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RAE(NPL) 5212 AIRFOIL (rae5212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAE(NPL) 5212 AIRFOIL (rae5212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.45 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rae5212-il-1000000.txt
Download as CSV file: xf-rae5212-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE(NPL) 5212 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8784   0.06195   0.05937  -0.0655   1.0000   0.0109
 -14.500  -0.9111   0.05398   0.05119  -0.0701   1.0000   0.0108
 -14.250  -0.9252   0.04945   0.04652  -0.0720   1.0000   0.0108
 -14.000  -0.9448   0.04468   0.04158  -0.0734   1.0000   0.0109
 -13.750  -0.9525   0.04167   0.03847  -0.0738   1.0000   0.0109
 -13.500  -0.9586   0.03906   0.03577  -0.0736   1.0000   0.0110
 -13.250  -0.9697   0.03619   0.03276  -0.0728   1.0000   0.0110
 -13.000  -0.9759   0.03411   0.03058  -0.0716   1.0000   0.0111
 -12.750  -0.9832   0.03225   0.02861  -0.0697   1.0000   0.0112
 -12.500  -0.9912   0.03092   0.02720  -0.0668   1.0000   0.0113
 -12.250  -1.0096   0.02976   0.02594  -0.0614   1.0000   0.0113
 -12.000  -1.0138   0.02859   0.02467  -0.0576   1.0000   0.0114
 -11.750  -1.0111   0.02758   0.02357  -0.0547   1.0000   0.0116
 -11.500  -1.0068   0.02645   0.02233  -0.0519   1.0000   0.0117
 -11.250  -0.9807   0.02505   0.02079  -0.0534   0.9984   0.0120
 -11.000  -0.9539   0.02376   0.01935  -0.0548   0.9967   0.0123
 -10.750  -0.9257   0.02263   0.01808  -0.0563   0.9952   0.0125
 -10.500  -0.8952   0.02177   0.01710  -0.0579   0.9941   0.0128
 -10.250  -0.8685   0.02099   0.01621  -0.0585   0.9920   0.0130
 -10.000  -0.8456   0.01904   0.01411  -0.0592   0.9895   0.0134
  -9.750  -0.8153   0.01839   0.01344  -0.0605   0.9878   0.0139
  -9.500  -0.7841   0.01771   0.01271  -0.0618   0.9864   0.0142
  -9.250  -0.7524   0.01704   0.01199  -0.0633   0.9853   0.0146
  -9.000  -0.7198   0.01646   0.01135  -0.0648   0.9844   0.0151
  -8.750  -0.6906   0.01584   0.01066  -0.0656   0.9825   0.0155
  -8.500  -0.6635   0.01531   0.01007  -0.0658   0.9791   0.0158
  -8.250  -0.6342   0.01442   0.00911  -0.0667   0.9769   0.0163
  -8.000  -0.6028   0.01370   0.00838  -0.0680   0.9753   0.0170
  -7.750  -0.5695   0.01325   0.00792  -0.0695   0.9742   0.0175
  -7.500  -0.5353   0.01285   0.00750  -0.0711   0.9733   0.0184
  -7.250  -0.5006   0.01247   0.00709  -0.0728   0.9726   0.0191
  -7.000  -0.4756   0.01192   0.00650  -0.0725   0.9682   0.0198
  -6.750  -0.4459   0.01135   0.00592  -0.0732   0.9651   0.0208
  -6.500  -0.4139   0.01096   0.00553  -0.0743   0.9628   0.0219
  -6.250  -0.3811   0.01061   0.00516  -0.0755   0.9609   0.0230
  -6.000  -0.3517   0.01016   0.00468  -0.0760   0.9578   0.0244
  -5.750  -0.3271   0.00983   0.00436  -0.0754   0.9515   0.0259
  -5.500  -0.2969   0.00954   0.00406  -0.0759   0.9476   0.0276
  -5.250  -0.2685   0.00918   0.00367  -0.0760   0.9426   0.0295
  -5.000  -0.2421   0.00891   0.00341  -0.0757   0.9352   0.0318
  -4.750  -0.2115   0.00865   0.00312  -0.0763   0.9303   0.0345
