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RAE(NPL) 5212 AIRFOIL (rae5212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE(NPL) 5212 AIRFOIL (rae5212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.32 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5212-il-1000000-n5.txt
Download as CSV file: xf-rae5212-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.9183   0.09547   0.09294  -0.0465   1.0000   0.0078
 -17.000  -0.9937   0.07630   0.07349  -0.0577   1.0000   0.0077
 -16.750  -1.0248   0.06677   0.06377  -0.0636   1.0000   0.0077
 -16.500  -1.0490   0.05933   0.05617  -0.0680   1.0000   0.0077
 -16.250  -1.0646   0.05395   0.05065  -0.0708   1.0000   0.0078
 -16.000  -1.0773   0.04940   0.04597  -0.0728   1.0000   0.0078
 -15.750  -1.0849   0.04576   0.04221  -0.0741   1.0000   0.0078
 -15.500  -1.0923   0.04238   0.03871  -0.0749   1.0000   0.0078
 -15.250  -1.0974   0.03943   0.03565  -0.0754   1.0000   0.0078
 -15.000  -1.0992   0.03699   0.03311  -0.0754   1.0000   0.0079
 -14.750  -1.0994   0.03485   0.03087  -0.0750   1.0000   0.0079
 -14.500  -1.1032   0.03254   0.02847  -0.0744   1.0000   0.0080
 -14.250  -1.1066   0.03046   0.02628  -0.0734   1.0000   0.0081
 -14.000  -1.1101   0.02858   0.02430  -0.0720   1.0000   0.0082
 -13.750  -1.1123   0.02707   0.02272  -0.0701   1.0000   0.0082
 -13.500  -1.1172   0.02581   0.02139  -0.0673   1.0000   0.0083
 -13.250  -1.1300   0.02486   0.02036  -0.0623   1.0000   0.0084
 -13.000  -1.1115   0.02384   0.01927  -0.0625   0.9988   0.0085
 -12.750  -1.0872   0.02285   0.01821  -0.0635   0.9972   0.0086
 -12.500  -1.0614   0.02198   0.01727  -0.0646   0.9956   0.0088
 -12.250  -1.0345   0.02116   0.01638  -0.0658   0.9943   0.0090
 -12.000  -1.0103   0.02042   0.01559  -0.0662   0.9924   0.0092
 -11.750  -0.9852   0.01975   0.01485  -0.0666   0.9905   0.0095
 -11.500  -0.9593   0.01903   0.01407  -0.0673   0.9886   0.0096
 -11.250  -0.9323   0.01834   0.01330  -0.0681   0.9871   0.0098
 -11.000  -0.9043   0.01768   0.01257  -0.0690   0.9859   0.0100
 -10.750  -0.8753   0.01705   0.01187  -0.0700   0.9848   0.0102
 -10.500  -0.8460   0.01638   0.01114  -0.0711   0.9839   0.0104
 -10.250  -0.8241   0.01575   0.01046  -0.0706   0.9809   0.0106
 -10.000  -0.7983   0.01519   0.00987  -0.0708   0.9785   0.0109
  -9.750  -0.7697   0.01474   0.00940  -0.0714   0.9767   0.0112
  -9.500  -0.7398   0.01427   0.00889  -0.0723   0.9753   0.0115
  -9.250  -0.7089   0.01381   0.00840  -0.0734   0.9741   0.0119
  -9.000  -0.6781   0.01339   0.00794  -0.0745   0.9729   0.0122
  -8.750  -0.6521   0.01299   0.00751  -0.0744   0.9701   0.0125
  -8.500  -0.6282   0.01263   0.00711  -0.0739   0.9656   0.0128
  -8.250  -0.6002   0.01221   0.00666  -0.0742   0.9624   0.0132
  -8.000  -0.5706   0.01181   0.00626  -0.0749   0.9599   0.0138
  -7.750  -0.5459   0.01151   0.00594  -0.0744   0.9548   0.0144
  -7.500  -0.5189   0.01121   0.00562  -0.0744   0.9500   0.0150
  -7.250  -0.4892   0.01089   0.00527  -0.0750   0.9463   0.0156
  -7.000  -0.4626   0.01061   0.00496  -0.0749   0.9405   0.0161
  -6.750  -0.4349   0.01027   0.00462  -0.0750   0.9338   0.0169
  -6.500  -0.4065   0.01000   0.00433  -0.0752   0.9269   0.0178
