -0.9791   0.01599   0.00951  -0.0445   0.6446   0.0435
 -12.000  -0.9612   0.01564   0.00914  -0.0426   0.6381   0.0452
 -11.750  -0.9424   0.01535   0.00881  -0.0408   0.6296   0.0468
 -11.500  -0.9239   0.01507   0.00849  -0.0390   0.6215   0.0486
 -11.250  -0.9042   0.01479   0.00819  -0.0374   0.6140   0.0505
 -11.000  -0.8829   0.01456   0.00791  -0.0360   0.6048   0.0524
 -10.750  -0.8610   0.01429   0.00762  -0.0348   0.5954   0.0543
 -10.500  -0.8386   0.01406   0.00734  -0.0336   0.5844   0.0565
 -10.250  -0.8152   0.01386   0.00710  -0.0326   0.5753   0.0583
 -10.000  -0.7922   0.01364   0.00685  -0.0315   0.5656   0.0605
  -9.750  -0.7684   0.01344   0.00662  -0.0306   0.5573   0.0627
  -9.500  -0.7441   0.01329   0.00641  -0.0297   0.5469   0.0644
  -9.250  -0.7200   0.01309   0.00619  -0.0288   0.5384   0.0661
  -9.000  -0.6955   0.01292   0.00599  -0.0280   0.5298   0.0680
  -8.750  -0.6705   0.01278   0.00580  -0.0272   0.5226   0.0696
  -8.500  -0.6451   0.01264   0.00562  -0.0265   0.5159   0.0710
  -8.250  -0.6202   0.01248   0.00544  -0.0257   0.5079   0.0726
  -8.000  -0.5949   0.01233   0.00527  -0.0250   0.5013   0.0744
  -7.750  -0.5691   0.01220   0.00511  -0.0244   0.4948   0.0762
  -7.500  -0.5432   0.01209   0.00496  -0.0238   0.4886   0.0777
  -7.250  -0.5172   0.01198   0.00480  -0.0232   0.4831   0.0789
  -7.000  -0.4914   0.01183   0.00465  -0.0226   0.4775   0.0806
  -6.750  -0.4654   0.01171   0.00451  -0.0220   0.4710   0.0823
  -6.500  -0.4392   0.01162   0.00438  -0.0215   0.4649   0.0840
  -6.250  -0.4124   0.01151   0.00426  -0.0210   0.4608   0.0856
  -6.000  -0.3859   0.01141   0.00413  -0.0205   0.4560   0.0874
  -5.750  -0.3596   0.01130   0.00402  -0.0200   0.4507   0.0900
  -5.500  -0.3331   0.01121   0.00392  -0.0195   0.4455   0.0923
  -5.250  -0.3061   0.01113   0.00381  -0.0191   0.4412   0.0941
  -5.000  -0.2790   0.01106   0.00371  -0.0187   0.4361   0.0952
  -4.750  -0.2525   0.01097   0.00360  -0.0182   0.4315   0.0974
  -4.500  -0.2259   0.01089   0.00351  -0.0178   0.4270   0.0996
  -4.250  -0.1988   0.01080   0.00343  -0.0174   0.4239   0.1016
  -4.000  -0.1716   0.01074   0.00335  -0.0171   0.4197   0.1035
  -3.750  -0.1444   0.01070   0.00327  -0.0167   0.4152   0.1051
  -3.500  -0.1178   0.01064   0.00320  -0.0163   0.4104   0.1079
  -3.250  -0.0907   0.01057   0.00314  -0.0159   0.4070   0.1107
  -3.000  -0.0634   0.01051   0.00308  -0.0156   0.4039   0.1133
  -2.750  -0.0360   0.01047   0.00303  -0.0153   0.4004   0.1156
  -2.500  -0.0090   0.01042   0.00298  -0.0150   0.3967   0.1189
  -2.250   0.0178   0.01038   0.00294  -0.0146   0.3926   0.1232
  -2.000   0.0450   0.01035   0.00290  -0.0143   0.3891   0.1269
  -1.750   0.0723   0.01031   0.00287  -0.0141   0.3859   0.1308
