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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 500,000
Max Cl/Cd: 57.38 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe703-il-500000-n5.txt
Download as CSV file: xf-goe703-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 703 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9179   0.09801   0.09355  -0.0667   1.0000   0.0285
 -19.500  -0.9296   0.09287   0.08830  -0.0692   1.0000   0.0286
 -19.250  -0.9406   0.08790   0.08322  -0.0716   1.0000   0.0287
 -19.000  -0.9507   0.08312   0.07834  -0.0738   1.0000   0.0288
 -18.750  -0.9597   0.07856   0.07368  -0.0759   1.0000   0.0289
 -18.500  -0.9690   0.07405   0.06906  -0.0779   1.0000   0.0290
 -18.250  -0.9772   0.06979   0.06470  -0.0797   1.0000   0.0291
 -18.000  -0.9840   0.06577   0.06056  -0.0813   1.0000   0.0292
 -17.750  -0.9895   0.06206   0.05676  -0.0826   1.0000   0.0293
 -17.500  -0.9946   0.05855   0.05314  -0.0836   1.0000   0.0294
 -17.250  -0.9983   0.05534   0.04983  -0.0844   1.0000   0.0295
 -17.000  -1.0009   0.05236   0.04676  -0.0849   1.0000   0.0296
 -16.750  -1.0028   0.04963   0.04393  -0.0851   1.0000   0.0297
 -16.500  -1.0037   0.04713   0.04134  -0.0850   1.0000   0.0297
 -16.250  -1.0043   0.04478   0.03892  -0.0846   1.0000   0.0298
 -16.000  -1.0070   0.04242   0.03649  -0.0839   1.0000   0.0300
 -15.750  -1.0075   0.04035   0.03437  -0.0829   1.0000   0.0302
 -15.500  -1.0069   0.03851   0.03247  -0.0818   1.0000   0.0302
 -15.250  -1.0063   0.03678   0.03069  -0.0803   1.0000   0.0304
 -15.000  -1.0047   0.03522   0.02908  -0.0787   1.0000   0.0306
 -14.750  -1.0020   0.03384   0.02765  -0.0769   1.0000   0.0308
 -14.500  -0.9987   0.03259   0.02636  -0.0749   1.0000   0.0310
 -14.250  -0.9946   0.03147   0.02520  -0.0728   1.0000   0.0312
 -14.000  -0.9911   0.03039   0.02407  -0.0705   1.0000   0.0313
 -13.750  -0.9821   0.02936   0.02299  -0.0690   0.9996   0.0316
 -13.250  -0.9366   0.02711   0.02065  -0.0709   0.9928   0.0323
 -12.250  -0.8590   0.02349   0.01682  -0.0703   0.9573   0.0335
 -12.000  -0.8311   0.02262   0.01590  -0.0716   0.9467   0.0339
 -11.750  -0.7979   0.02167   0.01492  -0.0741   0.9362   0.0343
 -11.500  -0.7586   0.02079   0.01399  -0.0778   0.9252   0.0349
 -11.250  -0.7111   0.01998   0.01314  -0.0829   0.9141   0.0356
 -11.000  -0.6601   0.01924   0.01232  -0.0888   0.9021   0.0365
 -10.750  -0.6157   0.01861   0.01160  -0.0932   0.8875   0.0372
 -10.500  -0.5778   0.01811   0.01098  -0.0962   0.8711   0.0380
 -10.250  -0.5493   0.01762   0.01041  -0.0972   0.8561   0.0388
 -10.000  -0.5261   0.01721   0.00993  -0.0969   0.8403   0.0396
  -9.750  -0.5052   0.01685   0.00951  -0.0961   0.8280   0.0404
  -9.250  -0.4656   0.01626   0.00878  -0.0938   0.8046   0.0428
  -9.000  -0.4474   0.01594   0.00840  -0.0924   0.7929   0.0439
  -8.750  -0.4294   0.01564   0.00806  -0.0908   0.7805   0.0457
  -8.500  -0.4107   0.01539   0.00775  -0.0892   0.7690   0.0471
  -8.250  -0.3928   0.01512   0.00744  -0.0876   0.7568   0.0488
  -8.000  -0.3749   0.01485   0.00713  -0.0858   0.7448   0.0513
  -7.750  -0.3573   0.01462   0.00685  -0.0840   0.7317   0.0541
  -7.500  -0.3399   0.01438   0.00656  -0.0821   0.7166   0.0579
  -7.250  -0.3225   0.01413   0.00629  -0.0803   0.7025   0.0628
