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GOE 629 AIRFOIL (goe629-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 629 AIRFOIL (goe629-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.16 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe629-il-1000000.txt
Download as CSV file: xf-goe629-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 629 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9816   0.08165   0.07854  -0.0654   1.0000   0.0205
 -17.250  -1.0824   0.06383   0.06047  -0.0758   1.0000   0.0196
 -17.000  -1.1800   0.04543   0.04171  -0.0878   1.0000   0.0185
 -16.750  -1.2139   0.03663   0.03266  -0.0948   1.0000   0.0185
 -16.500  -1.2318   0.03203   0.02791  -0.0971   1.0000   0.0187
 -16.250  -1.2433   0.02927   0.02503  -0.0967   1.0000   0.0190
 -16.000  -1.2514   0.02740   0.02306  -0.0947   1.0000   0.0192
 -15.750  -1.2585   0.02603   0.02160  -0.0916   1.0000   0.0196
 -15.500  -1.2663   0.02504   0.02054  -0.0873   1.0000   0.0199
 -15.250  -1.2812   0.02432   0.01975  -0.0811   1.0000   0.0202
 -15.000  -1.2966   0.02361   0.01897  -0.0745   1.0000   0.0206
 -14.750  -1.3022   0.02275   0.01806  -0.0697   1.0000   0.0212
 -14.500  -1.2800   0.02167   0.01691  -0.0701   0.9986   0.0225
 -14.250  -1.2540   0.02070   0.01588  -0.0710   0.9967   0.0241
 -14.000  -1.2282   0.01970   0.01484  -0.0719   0.9948   0.0264
 -13.750  -1.2008   0.01880   0.01391  -0.0730   0.9935   0.0292
 -13.500  -1.1772   0.01802   0.01310  -0.0730   0.9910   0.0325
 -13.250  -1.1510   0.01735   0.01242  -0.0734   0.9886   0.0359
 -13.000  -1.1232   0.01670   0.01176  -0.0741   0.9866   0.0396
 -12.750  -1.0932   0.01619   0.01122  -0.0751   0.9851   0.0426
 -12.500  -1.0620   0.01573   0.01076  -0.0762   0.9839   0.0458
 -12.250  -1.0300   0.01532   0.01032  -0.0775   0.9830   0.0484
 -12.000  -0.9973   0.01494   0.00996  -0.0788   0.9822   0.0513
 -11.750  -0.9722   0.01468   0.00965  -0.0784   0.9787   0.0532
 -11.500  -0.9438   0.01429   0.00924  -0.0788   0.9761   0.0553
 -11.250  -0.9127   0.01396   0.00891  -0.0797   0.9744   0.0575
 -11.000  -0.8800   0.01371   0.00864  -0.0809   0.9731   0.0595
 -10.750  -0.8463   0.01349   0.00837  -0.0821   0.9720   0.0609
 -10.500  -0.8136   0.01305   0.00792  -0.0834   0.9710   0.0633
 -10.250  -0.7783   0.01275   0.00763  -0.0851   0.9702   0.0654
 -10.000  -0.7423   0.01248   0.00734  -0.0870   0.9692   0.0672
  -9.750  -0.7164   0.01229   0.00711  -0.0865   0.9645   0.0685
  -9.500  -0.6851   0.01203   0.00681  -0.0873   0.9611   0.0699
  -9.250  -0.6544   0.01158   0.00636  -0.0880   0.9581   0.0725
  -9.000  -0.6207   0.01133   0.00611  -0.0893   0.9554   0.0749
  -8.750  -0.5941   0.01116   0.00592  -0.0890   0.9498   0.0767
  -8.500  -0.5661   0.01100   0.00571  -0.0889   0.9444   0.0780
  -8.250  -0.5362   0.01069   0.00535  -0.0894   0.9402   0.0797
  -8.000  -0.5124   0.01036   0.00501  -0.0886   0.9341   0.0819
  -7.750  -0.4868   0.01012   0.00475  -0.0881   0.9282   0.0837
  -7.500  -0.4578   0.00991   0.00451  -0.0882   0.9235   0.0855
  -7.250  -0.4329   0.00974   0.00432  -0.0876   0.9175   0.0871
  -7.000  -0.4065   0.00959   0.00412  -0.0871   0.9114   0.0883
  -6.500  -0.3550   0.00914   0.00363  -0.0861   0.8990   0.0931
