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GOE 693 AIRFOIL (goe693-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 693 AIRFOIL (goe693-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.54 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe693-il-1000000.txt
Download as CSV file: xf-goe693-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 693 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  -1.1162   0.03654   0.03357  -0.0903   1.0000   0.0168
 -15.000  -1.1298   0.03310   0.02998  -0.0907   1.0000   0.0170
 -14.750  -1.1318   0.03134   0.02813  -0.0888   1.0000   0.0172
 -14.500  -1.1232   0.03010   0.02683  -0.0876   1.0000   0.0175
 -14.250  -1.1136   0.02908   0.02575  -0.0860   1.0000   0.0178
 -14.000  -1.1057   0.02818   0.02477  -0.0838   1.0000   0.0181
 -13.750  -1.0989   0.02733   0.02386  -0.0812   1.0000   0.0185
 -13.500  -1.0919   0.02654   0.02298  -0.0784   1.0000   0.0188
 -13.250  -1.0835   0.02578   0.02212  -0.0758   1.0000   0.0191
 -13.000  -1.0639   0.02499   0.02123  -0.0752   0.9994   0.0195
 -12.750  -1.0347   0.02431   0.02044  -0.0764   0.9982   0.0198
 -12.500  -1.0126   0.02238   0.01836  -0.0774   0.9964   0.0206
 -12.250  -0.9823   0.02173   0.01769  -0.0787   0.9952   0.0211
 -12.000  -0.9507   0.02128   0.01720  -0.0801   0.9943   0.0217
 -11.750  -0.9201   0.02075   0.01662  -0.0812   0.9930   0.0223
 -11.500  -0.8911   0.02017   0.01595  -0.0821   0.9910   0.0229
 -11.250  -0.8607   0.01960   0.01529  -0.0831   0.9892   0.0234
 -11.000  -0.8289   0.01917   0.01477  -0.0843   0.9877   0.0238
 -10.750  -0.8016   0.01767   0.01313  -0.0854   0.9861   0.0247
 -10.500  -0.7695   0.01710   0.01254  -0.0868   0.9848   0.0254
 -10.250  -0.7372   0.01667   0.01208  -0.0881   0.9833   0.0261
 -10.000  -0.7094   0.01623   0.01158  -0.0884   0.9798   0.0267
  -9.750  -0.6816   0.01576   0.01104  -0.0886   0.9759   0.0274
  -9.500  -0.6533   0.01537   0.01058  -0.0889   0.9722   0.0280
  -9.250  -0.6259   0.01510   0.01025  -0.0888   0.9680   0.0284
  -9.000  -0.6038   0.01428   0.00932  -0.0880   0.9617   0.0291
  -8.750  -0.5804   0.01357   0.00856  -0.0873   0.9565   0.0300
  -8.500  -0.5557   0.01319   0.00814  -0.0867   0.9503   0.0307
  -8.250  -0.5306   0.01287   0.00779  -0.0861   0.9439   0.0314
  -8.000  -0.5052   0.01253   0.00739  -0.0856   0.9375   0.0322
  -7.750  -0.4796   0.01218   0.00698  -0.0851   0.9297   0.0328
  -7.500  -0.4536   0.01190   0.00663  -0.0847   0.9224   0.0335
  -7.250  -0.4269   0.01166   0.00634  -0.0844   0.9135   0.0340
  -7.000  -0.4018   0.01107   0.00566  -0.0839   0.9043   0.0350
  -6.750  -0.3760   0.01066   0.00518  -0.0834   0.8939   0.0361
  -6.500  -0.3492   0.01037   0.00485  -0.0832   0.8818   0.0371
  -6.250  -0.3221   0.01014   0.00455  -0.0830   0.8693   0.0381
  -6.000  -0.2948   0.00995   0.00428  -0.0828   0.8567   0.0393
  -5.750  -0.2674   0.00979   0.00403  -0.0826   0.8439   0.0402
  -5.500  -0.2404   0.00950   0.00366  -0.0824   0.8310   0.0418
  -5.250  -0.2130   0.00926   0.00338  -0.0822   0.8183   0.0440
  -5.000  -0.1852   0.00910   0.00316  -0.0822   0.8068   0.0461