  -1.500   0.0994   0.01026   0.00284  -0.0137   0.3824   0.1360
  -1.250   0.1266   0.01025   0.00282  -0.0135   0.3790   0.1406
  -1.000   0.1533   0.01022   0.00280  -0.0131   0.3755   0.1470
  -0.750   0.1800   0.01021   0.00280  -0.0128   0.3721   0.1542
  -0.500   0.2071   0.01016   0.00278  -0.0125   0.3699   0.1625
  -0.250   0.2341   0.01013   0.00278  -0.0122   0.3671   0.1714
   0.000   0.2605   0.01008   0.00277  -0.0118   0.3638   0.1841
   0.250   0.2866   0.01005   0.00278  -0.0114   0.3600   0.2014
   0.500   0.3120   0.01000   0.00280  -0.0109   0.3564   0.2257
   0.750   0.3374   0.00992   0.00281  -0.0104   0.3539   0.2548
   1.000   0.3633   0.00985   0.00283  -0.0099   0.3518   0.2834
   1.250   0.3886   0.00976   0.00286  -0.0094   0.3493   0.3177
   1.500   0.4138   0.00970   0.00289  -0.0088   0.3466   0.3502
   1.750   0.4385   0.00964   0.00293  -0.0082   0.3437   0.3856
   2.000   0.4623   0.00957   0.00297  -0.0074   0.3408   0.4286
   2.250   0.4823   0.00937   0.00302  -0.0060   0.3374   0.5133
   2.500   0.5040   0.00919   0.00306  -0.0047   0.3356   0.5823
   2.750   0.5249   0.00905   0.00311  -0.0033   0.3334   0.6413
   3.000   0.5407   0.00880   0.00316  -0.0008   0.3311   0.7304
   3.250   0.5575   0.00864   0.00325   0.0016   0.3289   0.8060
   3.500   0.5807   0.00861   0.00338   0.0026   0.3263   0.8579
   3.750   0.6168   0.00870   0.00359   0.0010   0.3234   0.9041
   4.000   0.6599   0.00889   0.00380  -0.0022   0.3204   0.9274
   4.250   0.7028   0.00906   0.00398  -0.0054   0.3186   0.9379
   4.500   0.7321   0.00921   0.00413  -0.0057   0.3163   0.9489
   4.750   0.7738   0.00940   0.00430  -0.0087   0.3134   0.9517
   5.000   0.8089   0.00960   0.00448  -0.0103   0.3107   0.9556
   5.250   0.8339   0.00981   0.00467  -0.0098   0.3084   0.9626
   5.500   0.8661   0.01004   0.00488  -0.0108   0.3056   0.9656
   5.750   0.9002   0.01024   0.00507  -0.0123   0.3033   0.9669
   6.000   0.9337   0.01040   0.00523  -0.0137   0.3014   0.9683
   6.250   0.9660   0.01058   0.00540  -0.0148   0.2992   0.9701
   6.500   0.9961   0.01076   0.00558  -0.0155   0.2966   0.9723
   6.750   1.0224   0.01097   0.00577  -0.0156   0.2936   0.9751
   7.000   1.0433   0.01122   0.00600  -0.0145   0.2906   0.9789
   7.250   1.0748   0.01146   0.00623  -0.0157   0.2875   0.9798
   7.500   1.1063   0.01163   0.00641  -0.0168   0.2857   0.9807
   7.750   1.1369   0.01183   0.00662  -0.0178   0.2838   0.9819
   8.000   1.1670   0.01205   0.00684  -0.0187   0.2817   0.9833
   8.250   1.1957   0.01229   0.00709  -0.0194   0.2792   0.9851
   8.500   1.2222   0.01257   0.00736  -0.0197   0.2767   0.9872
   8.750   1.2433   0.01290   0.00767  -0.0191   0.2738   0.9902
