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RAE 5215 AIRFOIL (rae5215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 5215 AIRFOIL (rae5215-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.05 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5215-il-1000000-n5.txt
Download as CSV file: xf-rae5215-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 5215 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -1.1147   0.06345   0.06084  -0.0312   1.0000   0.0065
 -14.750  -1.1542   0.05238   0.04951  -0.0396   1.0000   0.0064
 -14.500  -1.1739   0.04585   0.04278  -0.0441   1.0000   0.0064
 -14.250  -1.1853   0.04097   0.03773  -0.0471   1.0000   0.0064
 -14.000  -1.1914   0.03706   0.03365  -0.0493   1.0000   0.0064
 -13.750  -1.1941   0.03383   0.03026  -0.0510   1.0000   0.0064
 -13.500  -1.1928   0.03131   0.02758  -0.0519   1.0000   0.0065
 -13.250  -1.1828   0.02939   0.02550  -0.0520   1.0000   0.0065
 -13.000  -1.1695   0.02773   0.02370  -0.0520   1.0000   0.0065
 -12.750  -1.1536   0.02626   0.02209  -0.0519   1.0000   0.0066
 -12.500  -1.1359   0.02493   0.02064  -0.0518   1.0000   0.0066
 -12.250  -1.1167   0.02372   0.01931  -0.0517   1.0000   0.0067
 -12.000  -1.0963   0.02261   0.01808  -0.0516   1.0000   0.0067
 -11.750  -1.0750   0.02158   0.01695  -0.0515   1.0000   0.0068
 -11.500  -1.0528   0.02064   0.01590  -0.0513   1.0000   0.0069
 -11.250  -1.0300   0.01975   0.01492  -0.0512   1.0000   0.0069
 -11.000  -1.0066   0.01893   0.01401  -0.0511   1.0000   0.0070
 -10.750  -0.9827   0.01817   0.01316  -0.0510   1.0000   0.0071
 -10.500  -0.9584   0.01745   0.01236  -0.0509   1.0000   0.0072
 -10.250  -0.9337   0.01678   0.01162  -0.0508   1.0000   0.0073
 -10.000  -0.9088   0.01616   0.01093  -0.0507   1.0000   0.0074
  -9.750  -0.8836   0.01558   0.01029  -0.0505   1.0000   0.0076
  -9.500  -0.8584   0.01505   0.00970  -0.0504   1.0000   0.0077
  -9.250  -0.8334   0.01443   0.00904  -0.0502   1.0000   0.0079
  -9.000  -0.8083   0.01393   0.00850  -0.0499   1.0000   0.0082
  -8.750  -0.7834   0.01350   0.00805  -0.0496   1.0000   0.0085
  -8.500  -0.7526   0.01306   0.00758  -0.0505   0.9978   0.0089
  -8.250  -0.7212   0.01264   0.00713  -0.0515   0.9954   0.0092
  -8.000  -0.6901   0.01225   0.00670  -0.0524   0.9923   0.0096
  -7.750  -0.6590   0.01186   0.00629  -0.0532   0.9884   0.0100
  -7.500  -0.6272   0.01153   0.00596  -0.0542   0.9848   0.0105
  -7.250  -0.5969   0.01124   0.00566  -0.0549   0.9795   0.0111
  -7.000  -0.5661   0.01094   0.00534  -0.0556   0.9744   0.0117
  -6.750  -0.5364   0.01066   0.00503  -0.0560   0.9685   0.0122
  -6.500  -0.5072   0.01041   0.00478  -0.0563   0.9618   0.0128
  -6.250  -0.4788   0.01019   0.00455  -0.0564   0.9547   0.0135
  -6.000  -0.4509   0.00998   0.00430  -0.0564   0.9464   0.0143
  -5.750  -0.4231   0.00977   0.00407  -0.0563   0.9382   0.0149
  -5.500  -0.3955   0.00956   0.00384  -0.0562   0.9299   0.0156
  -5.250  -0.3675   0.00937   0.00364  -0.0562   0.9225   0.0163
