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DF102 (df102-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DF102 (df102-il)
Reynolds number: 500,000
Max Cl/Cd: 82.09 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-df102-il-500000.txt
Download as CSV file: xf-df102-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DF102                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.5550   0.07820   0.07584  -0.0416   1.0000   0.0168
 -11.000  -0.5622   0.07277   0.07041  -0.0439   1.0000   0.0155
 -10.750  -0.5971   0.06059   0.05815  -0.0535   1.0000   0.0150
 -10.500  -0.6270   0.05069   0.04807  -0.0641   1.0000   0.0148
 -10.250  -0.7444   0.03843   0.03495  -0.0615   1.0000   0.0129
 -10.000  -0.7574   0.03614   0.03242  -0.0572   1.0000   0.0128
  -9.750  -0.7680   0.03412   0.03025  -0.0527   1.0000   0.0129
  -9.500  -0.7753   0.03218   0.02811  -0.0483   1.0000   0.0130
  -9.250  -0.7654   0.03004   0.02578  -0.0470   0.9987   0.0132
  -9.000  -0.7390   0.02770   0.02319  -0.0488   0.9957   0.0134
  -8.750  -0.7095   0.02615   0.02149  -0.0504   0.9931   0.0139
  -8.500  -0.6834   0.02403   0.01910  -0.0513   0.9893   0.0142
  -8.250  -0.6531   0.02251   0.01737  -0.0526   0.9864   0.0148
  -8.000  -0.6206   0.02119   0.01584  -0.0542   0.9842   0.0155
  -7.750  -0.5872   0.02054   0.01494  -0.0555   0.9817   0.0162
  -7.500  -0.5627   0.01812   0.01238  -0.0557   0.9773   0.0170
  -7.250  -0.5306   0.01706   0.01128  -0.0570   0.9745   0.0178
  -7.000  -0.4963   0.01617   0.01032  -0.0586   0.9725   0.0188
  -6.750  -0.4605   0.01535   0.00942  -0.0604   0.9710   0.0200
  -6.500  -0.4297   0.01458   0.00855  -0.0611   0.9674   0.0211
  -6.250  -0.4023   0.01359   0.00755  -0.0614   0.9623   0.0231
  -6.000  -0.3698   0.01306   0.00697  -0.0624   0.9589   0.0251
  -5.750  -0.3369   0.01252   0.00637  -0.0634   0.9559   0.0268
  -5.500  -0.3145   0.01179   0.00559  -0.0623   0.9482   0.0295
  -5.250  -0.2853   0.01140   0.00516  -0.0625   0.9433   0.0329
  -5.000  -0.2602   0.01092   0.00464  -0.0617   0.9368   0.0373
  -4.750  -0.2343   0.01052   0.00422  -0.0611   0.9301   0.0442
  -4.500  -0.2114   0.00970   0.00370  -0.0602   0.9235   0.1022
  -4.250  -0.1876   0.00921   0.00346  -0.0594   0.9158   0.1628
  -4.000  -0.1614   0.00897   0.00329  -0.0589   0.9097   0.1941
  -3.750  -0.1358   0.00879   0.00315  -0.0583   0.9015   0.2170
  -3.500  -0.1090   0.00863   0.00300  -0.0578   0.8950   0.2361
  -3.250  -0.0832   0.00848   0.00288  -0.0572   0.8864   0.2548
  -3.000  -0.0565   0.00833   0.00275  -0.0568   0.8791   0.2768
  -2.750  -0.0304   0.00817   0.00264  -0.0562   0.8702   0.2991
  -2.500  -0.0039   0.00802   0.00253  -0.0558   0.8619   0.3248
  -2.250   0.0224   0.00785   0.00241  -0.0553   0.8529   0.3473
  -1.750   0.0748   0.00753   0.00219  -0.0542   0.8322   0.4017
  -1.500   0.1002   0.00733   0.00207  -0.0535   0.8190   0.4410
  -1.250   0.1252   0.00711   0.00198  -0.0527   0.8050   0.4932
  -1.000   0.1497   0.00688   0.00191  -0.0518   0.7909   0.5585
  -0.750   0.1736   0.00665   0.00187  -0.0508   0.7763   0.6282
  -0.500   0.1970   0.00642   0.00184  -0.0496   0.7617   0.7006
  -0.250   0.2194   0.00617   0.00184  -0.0481   0.7469   0.7856
   0.000   0.2440   0.00604   0.00192  -0.0467   0.7315   0.8733
   0.250   0.2751   0.00611   0.00198  -0.0468   0.7146   0.9249
   0.500   0.3112   0.00621   0.00202  -0.0482   0.6988   0.9497
   0.750   0.3484   0.00633   0.00206  -0.0499   0.6816   0.9655
   1.000   0.3899   0.00645   0.00209  -0.0526   0.6638   0.9749
   1.250   0.4298   0.00659   0.00212  -0.0550   0.6451   0.9836
   1.500   0.4732   0.00671   0.00214  -0.0583   0.6239   0.9899
   1.750   0.5145   0.00683   0.00215  -0.0611   0.6002   0.9960
   2.000   0.5520   0.00697   0.00216  -0.0633   0.5735   1.0000
   2.250   0.5739   0.00711   0.00220  -0.0620   0.5490   1.0000
   2.500   0.5956   0.00728   0.00225  -0.0608   0.5210   1.0000