  -6.250  -0.3284   0.00896   0.00344  -0.0857   0.8926   0.0959
  -6.000  -0.3019   0.00881   0.00326  -0.0853   0.8862   0.0983
  -5.750  -0.2757   0.00870   0.00311  -0.0848   0.8793   0.1001
  -5.500  -0.2492   0.00850   0.00291  -0.0844   0.8729   0.1055
  -5.250  -0.2236   0.00836   0.00279  -0.0839   0.8660   0.1100
  -5.000  -0.1971   0.00823   0.00265  -0.0834   0.8589   0.1156
  -4.750  -0.1707   0.00811   0.00255  -0.0830   0.8520   0.1224
  -4.500  -0.1444   0.00801   0.00244  -0.0825   0.8440   0.1289
  -4.250  -0.1178   0.00792   0.00236  -0.0821   0.8366   0.1359
  -4.000  -0.0910   0.00787   0.00228  -0.0817   0.8286   0.1403
  -3.750  -0.0647   0.00777   0.00218  -0.0812   0.8209   0.1467
  -3.500  -0.0384   0.00771   0.00211  -0.0807   0.8115   0.1513
  -3.250  -0.0117   0.00769   0.00204  -0.0803   0.8018   0.1542
  -3.000   0.0139   0.00760   0.00193  -0.0796   0.7910   0.1599
  -2.750   0.0398   0.00753   0.00187  -0.0790   0.7799   0.1649
  -2.500   0.0658   0.00751   0.00180  -0.0785   0.7688   0.1687
  -2.250   0.0918   0.00748   0.00173  -0.0779   0.7570   0.1726
  -2.000   0.1173   0.00741   0.00167  -0.0772   0.7447   0.1786
  -1.750   0.1426   0.00739   0.00161  -0.0765   0.7304   0.1837
  -1.500   0.1679   0.00738   0.00156  -0.0758   0.7157   0.1894
  -1.250   0.1927   0.00735   0.00152  -0.0750   0.7009   0.1989
  -1.000   0.2175   0.00732   0.00149  -0.0742   0.6860   0.2106
  -0.750   0.2422   0.00729   0.00147  -0.0734   0.6704   0.2274
  -0.500   0.2666   0.00724   0.00145  -0.0726   0.6547   0.2510
  -0.250   0.2909   0.00719   0.00145  -0.0718   0.6398   0.2796
   0.000   0.3151   0.00715   0.00146  -0.0709   0.6256   0.3108
   0.250   0.3391   0.00709   0.00147  -0.0700   0.6122   0.3460
   0.500   0.3628   0.00704   0.00149  -0.0691   0.5990   0.3844
   0.750   0.3863   0.00696   0.00152  -0.0681   0.5863   0.4355
   1.000   0.4095   0.00683   0.00156  -0.0671   0.5757   0.4962
   1.250   0.4314   0.00672   0.00161  -0.0658   0.5658   0.5646
   1.500   0.4532   0.00652   0.00165  -0.0644   0.5572   0.6450
   1.750   0.4716   0.00633   0.00173  -0.0622   0.5488   0.7429
   2.000   0.4919   0.00617   0.00181  -0.0604   0.5405   0.8216
   2.250   0.5159   0.00612   0.00193  -0.0592   0.5307   0.8902
   2.500   0.5545   0.00622   0.00208  -0.0613   0.5183   0.9357
   2.750   0.5986   0.00638   0.00221  -0.0648   0.5052   0.9546
   3.000   0.6383   0.00656   0.00233  -0.0673   0.4906   0.9652
   3.250   0.6766   0.00674   0.00246  -0.0695   0.4782   0.9726
   3.500   0.7089   0.00694   0.00259  -0.0703   0.4616   0.9805
   3.750   0.7483   0.00715   0.00272  -0.0728   0.4387   0.9847
   4.000   0.7848   0.00743   0.00286  -0.0747   0.4099   0.9890
   4.250   0.8176   0.00775   0.00303  -0.0759   0.3802   0.9932
   4.500   0.8584   0.00806   0.00321  -0.0788   0.3533   0.9966
   4.750   0.8969   0.00837   0.00340  -0.0813   0.3310   0.9994
   5.250   0.9390   0.00879   0.00369  -0.0786   0.3019   1.0000
   5.500   0.9573   0.00896   0.00383  -0.0766   0.2911   1.0000
   5.750   0.9747   0.00917   0.00398  -0.0745   0.2787   1.0000
   6.250   1.0088   0.00964   0.00433  -0.0701   0.2495   1.0000
   6.500   1.0249   0.00992   0.00452  -0.0677   0.2297   1.0000