  -5.000  -0.3395   0.00920   0.00343  -0.0561   0.9148   0.0171
  -4.750  -0.3113   0.00904   0.00324  -0.0561   0.9080   0.0176
  -4.500  -0.2830   0.00883   0.00303  -0.0561   0.9007   0.0185
  -4.250  -0.2548   0.00868   0.00284  -0.0561   0.8940   0.0192
  -4.000  -0.2260   0.00853   0.00268  -0.0562   0.8878   0.0202
  -3.750  -0.1974   0.00838   0.00252  -0.0563   0.8814   0.0211
  -3.500  -0.1688   0.00823   0.00236  -0.0564   0.8754   0.0227
  -3.250  -0.1398   0.00810   0.00223  -0.0565   0.8683   0.0241
  -3.000  -0.1115   0.00798   0.00207  -0.0564   0.8578   0.0260
  -2.750  -0.0827   0.00786   0.00194  -0.0565   0.8468   0.0281
  -2.500  -0.0540   0.00774   0.00182  -0.0565   0.8356   0.0325
  -2.250  -0.0251   0.00758   0.00171  -0.0567   0.8267   0.0468
  -2.000   0.0040   0.00743   0.00161  -0.0569   0.8194   0.0655
  -1.750   0.0327   0.00724   0.00149  -0.0570   0.8024   0.1011
  -1.500   0.0610   0.00705   0.00137  -0.0571   0.7710   0.1569
  -1.250   0.0895   0.00672   0.00122  -0.0574   0.7336   0.2576
  -1.000   0.1180   0.00633   0.00108  -0.0579   0.6821   0.3945
  -0.750   0.1455   0.00626   0.00108  -0.0581   0.5960   0.5116
  -0.500   0.1721   0.00670   0.00121  -0.0580   0.4731   0.5635
  -0.250   0.1991   0.00718   0.00135  -0.0580   0.3651   0.5876
   0.000   0.2266   0.00756   0.00147  -0.0580   0.2827   0.6050
   0.250   0.2545   0.00784   0.00156  -0.0580   0.2264   0.6117
   0.500   0.2825   0.00810   0.00163  -0.0580   0.1836   0.6159
   0.750   0.3107   0.00832   0.00170  -0.0580   0.1512   0.6197
   1.000   0.3392   0.00847   0.00178  -0.0580   0.1340   0.6235
   1.500   0.3961   0.00871   0.00194  -0.0581   0.1150   0.6316
   1.750   0.4245   0.00885   0.00203  -0.0581   0.1089   0.6356
   2.000   0.4531   0.00896   0.00211  -0.0581   0.1051   0.6391
   2.250   0.4815   0.00906   0.00221  -0.0581   0.1014   0.6430
   2.500   0.5099   0.00918   0.00232  -0.0581   0.0975   0.6467
   2.750   0.5382   0.00931   0.00243  -0.0581   0.0943   0.6506
   3.000   0.5665   0.00942   0.00253  -0.0581   0.0917   0.6542
   3.250   0.5947   0.00957   0.00265  -0.0580   0.0870   0.6572
   3.500   0.6228   0.00970   0.00277  -0.0580   0.0825   0.6608
   3.750   0.6508   0.00984   0.00290  -0.0580   0.0779   0.6646
   4.000   0.6787   0.01000   0.00304  -0.0579   0.0736   0.6684
   4.250   0.7067   0.01015   0.00318  -0.0579   0.0695   0.6718
   4.750   0.7621   0.01050   0.00350  -0.0577   0.0609   0.6792
   5.000   0.7896   0.01069   0.00368  -0.0576   0.0566   0.6833
   5.500   0.8443   0.01112   0.00408  -0.0573   0.0484   0.6910
   5.750   0.8714   0.01135   0.00431  -0.0572   0.0452   0.6949
   6.000   0.8985   0.01158   0.00454  -0.0570   0.0423   0.6997
   6.250   0.9255   0.01182   0.00479  -0.0568   0.0396   0.7048
   6.500   0.9523   0.01208   0.00505  -0.0566   0.0369   0.7095
   6.750   0.9790   0.01233   0.00532  -0.0564   0.0344   0.7144
   7.000   1.0055   0.01261   0.00561  -0.0562   0.0319   0.7201