  -6.250  -0.3783   0.00977   0.00406  -0.0754   0.9180   0.0187
  -6.000  -0.3502   0.00955   0.00381  -0.0755   0.9094   0.0197
  -5.500  -0.2953   0.00911   0.00331  -0.0754   0.8910   0.0222
  -5.250  -0.2680   0.00895   0.00310  -0.0753   0.8824   0.0233
  -5.000  -0.2414   0.00876   0.00289  -0.0751   0.8733   0.0251
  -4.750  -0.2144   0.00861   0.00272  -0.0749   0.8654   0.0270
  -4.500  -0.1876   0.00847   0.00255  -0.0747   0.8570   0.0296
  -4.250  -0.1608   0.00833   0.00240  -0.0745   0.8493   0.0334
  -4.000  -0.1340   0.00818   0.00225  -0.0743   0.8415   0.0386
  -3.750  -0.1072   0.00804   0.00211  -0.0740   0.8341   0.0458
  -3.500  -0.0803   0.00789   0.00199  -0.0738   0.8266   0.0551
  -3.000  -0.0269   0.00754   0.00173  -0.0734   0.8124   0.0928
  -2.750  -0.0008   0.00729   0.00160  -0.0732   0.8051   0.1346
  -2.500   0.0252   0.00698   0.00147  -0.0729   0.7983   0.1881
  -2.250   0.0501   0.00651   0.00129  -0.0726   0.7910   0.2838
  -2.000   0.0748   0.00604   0.00114  -0.0722   0.7841   0.3864
  -1.750   0.0999   0.00567   0.00105  -0.0718   0.7752   0.4778
  -1.500   0.1263   0.00556   0.00106  -0.0715   0.7650   0.5330
  -1.250   0.1530   0.00557   0.00106  -0.0711   0.7502   0.5556
  -1.000   0.1788   0.00564   0.00107  -0.0705   0.7268   0.5715
  -0.750   0.2045   0.00572   0.00108  -0.0699   0.7031   0.5822
  -0.500   0.2311   0.00580   0.00108  -0.0695   0.6822   0.5884
  -0.250   0.2574   0.00589   0.00109  -0.0691   0.6601   0.5928
   0.000   0.2826   0.00604   0.00111  -0.0684   0.6259   0.5961
   0.250   0.3055   0.00634   0.00115  -0.0673   0.5633   0.5993
   0.500   0.3288   0.00667   0.00123  -0.0664   0.5043   0.6020
   0.750   0.3507   0.00710   0.00136  -0.0652   0.4282   0.6049
   1.000   0.3738   0.00748   0.00150  -0.0644   0.3663   0.6080
   1.250   0.3974   0.00783   0.00163  -0.0636   0.3095   0.6112
   1.500   0.4217   0.00814   0.00175  -0.0629   0.2646   0.6143
   1.750   0.4465   0.00843   0.00187  -0.0623   0.2267   0.6172
   2.000   0.4712   0.00870   0.00200  -0.0617   0.1922   0.6200
   2.250   0.4958   0.00897   0.00214  -0.0611   0.1603   0.6229
   2.500   0.5209   0.00921   0.00228  -0.0605   0.1348   0.6261
   2.750   0.5461   0.00944   0.00242  -0.0600   0.1156   0.6294
   3.000   0.5715   0.00966   0.00256  -0.0596   0.1004   0.6325
   3.250   0.5970   0.00987   0.00270  -0.0591   0.0875   0.6354
   3.500   0.6227   0.01003   0.00284  -0.0586   0.0809   0.6388
   3.750   0.6484   0.01021   0.00300  -0.0582   0.0754   0.6422
   4.000   0.6744   0.01035   0.00315  -0.0578   0.0732   0.6457
   4.250   0.7002   0.01052   0.00330  -0.0574   0.0702   0.6489
   4.500   0.7257   0.01071   0.00347  -0.0570   0.0680   0.6516
   4.750   0.7510   0.01089   0.00365  -0.0564   0.0657   0.6548
   5.000   0.7763   0.01106   0.00384  -0.0559   0.0640   0.6582
   5.250   0.8019   0.01122   0.00401  -0.0555   0.0632   0.6616
   5.500   0.8273   0.01138   0.00420  -0.0551   0.0621   0.6648
   6.000   0.8773   0.01175   0.00460  -0.0540   0.0599   0.6709
   6.250   0.9018   0.01195   0.00483  -0.0534   0.0587   0.6743
   6.500   0.9261   0.01217   0.00505  -0.0527   0.0574   0.6780
   6.750   0.9500   0.01242   0.00531  -0.0520   0.0560   0.6819