   9.000   1.2660   0.01318   0.00798  -0.0188   0.2718   0.9924
   9.250   1.2944   0.01341   0.00822  -0.0196   0.2704   0.9938
   9.500   1.3217   0.01368   0.00851  -0.0203   0.2686   0.9954
   9.750   1.3483   0.01399   0.00886  -0.0210   0.2666   0.9972
  10.000   1.3737   0.01439   0.00926  -0.0217   0.2641   0.9987
  10.250   1.3988   0.01487   0.00975  -0.0225   0.2615   0.9998
  10.500   1.4038   0.01548   0.01038  -0.0197   0.2592   1.0000
  10.750   1.4074   0.01618   0.01109  -0.0168   0.2570   1.0000
  11.000   1.4172   0.01673   0.01168  -0.0148   0.2555   1.0000
  11.250   1.4273   0.01733   0.01232  -0.0130   0.2539   1.0000
  11.500   1.4375   0.01799   0.01301  -0.0113   0.2520   1.0000
  11.750   1.4471   0.01873   0.01377  -0.0096   0.2499   1.0000
  12.000   1.4559   0.01957   0.01463  -0.0080   0.2477   1.0000
  12.250   1.4636   0.02053   0.01560  -0.0065   0.2453   1.0000
  12.500   1.4703   0.02160   0.01669  -0.0049   0.2428   1.0000
  12.750   1.4808   0.02248   0.01761  -0.0038   0.2411   1.0000
  13.000   1.4918   0.02337   0.01853  -0.0028   0.2388   1.0000
  13.250   1.4999   0.02446   0.01965  -0.0016   0.2349   1.0000
  13.500   1.5039   0.02589   0.02108  -0.0004   0.2311   1.0000
  13.750   1.5061   0.02749   0.02269   0.0009   0.2276   1.0000
  14.000   1.5150   0.02865   0.02389   0.0017   0.2241   1.0000
  14.250   1.5169   0.03038   0.02563   0.0027   0.2188   1.0000
  14.500   1.5161   0.03242   0.02769   0.0037   0.2148   1.0000
  14.750   1.5204   0.03412   0.02942   0.0043   0.2105   1.0000
  15.000   1.5236   0.03598   0.03132   0.0049   0.2071   1.0000
  15.250   1.5195   0.03855   0.03390   0.0055   0.2021   1.0000
  15.500   1.5190   0.04086   0.03624   0.0059   0.1988   1.0000
  15.750   1.5181   0.04324   0.03865   0.0063   0.1936   1.0000
  16.000   1.5134   0.04605   0.04149   0.0066   0.1899   1.0000
  16.250   1.5040   0.04939   0.04485   0.0068   0.1850   1.0000
  16.500   1.5035   0.05188   0.04739   0.0069   0.1821   1.0000
  16.750   1.4968   0.05503   0.05057   0.0070   0.1777   1.0000
  17.000   1.4833   0.05897   0.05454   0.0069   0.1735   1.0000
  17.250   1.4814   0.06175   0.05737   0.0068   0.1710   1.0000
  17.500   1.4738   0.06515   0.06081   0.0066   0.1661   1.0000
  17.750   1.4588   0.06946   0.06515   0.0062   0.1620   1.0000
  18.000   1.4541   0.07266   0.06840   0.0059   0.1598   1.0000
  18.250   1.4510   0.07572   0.07150   0.0055   0.1565   1.0000
  18.500   1.4362   0.08019   0.07600   0.0048   0.1517   1.0000
  18.750   1.4283   0.08387   0.07971   0.0042   0.1488   1.0000
  19.000   1.4250   0.08707   0.08298   0.0036   0.1468   1.0000
  19.250   1.4205   0.09044   0.08638   0.0029   0.1427   1.0000
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