   7.250   1.0319   0.01289   0.00591  -0.0559   0.0299   0.7259
   7.500   1.0581   0.01319   0.00623  -0.0556   0.0281   0.7327
   7.750   1.0842   0.01349   0.00657  -0.0553   0.0268   0.7410
   8.000   1.1102   0.01380   0.00691  -0.0550   0.0256   0.7497
   8.250   1.1359   0.01414   0.00729  -0.0547   0.0245   0.7600
   8.500   1.1614   0.01449   0.00769  -0.0543   0.0238   0.7714
   8.750   1.1869   0.01480   0.00808  -0.0539   0.0233   0.7855
   9.000   1.2121   0.01511   0.00848  -0.0535   0.0227   0.8050
   9.250   1.2365   0.01541   0.00891  -0.0530   0.0222   0.8399
   9.500   1.2563   0.01550   0.00928  -0.0512   0.0218   1.0000
   9.750   1.2809   0.01596   0.00976  -0.0508   0.0213   1.0000
  10.000   1.3050   0.01647   0.01030  -0.0503   0.0209   1.0000
  10.250   1.3290   0.01696   0.01083  -0.0498   0.0206   1.0000
  10.500   1.3531   0.01741   0.01133  -0.0492   0.0203   1.0000
  10.750   1.3769   0.01789   0.01184  -0.0487   0.0200   1.0000
  11.000   1.4004   0.01838   0.01239  -0.0481   0.0197   1.0000
  11.250   1.4234   0.01889   0.01295  -0.0475   0.0194   1.0000
  11.500   1.4460   0.01944   0.01355  -0.0468   0.0192   1.0000
  11.750   1.4681   0.02002   0.01418  -0.0460   0.0189   1.0000
  12.000   1.4896   0.02062   0.01483  -0.0452   0.0187   1.0000
  12.250   1.5105   0.02126   0.01553  -0.0443   0.0185   1.0000
  12.500   1.5306   0.02196   0.01628  -0.0434   0.0183   1.0000
  12.750   1.5497   0.02272   0.01711  -0.0423   0.0181   1.0000
  13.000   1.5672   0.02358   0.01803  -0.0410   0.0178   1.0000
  13.250   1.5839   0.02446   0.01899  -0.0396   0.0177   1.0000
  13.500   1.6011   0.02522   0.01983  -0.0383   0.0176   1.0000
  13.750   1.6172   0.02602   0.02073  -0.0368   0.0175   1.0000
  14.000   1.6316   0.02688   0.02167  -0.0352   0.0174   1.0000
  14.250   1.6430   0.02777   0.02265  -0.0331   0.0173   1.0000
  14.500   1.6516   0.02873   0.02370  -0.0306   0.0172   1.0000
  14.750   1.6591   0.02981   0.02488  -0.0282   0.0171   1.0000
  15.000   1.6657   0.03101   0.02618  -0.0260   0.0170   1.0000
  15.250   1.6712   0.03235   0.02762  -0.0239   0.0169   1.0000
  15.500   1.6755   0.03386   0.02923  -0.0220   0.0168   1.0000
  15.750   1.6789   0.03554   0.03102  -0.0202   0.0167   1.0000
  16.000   1.6804   0.03746   0.03306  -0.0187   0.0166   1.0000
  16.250   1.6807   0.03963   0.03534  -0.0174   0.0165   1.0000
  16.500   1.6793   0.04208   0.03791  -0.0165   0.0164   1.0000
  16.750   1.6761   0.04490   0.04085  -0.0159   0.0163   1.0000
  17.000   1.6715   0.04806   0.04414  -0.0158   0.0162   1.0000
  17.250   1.6638   0.05183   0.04804  -0.0162   0.0161   1.0000
  17.500   1.6520   0.05649   0.05284  -0.0175   0.0161   1.0000
  17.750   1.6301   0.06316   0.05970  -0.0204   0.0161   1.0000
  18.000   1.6024   0.07187   0.06861  -0.0254   0.0161   1.0000
  18.250   1.5387   0.08912   0.08619  -0.0364   0.0162   1.0000
  18.500   1.4133   0.11862   0.11607  -0.0533   0.0165   1.0000
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