  -7.000  -0.3053   0.01390   0.00603  -0.0783   0.6895   0.0691
  -6.750  -0.2883   0.01365   0.00578  -0.0764   0.6775   0.0793
  -6.500  -0.2712   0.01338   0.00555  -0.0745   0.6671   0.0928
  -6.250  -0.2538   0.01317   0.00534  -0.0725   0.6570   0.1066
  -6.000  -0.2353   0.01298   0.00517  -0.0708   0.6480   0.1191
  -5.750  -0.2166   0.01280   0.00500  -0.0691   0.6393   0.1301
  -5.500  -0.1976   0.01265   0.00485  -0.0674   0.6324   0.1397
  -5.250  -0.1778   0.01249   0.00471  -0.0659   0.6260   0.1490
  -5.000  -0.1583   0.01237   0.00457  -0.0643   0.6192   0.1581
  -4.750  -0.1396   0.01224   0.00444  -0.0625   0.6131   0.1681
  -4.500  -0.1193   0.01210   0.00433  -0.0610   0.6077   0.1777
  -4.250  -0.0994   0.01197   0.00421  -0.0595   0.6020   0.1878
  -4.000  -0.0804   0.01184   0.00411  -0.0577   0.5965   0.2000
  -3.750  -0.0616   0.01170   0.00401  -0.0560   0.5917   0.2157
  -3.500  -0.0425   0.01154   0.00392  -0.0542   0.5868   0.2333
  -3.250  -0.0244   0.01137   0.00382  -0.0523   0.5818   0.2538
  -3.000  -0.0064   0.01124   0.00373  -0.0504   0.5767   0.2720
  -2.750   0.0120   0.01113   0.00364  -0.0484   0.5719   0.2890
  -2.500   0.0309   0.01098   0.00356  -0.0466   0.5669   0.3071
  -2.250   0.0484   0.01083   0.00347  -0.0445   0.5623   0.3265
  -2.000   0.0640   0.01067   0.00338  -0.0420   0.5572   0.3508
  -1.500   0.0837   0.01012   0.00318  -0.0347   0.5486   0.4457
  -1.250   0.0862   0.00977   0.00308  -0.0294   0.5446   0.5080
  -1.000   0.0873   0.00950   0.00301  -0.0238   0.5403   0.5608
  -0.750   0.0859   0.00928   0.00296  -0.0175   0.5361   0.6128
  -0.500   0.0827   0.00909   0.00296  -0.0107   0.5323   0.6640
  -0.250   0.0882   0.00889   0.00301  -0.0057   0.5287   0.7204
   0.000   0.1096   0.00882   0.00309  -0.0041   0.5244   0.7612
   0.250   0.1355   0.00885   0.00318  -0.0036   0.5198   0.7893
   0.500   0.1610   0.00893   0.00327  -0.0029   0.5151   0.8089
   0.750   0.1903   0.00902   0.00338  -0.0031   0.5105   0.8258
   1.000   0.2252   0.00913   0.00352  -0.0045   0.5057   0.8374
   1.250   0.2407   0.00921   0.00359  -0.0017   0.5012   0.8491
   1.500   0.2733   0.00938   0.00374  -0.0026   0.4963   0.8579
   1.750   0.2872   0.00946   0.00382   0.0005   0.4918   0.8674
   2.000   0.3257   0.00965   0.00401  -0.0016   0.4864   0.8734
   2.750   0.4012   0.01015   0.00445   0.0004   0.4681   0.8910
   3.000   0.3897   0.01015   0.00445   0.0090   0.4625   0.9013
   3.250   0.4315   0.01044   0.00469   0.0059   0.4550   0.9033
   3.500   0.4717   0.01067   0.00492   0.0033   0.4481   0.9050
   3.750   0.5015   0.01088   0.00510   0.0028   0.4412   0.9073
   4.000   0.5216   0.01101   0.00521   0.0044   0.4349   0.9106
   4.250   0.5094   0.01094   0.00514   0.0130   0.4290   0.9192
   4.500   0.5399   0.01114   0.00530   0.0122   0.4214   0.9203
   4.750   0.5702   0.01129   0.00545   0.0115   0.4141   0.9214
   5.000   0.5959   0.01150   0.00561   0.0117   0.4051   0.9229
   5.250   0.6205   0.01169   0.00578   0.0122   0.3961   0.9249
   5.500   0.6395   0.01188   0.00594   0.0138   0.3875   0.9279
   5.750   0.6332   0.01190   0.00595   0.0208   0.3814   0.9357
   6.000   0.6618   0.01216   0.00618   0.0202   0.3706   0.9367
   6.250   0.6886   0.01243   0.00641   0.0200   0.3602   0.9378