   6.750   1.0389   0.01029   0.00477  -0.0650   0.2051   1.0000
   7.000   1.0517   0.01072   0.00505  -0.0621   0.1803   1.0000
   7.250   1.0644   0.01115   0.00537  -0.0592   0.1602   1.0000
   7.750   1.0886   0.01191   0.00597  -0.0530   0.1298   1.0000
   8.250   1.1132   0.01266   0.00658  -0.0471   0.1046   1.0000
   8.500   1.1268   0.01306   0.00693  -0.0445   0.0938   1.0000
   8.750   1.1406   0.01349   0.00730  -0.0420   0.0835   1.0000
   9.000   1.1541   0.01396   0.00772  -0.0395   0.0728   1.0000
   9.250   1.1650   0.01458   0.00823  -0.0367   0.0558   1.0000
   9.500   1.1748   0.01529   0.00883  -0.0338   0.0427   1.0000
   9.750   1.1884   0.01585   0.00937  -0.0316   0.0385   1.0000
  10.000   1.2022   0.01641   0.00993  -0.0295   0.0362   1.0000
  10.250   1.2165   0.01697   0.01051  -0.0275   0.0347   1.0000
  10.500   1.2319   0.01749   0.01106  -0.0257   0.0338   1.0000
  10.750   1.2465   0.01807   0.01167  -0.0239   0.0330   1.0000
  11.000   1.2601   0.01872   0.01235  -0.0221   0.0321   1.0000
  11.250   1.2716   0.01951   0.01316  -0.0200   0.0310   1.0000
  11.500   1.2817   0.02042   0.01411  -0.0179   0.0302   1.0000
  11.750   1.2958   0.02110   0.01484  -0.0164   0.0298   1.0000
  12.000   1.3089   0.02188   0.01567  -0.0148   0.0294   1.0000
  12.250   1.3213   0.02272   0.01656  -0.0133   0.0289   1.0000
  12.500   1.3330   0.02363   0.01751  -0.0118   0.0284   1.0000
  12.750   1.3436   0.02465   0.01858  -0.0102   0.0279   1.0000
  13.000   1.3536   0.02574   0.01971  -0.0088   0.0274   1.0000
  13.250   1.3610   0.02706   0.02108  -0.0072   0.0269   1.0000
  13.500   1.3655   0.02866   0.02273  -0.0056   0.0264   1.0000
  13.750   1.3657   0.03064   0.02479  -0.0039   0.0259   1.0000
  14.000   1.3741   0.03206   0.02627  -0.0029   0.0256   1.0000
  14.250   1.3837   0.03342   0.02769  -0.0020   0.0253   1.0000
  14.500   1.3910   0.03501   0.02935  -0.0011   0.0251   1.0000
  14.750   1.3980   0.03668   0.03109  -0.0004   0.0247   1.0000
  15.000   1.4034   0.03856   0.03303   0.0003   0.0244   1.0000
  15.250   1.4083   0.04055   0.03509   0.0009   0.0240   1.0000
  15.500   1.4118   0.04275   0.03735   0.0013   0.0237   1.0000
  15.750   1.4141   0.04513   0.03979   0.0017   0.0234   1.0000
  16.000   1.4158   0.04765   0.04237   0.0018   0.0231   1.0000
  16.250   1.4162   0.05039   0.04517   0.0019   0.0227   1.0000
  16.500   1.4117   0.05373   0.04858   0.0018   0.0224   1.0000
  16.750   1.4034   0.05758   0.05253   0.0015   0.0222   1.0000
  17.000   1.3942   0.06162   0.05665   0.0011   0.0220   1.0000
  17.250   1.4011   0.06388   0.05899   0.0007   0.0217   1.0000
  17.500   1.4003   0.06704   0.06223   0.0002   0.0215   1.0000
  17.750   1.3987   0.07036   0.06563  -0.0004   0.0214   1.0000
  18.000   1.3979   0.07365   0.06901  -0.0011   0.0211   1.0000
  18.250   1.3941   0.07736   0.07280  -0.0020   0.0209   1.0000
  18.500   1.3911   0.08100   0.07652  -0.0029   0.0207   1.0000
  18.750   1.3874   0.08478   0.08038  -0.0039   0.0204   1.0000
  19.000   1.3839   0.08860   0.08428  -0.0051   0.0201   1.0000
  19.250   1.3794   0.09261   0.08836  -0.0063   0.0199   1.0000
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