  -4.750  -0.1572   0.00899   0.00298  -0.0821   0.7963   0.0481
  -4.500  -0.1297   0.00876   0.00273  -0.0820   0.7854   0.0536
  -4.250  -0.1017   0.00860   0.00255  -0.0820   0.7749   0.0600
  -4.000  -0.0738   0.00846   0.00241  -0.0820   0.7650   0.0693
  -3.750  -0.0455   0.00835   0.00231  -0.0821   0.7559   0.0794
  -3.500  -0.0171   0.00828   0.00225  -0.0821   0.7482   0.0879
  -3.250   0.0114   0.00822   0.00216  -0.0822   0.7401   0.0942
  -3.000   0.0399   0.00817   0.00210  -0.0823   0.7327   0.1001
  -2.750   0.0687   0.00816   0.00205  -0.0824   0.7253   0.1034
  -2.500   0.0970   0.00806   0.00195  -0.0825   0.7181   0.1100
  -2.250   0.1256   0.00800   0.00188  -0.0826   0.7096   0.1146
  -2.000   0.1542   0.00799   0.00182  -0.0827   0.7013   0.1176
  -1.750   0.1826   0.00791   0.00173  -0.0828   0.6929   0.1241
  -1.500   0.2111   0.00786   0.00168  -0.0829   0.6858   0.1303
  -1.250   0.2399   0.00780   0.00162  -0.0830   0.6789   0.1385
  -1.000   0.2683   0.00775   0.00158  -0.0831   0.6729   0.1489
  -0.750   0.2969   0.00763   0.00154  -0.0833   0.6675   0.1699
  -0.500   0.3253   0.00748   0.00151  -0.0834   0.6617   0.2082
  -0.250   0.3533   0.00734   0.00150  -0.0835   0.6560   0.2601
   0.000   0.3815   0.00711   0.00149  -0.0837   0.6503   0.3298
   0.250   0.4089   0.00683   0.00149  -0.0838   0.6439   0.4345
   0.500   0.4355   0.00643   0.00152  -0.0837   0.6375   0.5823
   0.750   0.4608   0.00601   0.00156  -0.0832   0.6293   0.7400
   1.000   0.4827   0.00566   0.00163  -0.0817   0.6217   0.8816
   1.250   0.5128   0.00561   0.00170  -0.0817   0.6135   0.9674
   1.500   0.5518   0.00569   0.00174  -0.0841   0.6052   0.9867
   1.750   0.5912   0.00578   0.00178  -0.0867   0.5954   0.9948
   2.000   0.6320   0.00588   0.00182  -0.0895   0.5820   0.9993
   2.250   0.6605   0.00597   0.00185  -0.0897   0.5686   1.0000
   2.500   0.6861   0.00607   0.00189  -0.0892   0.5550   1.0000
   2.750   0.7113   0.00619   0.00193  -0.0887   0.5369   1.0000
   3.000   0.7360   0.00637   0.00200  -0.0880   0.5141   1.0000
   3.250   0.7602   0.00658   0.00209  -0.0873   0.4858   1.0000
   3.500   0.7836   0.00688   0.00222  -0.0865   0.4514   1.0000
   3.750   0.8070   0.00719   0.00238  -0.0857   0.4186   1.0000
   4.000   0.8308   0.00750   0.00255  -0.0850   0.3911   1.0000
   4.250   0.8555   0.00775   0.00270  -0.0844   0.3713   1.0000
   4.500   0.8806   0.00797   0.00286  -0.0839   0.3560   1.0000
   4.750   0.9059   0.00819   0.00302  -0.0835   0.3430   1.0000
   5.000   0.9314   0.00841   0.00318  -0.0831   0.3306   1.0000
   5.250   0.9569   0.00862   0.00334  -0.0827   0.3180   1.0000
   5.500   0.9825   0.00882   0.00351  -0.0824   0.3072   1.0000
   5.750   1.0079   0.00905   0.00369  -0.0820   0.2961   1.0000
   6.000   1.0330   0.00929   0.00388  -0.0816   0.2819   1.0000
   6.250   1.0569   0.00962   0.00410  -0.0810   0.2557   1.0000
   6.500   1.0761   0.01030   0.00449  -0.0797   0.2022   1.0000
   6.750   1.0971   0.01083   0.00486  -0.0786   0.1783   1.0000
   7.000   1.1204   0.01118   0.00516  -0.0779   0.1690   1.0000
   7.250   1.1443   0.01146   0.00544  -0.0773   0.1621   1.0000