   7.000   0.9733   0.01270   0.00562  -0.0512   0.0545   0.6856
   7.250   0.9972   0.01291   0.00587  -0.0505   0.0540   0.6897
   7.500   1.0212   0.01310   0.00610  -0.0498   0.0534   0.6940
   7.750   1.0450   0.01331   0.00635  -0.0491   0.0526   0.6982
   8.000   1.0683   0.01353   0.00661  -0.0483   0.0517   0.7025
   8.250   1.0912   0.01376   0.00688  -0.0475   0.0507   0.7076
   8.500   1.1138   0.01401   0.00717  -0.0466   0.0497   0.7131
   8.750   1.1359   0.01428   0.00746  -0.0456   0.0487   0.7187
   9.000   1.1575   0.01456   0.00777  -0.0446   0.0475   0.7257
   9.500   1.1977   0.01514   0.00846  -0.0419   0.0455   0.7428
   9.750   1.2176   0.01536   0.00876  -0.0405   0.0448   0.7545
  10.000   1.2369   0.01559   0.00907  -0.0391   0.0439   0.7708
  10.250   1.2557   0.01582   0.00939  -0.0375   0.0426   0.7948
  10.500   1.2715   0.01595   0.00971  -0.0354   0.0413   0.8589
  10.750   1.3012   0.01620   0.01016  -0.0363   0.0398   1.0000
  11.000   1.3192   0.01660   0.01058  -0.0347   0.0389   1.0000
  11.250   1.3376   0.01697   0.01100  -0.0333   0.0383   1.0000
  11.500   1.3557   0.01735   0.01142  -0.0318   0.0376   1.0000
  11.750   1.3735   0.01776   0.01186  -0.0303   0.0367   1.0000
  12.000   1.3909   0.01820   0.01233  -0.0289   0.0358   1.0000
  12.250   1.4078   0.01867   0.01282  -0.0274   0.0348   1.0000
  12.500   1.4238   0.01919   0.01336  -0.0258   0.0337   1.0000
  12.750   1.4396   0.01973   0.01393  -0.0242   0.0328   1.0000
  13.000   1.4556   0.02024   0.01450  -0.0227   0.0320   1.0000
  13.250   1.4711   0.02080   0.01511  -0.0212   0.0310   1.0000
  13.500   1.4858   0.02141   0.01576  -0.0196   0.0300   1.0000
  13.750   1.4997   0.02209   0.01647  -0.0180   0.0288   1.0000
  14.000   1.5126   0.02285   0.01726  -0.0164   0.0278   1.0000
  14.250   1.5262   0.02356   0.01803  -0.0149   0.0266   1.0000
  14.500   1.5388   0.02436   0.01888  -0.0134   0.0256   1.0000
  14.750   1.5499   0.02528   0.01983  -0.0118   0.0239   1.0000
  15.000   1.5605   0.02625   0.02085  -0.0102   0.0229   1.0000
  15.250   1.5706   0.02729   0.02194  -0.0088   0.0214   1.0000
  15.500   1.5786   0.02851   0.02320  -0.0072   0.0199   1.0000
  15.750   1.5865   0.02977   0.02452  -0.0058   0.0188   1.0000
  16.000   1.5931   0.03118   0.02598  -0.0044   0.0176   1.0000
  16.250   1.5985   0.03271   0.02758  -0.0030   0.0167   1.0000
  16.500   1.6029   0.03438   0.02932  -0.0018   0.0159   1.0000
  16.750   1.6074   0.03610   0.03112  -0.0007   0.0154   1.0000
  17.000   1.6108   0.03796   0.03306   0.0003   0.0149   1.0000
  17.250   1.6118   0.04013   0.03531   0.0011   0.0143   1.0000
  17.500   1.6121   0.04246   0.03773   0.0018   0.0139   1.0000
  17.750   1.6105   0.04508   0.04045   0.0022   0.0135   1.0000
  18.000   1.6082   0.04788   0.04335   0.0024   0.0131   1.0000
  18.250   1.6057   0.05085   0.04643   0.0024   0.0129   1.0000
  18.500   1.6019   0.05412   0.04981   0.0020   0.0127   1.0000
  18.750   1.5962   0.05778   0.05358   0.0013   0.0125   1.0000
  19.000   1.5880   0.06196   0.05789   0.0002   0.0123   1.0000
  19.250   1.5772   0.06677   0.06282  -0.0015   0.0121   1.0000
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