  -4.500  -0.1858   0.00840   0.00288  -0.0758   0.9211   0.0387
  -4.250  -0.1571   0.00814   0.00263  -0.0760   0.9139   0.0456
  -4.000  -0.1299   0.00791   0.00242  -0.0759   0.9050   0.0565
  -3.750  -0.1027   0.00763   0.00221  -0.0758   0.8968   0.0781
  -3.500  -0.0769   0.00723   0.00199  -0.0755   0.8879   0.1329
  -3.250  -0.0525   0.00669   0.00176  -0.0751   0.8793   0.2254
  -3.000  -0.0304   0.00583   0.00146  -0.0745   0.8706   0.3934
  -2.750  -0.0055   0.00544   0.00136  -0.0741   0.8626   0.4857
  -2.500   0.0217   0.00535   0.00134  -0.0739   0.8550   0.5276
  -2.250   0.0496   0.00534   0.00133  -0.0737   0.8479   0.5489
  -2.000   0.0774   0.00533   0.00132  -0.0736   0.8403   0.5626
  -1.750   0.1052   0.00535   0.00132  -0.0734   0.8324   0.5768
  -1.500   0.1327   0.00537   0.00133  -0.0732   0.8231   0.5910
  -1.250   0.1601   0.00543   0.00135  -0.0728   0.8116   0.6029
  -1.000   0.1866   0.00548   0.00137  -0.0723   0.7962   0.6130
  -0.750   0.2135   0.00555   0.00137  -0.0719   0.7815   0.6199
  -0.500   0.2405   0.00558   0.00137  -0.0716   0.7686   0.6249
  -0.250   0.2676   0.00564   0.00137  -0.0713   0.7553   0.6286
   0.000   0.2946   0.00569   0.00136  -0.0709   0.7397   0.6318
   0.250   0.3214   0.00577   0.00136  -0.0706   0.7234   0.6344
   0.500   0.3485   0.00579   0.00136  -0.0703   0.7097   0.6377
   0.750   0.3751   0.00585   0.00138  -0.0699   0.6925   0.6406
   1.000   0.4015   0.00593   0.00140  -0.0694   0.6741   0.6436
   1.250   0.4279   0.00603   0.00143  -0.0690   0.6528   0.6467
   1.500   0.4533   0.00618   0.00147  -0.0684   0.6232   0.6496
   1.750   0.4768   0.00641   0.00152  -0.0674   0.5756   0.6524
   2.000   0.4978   0.00679   0.00165  -0.0661   0.5051   0.6557
   2.250   0.5178   0.00733   0.00184  -0.0646   0.4209   0.6587
   2.500   0.5388   0.00785   0.00204  -0.0633   0.3457   0.6619
   2.750   0.5603   0.00834   0.00224  -0.0622   0.2782   0.6651
   3.000   0.5824   0.00881   0.00244  -0.0611   0.2210   0.6680
   3.250   0.6044   0.00923   0.00265  -0.0601   0.1678   0.6716
   3.500   0.6270   0.00963   0.00287  -0.0591   0.1269   0.6751
   3.750   0.6508   0.00996   0.00308  -0.0584   0.1032   0.6788
   4.000   0.6755   0.01022   0.00326  -0.0578   0.0913   0.6824
   4.250   0.7008   0.01041   0.00343  -0.0573   0.0852   0.6860
   4.500   0.7259   0.01059   0.00362  -0.0567   0.0817   0.6898
   4.750   0.7506   0.01082   0.00384  -0.0561   0.0780   0.6936
   5.000   0.7754   0.01106   0.00408  -0.0555   0.0752   0.6975
   5.250   0.8008   0.01122   0.00427  -0.0550   0.0740   0.7014
   5.500   0.8257   0.01138   0.00448  -0.0545   0.0725   0.7057
   5.750   0.8503   0.01159   0.00471  -0.0539   0.0709   0.7101
   6.000   0.8746   0.01182   0.00495  -0.0532   0.0693   0.7144
   6.250   0.8982   0.01209   0.00523  -0.0524   0.0675   0.7190
   6.500   0.9202   0.01245   0.00564  -0.0514   0.0653   0.7241
   6.750   0.9425   0.01280   0.00603  -0.0504   0.0640   0.7298
   7.000   0.9666   0.01298   0.00627  -0.0497   0.0634   0.7359
   7.250   0.9903   0.01318   0.00652  -0.0489   0.0625   0.7431
   7.500   1.0138   0.01339   0.00677  -0.0482   0.0613   0.7506