   7.500   1.1684   0.01173   0.00571  -0.0768   0.1569   1.0000
   7.750   1.1913   0.01208   0.00602  -0.0760   0.1502   1.0000
   8.000   1.2160   0.01228   0.00626  -0.0756   0.1454   1.0000
   8.250   1.2387   0.01261   0.00655  -0.0748   0.1376   1.0000
   8.500   1.2621   0.01288   0.00683  -0.0742   0.1298   1.0000
   8.750   1.2822   0.01336   0.00718  -0.0730   0.1094   1.0000
   9.000   1.2986   0.01405   0.00771  -0.0713   0.0874   1.0000
   9.250   1.3172   0.01456   0.00818  -0.0699   0.0787   1.0000
   9.500   1.3354   0.01505   0.00866  -0.0684   0.0707   1.0000
   9.750   1.3481   0.01571   0.00924  -0.0660   0.0547   1.0000
  10.000   1.3515   0.01689   0.01022  -0.0621   0.0303   1.0000
  10.250   1.3636   0.01767   0.01098  -0.0597   0.0247   1.0000
  10.500   1.3762   0.01843   0.01175  -0.0576   0.0217   1.0000
  10.750   1.3910   0.01910   0.01245  -0.0558   0.0202   1.0000
  11.000   1.4049   0.01983   0.01322  -0.0540   0.0189   1.0000
  11.250   1.4159   0.02077   0.01419  -0.0519   0.0175   1.0000
  11.500   1.4298   0.02155   0.01502  -0.0503   0.0168   1.0000
  11.750   1.4434   0.02236   0.01588  -0.0487   0.0161   1.0000
  12.000   1.4558   0.02328   0.01684  -0.0471   0.0155   1.0000
  12.250   1.4664   0.02436   0.01796  -0.0454   0.0148   1.0000
  12.500   1.4728   0.02579   0.01947  -0.0434   0.0142   1.0000
  12.750   1.4819   0.02706   0.02081  -0.0418   0.0138   1.0000
  13.000   1.4926   0.02824   0.02205  -0.0405   0.0135   1.0000
  13.250   1.5021   0.02957   0.02345  -0.0392   0.0131   1.0000
  13.500   1.5106   0.03101   0.02495  -0.0379   0.0128   1.0000
  13.750   1.5184   0.03255   0.02655  -0.0367   0.0125   1.0000
  14.000   1.5252   0.03423   0.02830  -0.0356   0.0121   1.0000
  14.250   1.5296   0.03618   0.03031  -0.0345   0.0118   1.0000
  14.500   1.5289   0.03865   0.03287  -0.0333   0.0115   1.0000
  14.750   1.5210   0.04195   0.03628  -0.0320   0.0111   1.0000
  15.000   1.5276   0.04388   0.03828  -0.0314   0.0110   1.0000
  15.250   1.5310   0.04617   0.04066  -0.0309   0.0109   1.0000
  15.500   1.5332   0.04866   0.04324  -0.0304   0.0107   1.0000
  15.750   1.5338   0.05140   0.04607  -0.0300   0.0105   1.0000
  16.000   1.5334   0.05433   0.04909  -0.0298   0.0103   1.0000
  16.250   1.5320   0.05745   0.05230  -0.0297   0.0102   1.0000
  16.500   1.5296   0.06077   0.05571  -0.0297   0.0100   1.0000
  16.750   1.5262   0.06431   0.05934  -0.0300   0.0099   1.0000
  17.000   1.5220   0.06807   0.06319  -0.0304   0.0097   1.0000
  17.250   1.5163   0.07210   0.06731  -0.0309   0.0096   1.0000
  17.500   1.5095   0.07637   0.07168  -0.0317   0.0095   1.0000
  17.750   1.5018   0.08088   0.07629  -0.0327   0.0094   1.0000
  18.000   1.4921   0.08581   0.08132  -0.0339   0.0093   1.0000
  18.250   1.4815   0.09093   0.08653  -0.0353   0.0092   1.0000
  18.500   1.4693   0.09640   0.09211  -0.0370   0.0091   1.0000
  18.750   1.4561   0.10211   0.09792  -0.0388   0.0090   1.0000
  19.000   1.4420   0.10803   0.10395  -0.0409   0.0090   1.0000
  19.250   1.4275   0.11403   0.11005  -0.0431   0.0089   1.0000
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