   2.750   0.6165   0.00751   0.00232  -0.0594   0.4849   1.0000
   3.000   0.6363   0.00782   0.00243  -0.0578   0.4383   1.0000
   3.250   0.6545   0.00827   0.00259  -0.0560   0.3787   1.0000
   3.500   0.6717   0.00882   0.00282  -0.0541   0.3138   1.0000
   3.750   0.6901   0.00932   0.00306  -0.0524   0.2684   1.0000
   4.000   0.7103   0.00968   0.00330  -0.0510   0.2433   1.0000
   4.250   0.7313   0.01000   0.00352  -0.0497   0.2260   1.0000
   4.500   0.7527   0.01029   0.00374  -0.0485   0.2126   1.0000
   4.750   0.7745   0.01057   0.00396  -0.0473   0.2011   1.0000
   5.000   0.7960   0.01087   0.00420  -0.0461   0.1912   1.0000
   5.250   0.8185   0.01110   0.00442  -0.0450   0.1830   1.0000
   5.500   0.8402   0.01140   0.00468  -0.0439   0.1755   1.0000
   5.750   0.8627   0.01164   0.00492  -0.0429   0.1686   1.0000
   6.000   0.8841   0.01199   0.00522  -0.0417   0.1620   1.0000
   6.250   0.9073   0.01221   0.00546  -0.0408   0.1565   1.0000
   6.500   0.9287   0.01256   0.00577  -0.0396   0.1505   1.0000
   6.750   0.9513   0.01284   0.00608  -0.0387   0.1455   1.0000
   7.000   0.9739   0.01311   0.00636  -0.0378   0.1406   1.0000
   7.250   0.9943   0.01356   0.00676  -0.0365   0.1356   1.0000
   7.500   1.0168   0.01385   0.00710  -0.0355   0.1322   1.0000
   7.750   1.0393   0.01414   0.00744  -0.0346   0.1287   1.0000
   8.000   1.0605   0.01451   0.00781  -0.0335   0.1251   1.0000
   8.250   1.0790   0.01510   0.00837  -0.0320   0.1209   1.0000
   8.500   1.1017   0.01535   0.00870  -0.0312   0.1186   1.0000
   8.750   1.1233   0.01567   0.00908  -0.0302   0.1158   1.0000
   9.000   1.1440   0.01605   0.00950  -0.0290   0.1132   1.0000
   9.250   1.1631   0.01654   0.00999  -0.0277   0.1105   1.0000
   9.500   1.1803   0.01720   0.01066  -0.0261   0.1073   1.0000
   9.750   1.2024   0.01736   0.01091  -0.0252   0.1045   1.0000
  10.000   1.2228   0.01761   0.01123  -0.0241   0.1012   1.0000
  10.250   1.2399   0.01799   0.01160  -0.0224   0.0978   1.0000
  10.500   1.2542   0.01857   0.01219  -0.0204   0.0942   1.0000
  10.750   1.2751   0.01869   0.01241  -0.0193   0.0909   1.0000
  11.000   1.2931   0.01900   0.01276  -0.0179   0.0873   1.0000
  11.250   1.3071   0.01957   0.01333  -0.0160   0.0837   1.0000
  11.500   1.3239   0.02002   0.01385  -0.0146   0.0811   1.0000
  11.750   1.3427   0.02034   0.01426  -0.0134   0.0777   1.0000
  12.000   1.3588   0.02082   0.01477  -0.0120   0.0740   1.0000
  12.250   1.3725   0.02147   0.01544  -0.0104   0.0702   1.0000
  12.500   1.3908   0.02187   0.01591  -0.0093   0.0647   1.0000
  12.750   1.4047   0.02255   0.01660  -0.0078   0.0575   1.0000
  13.000   1.4138   0.02361   0.01757  -0.0060   0.0429   1.0000
  13.250   1.4097   0.02568   0.01947  -0.0031   0.0254   1.0000
  13.500   1.4087   0.02758   0.02139  -0.0007   0.0192   1.0000
  13.750   1.4065   0.02967   0.02353   0.0014   0.0157   1.0000
  14.000   1.4085   0.03148   0.02545   0.0031   0.0142   1.0000
  14.250   1.4062   0.03375   0.02782   0.0046   0.0130   1.0000
  14.500   1.4015   0.03637   0.03057   0.0059   0.0120   1.0000
  14.750   1.4008   0.03875   0.03308   0.0066   0.0116   1.0000
  15.000   1.3968   0.04160   0.03607   0.0071   0.0109   1.0000
  15.250   1.3921   0.04469   0.03929   0.0073   0.0105   1.0000
  15.500   1.3835   0.04842   0.04314   0.0069   0.0101   1.0000
  15.750   1.3698   0.05305   0.04792   0.0059   0.0098   1.0000
  16.000   1.3541   0.05829   0.05331   0.0043   0.0096   1.0000
  16.250   1.3405   0.06361   0.05878   0.0023   0.0096   1.0000
  16.500   1.3206   0.07026   0.06560  -0.0006   0.0095   1.0000
  16.750   1.2995   0.07756   0.07307  -0.0041   0.0095   1.0000
  17.000   1.2779   0.08534   0.08101  -0.0081   0.0095   1.0000
  17.250   1.2542   0.09387   0.08971  -0.0125   0.0095   1.0000
  17.500   1.2311   0.10258   0.09859  -0.0170   0.0096   1.0000
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