   6.500   0.7137   0.01270   0.00666   0.0202   0.3519   0.9391
   6.750   0.7379   0.01296   0.00690   0.0205   0.3438   0.9407
   7.000   0.7587   0.01327   0.00718   0.0214   0.3342   0.9429
   7.250   0.7758   0.01352   0.00742   0.0232   0.3277   0.9465
   7.500   0.7805   0.01375   0.00763   0.0274   0.3190   0.9519
   7.750   0.8055   0.01412   0.00798   0.0272   0.3101   0.9528
   8.000   0.8294   0.01453   0.00836   0.0272   0.2999   0.9539
   8.250   0.8533   0.01493   0.00875   0.0272   0.2907   0.9553
   8.500   0.8737   0.01543   0.00921   0.0277   0.2805   0.9572
   8.750   0.8934   0.01584   0.00961   0.0285   0.2711   0.9595
   9.000   0.9036   0.01635   0.01010   0.0309   0.2618   0.9634
   9.250   0.9143   0.01692   0.01064   0.0331   0.2498   0.9668
   9.500   0.9347   0.01765   0.01132   0.0331   0.2350   0.9680
   9.750   0.9527   0.01847   0.01208   0.0333   0.2200   0.9695
  10.000   0.9678   0.01938   0.01294   0.0338   0.2052   0.9714
  10.250   0.9793   0.02041   0.01391   0.0349   0.1905   0.9738
  10.500   0.9888   0.02141   0.01487   0.0363   0.1798   0.9768
  10.750   0.9958   0.02249   0.01592   0.0382   0.1711   0.9802
  11.000   1.0132   0.02353   0.01695   0.0379   0.1626   0.9813
  11.250   1.0282   0.02468   0.01809   0.0379   0.1556   0.9825
  11.500   1.0440   0.02575   0.01918   0.0378   0.1503   0.9838
  11.750   1.0564   0.02705   0.02047   0.0380   0.1449   0.9854
  12.000   1.0709   0.02819   0.02164   0.0380   0.1412   0.9871
  12.250   1.0838   0.02946   0.02294   0.0382   0.1371   0.9889
  12.500   1.0937   0.03097   0.02445   0.0385   0.1331   0.9908
  12.750   1.1046   0.03232   0.02584   0.0389   0.1307   0.9923
  13.000   1.1192   0.03365   0.02721   0.0385   0.1278   0.9934
  13.250   1.1318   0.03513   0.02872   0.0382   0.1248   0.9947
  13.500   1.1426   0.03680   0.03041   0.0379   0.1220   0.9959
  13.750   1.1539   0.03850   0.03215   0.0375   0.1193   0.9971
  14.000   1.1679   0.04004   0.03373   0.0369   0.1166   0.9982
  14.250   1.1801   0.04177   0.03551   0.0363   0.1139   0.9991
  14.500   1.1893   0.04375   0.03751   0.0357   0.1105   0.9998
  14.750   1.1911   0.04566   0.03945   0.0367   0.1086   1.0000
  15.000   1.1944   0.04716   0.04101   0.0380   0.1061   1.0000
  15.250   1.1958   0.04890   0.04279   0.0392   0.1038   1.0000
  15.500   1.1952   0.05087   0.04479   0.0404   0.1005   1.0000
  15.750   1.1944   0.05290   0.04684   0.0415   0.0976   1.0000
  16.000   1.1964   0.05472   0.04871   0.0425   0.0935   1.0000
  16.250   1.1948   0.05695   0.05096   0.0434   0.0881   1.0000
  16.500   1.1899   0.05959   0.05358   0.0442   0.0781   1.0000
  16.750   1.1816   0.06264   0.05659   0.0449   0.0699   1.0000
  17.000   1.1759   0.06550   0.05945   0.0454   0.0660   1.0000
  17.250   1.1697   0.06850   0.06247   0.0458   0.0629   1.0000
  17.500   1.1658   0.07129   0.06529   0.0462   0.0611   1.0000
  17.750   1.1608   0.07429   0.06834   0.0464   0.0595   1.0000
  18.000   1.1582   0.07705   0.07115   0.0465   0.0582   1.0000
  18.250   1.1551   0.07993   0.07408   0.0465   0.0572   1.0000
  18.500   1.1509   0.08300   0.07721   0.0464   0.0561   1.0000
  18.750   1.1460   0.08621   0.08046   0.0463   0.0551   1.0000
  19.000   1.1407   0.08951   0.08382   0.0459   0.0545   1.0000
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