   7.750   1.0365   0.01362   0.00707  -0.0473   0.0602   0.7600
   8.000   1.0587   0.01387   0.00737  -0.0463   0.0591   0.7711
   8.250   1.0802   0.01413   0.00770  -0.0452   0.0579   0.7863
   8.500   1.0997   0.01445   0.00811  -0.0437   0.0566   0.8110
   8.750   1.1113   0.01475   0.00877  -0.0406   0.0549   0.9182
   9.000   1.1441   0.01522   0.00933  -0.0422   0.0539   1.0000
   9.250   1.1661   0.01542   0.00955  -0.0412   0.0533   1.0000
   9.500   1.1873   0.01564   0.00980  -0.0400   0.0524   1.0000
   9.750   1.2071   0.01595   0.01013  -0.0387   0.0515   1.0000
  10.000   1.2273   0.01621   0.01041  -0.0374   0.0504   1.0000
  10.250   1.2478   0.01645   0.01065  -0.0362   0.0493   1.0000
  10.500   1.2672   0.01676   0.01095  -0.0349   0.0481   1.0000
  10.750   1.2818   0.01739   0.01160  -0.0329   0.0468   1.0000
  11.000   1.2964   0.01802   0.01228  -0.0309   0.0458   1.0000
  11.250   1.3160   0.01833   0.01263  -0.0297   0.0454   1.0000
  11.500   1.3351   0.01865   0.01301  -0.0284   0.0447   1.0000
  11.750   1.3536   0.01902   0.01341  -0.0271   0.0439   1.0000
  12.000   1.3719   0.01940   0.01382  -0.0258   0.0431   1.0000
  12.250   1.3898   0.01979   0.01424  -0.0245   0.0422   1.0000
  12.500   1.4076   0.02020   0.01466  -0.0232   0.0413   1.0000
  12.750   1.4229   0.02075   0.01523  -0.0216   0.0401   1.0000
  13.000   1.4334   0.02164   0.01617  -0.0195   0.0389   1.0000
  13.250   1.4519   0.02202   0.01660  -0.0184   0.0383   1.0000
  13.500   1.4686   0.02252   0.01716  -0.0172   0.0376   1.0000
  13.750   1.4852   0.02302   0.01770  -0.0160   0.0366   1.0000
  14.000   1.5006   0.02361   0.01833  -0.0147   0.0356   1.0000
  14.250   1.5151   0.02428   0.01899  -0.0134   0.0341   1.0000
  14.500   1.5236   0.02536   0.02012  -0.0115   0.0329   1.0000
  14.750   1.5398   0.02595   0.02078  -0.0105   0.0321   1.0000
  15.000   1.5537   0.02670   0.02160  -0.0093   0.0310   1.0000
  15.250   1.5661   0.02758   0.02249  -0.0081   0.0296   1.0000
  15.500   1.5740   0.02881   0.02376  -0.0066   0.0280   1.0000
  15.750   1.5857   0.02979   0.02481  -0.0054   0.0269   1.0000
  16.000   1.5960   0.03091   0.02598  -0.0043   0.0255   1.0000
  16.250   1.6024   0.03236   0.02747  -0.0030   0.0242   1.0000
  16.500   1.6073   0.03399   0.02916  -0.0017   0.0230   1.0000
  16.750   1.6135   0.03555   0.03080  -0.0007   0.0219   1.0000
  17.000   1.6171   0.03740   0.03272   0.0003   0.0211   1.0000
  17.250   1.6173   0.03963   0.03501   0.0012   0.0200   1.0000
  17.500   1.6156   0.04215   0.03762   0.0019   0.0194   1.0000
  17.750   1.6168   0.04447   0.04005   0.0023   0.0188   1.0000
  18.000   1.6158   0.04712   0.04280   0.0026   0.0183   1.0000
  18.250   1.6121   0.05021   0.04597   0.0026   0.0177   1.0000
  18.500   1.6063   0.05369   0.04956   0.0022   0.0174   1.0000
  18.750   1.5973   0.05777   0.05375   0.0014   0.0170   1.0000
  19.000   1.5846   0.06262   0.05872   0.0000   0.0167   1.0000
  19.250   1.5671   0.06848   0.06471  -0.0023   0.0163   1.0000
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