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S9033 (7.5%) (s9033-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S9033 (7.5%) (s9033-il)
Reynolds number: 500,000
Max Cl/Cd: 58.94 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s9033-il-500000-n5.txt
Download as CSV file: xf-s9033-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S9033 (7.5%)                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0456   0.09498   0.09240   0.0140   1.0000   0.0071
 -14.500  -1.1127   0.07768   0.07488   0.0035   1.0000   0.0067
 -14.250  -1.1732   0.06130   0.05831  -0.0074   1.0000   0.0062
 -14.000  -1.2131   0.04846   0.04521  -0.0180   1.0000   0.0059
 -13.750  -1.2349   0.04160   0.03813  -0.0234   1.0000   0.0060
 -13.500  -1.2503   0.03776   0.03410  -0.0243   1.0000   0.0060
 -13.250  -1.2592   0.03534   0.03151  -0.0226   1.0000   0.0061
 -13.000  -1.2592   0.03335   0.02934  -0.0209   1.0000   0.0064
 -12.750  -1.2522   0.03157   0.02740  -0.0197   1.0000   0.0066
 -12.500  -1.2413   0.03001   0.02571  -0.0187   1.0000   0.0070
 -12.250  -1.2261   0.02885   0.02445  -0.0179   1.0000   0.0073
 -12.000  -1.2088   0.02784   0.02333  -0.0172   1.0000   0.0078
 -11.750  -1.1912   0.02681   0.02217  -0.0165   1.0000   0.0083
 -11.500  -1.1725   0.02582   0.02105  -0.0158   1.0000   0.0089
 -11.250  -1.1527   0.02494   0.02003  -0.0151   1.0000   0.0094
 -11.000  -1.1314   0.02422   0.01915  -0.0145   1.0000   0.0098
 -10.750  -1.1139   0.02288   0.01769  -0.0137   1.0000   0.0105
 -10.500  -1.0925   0.02212   0.01685  -0.0132   1.0000   0.0111
 -10.250  -1.0698   0.02153   0.01619  -0.0127   1.0000   0.0118
 -10.000  -1.0471   0.02087   0.01544  -0.0122   1.0000   0.0125
  -9.750  -1.0241   0.02023   0.01470  -0.0117   1.0000   0.0132
  -9.500  -1.0006   0.01965   0.01400  -0.0112   1.0000   0.0138
  -9.250  -0.9769   0.01908   0.01333  -0.0107   1.0000   0.0142
  -9.000  -0.9567   0.01776   0.01185  -0.0099   1.0000   0.0150
  -8.750  -0.9338   0.01695   0.01095  -0.0093   1.0000   0.0157
  -8.500  -0.9099   0.01632   0.01026  -0.0088   1.0000   0.0165
  -8.250  -0.8856   0.01575   0.00961  -0.0083   1.0000   0.0172
  -8.000  -0.8613   0.01515   0.00893  -0.0077   1.0000   0.0179
  -7.750  -0.8367   0.01458   0.00827  -0.0072   1.0000   0.0185
  -7.500  -0.8119   0.01405   0.00764  -0.0067   1.0000   0.0192
  -7.250  -0.7868   0.01358   0.00708  -0.0062   1.0000   0.0198
  -7.000  -0.7619   0.01303   0.00646  -0.0057   1.0000   0.0208
  -6.750  -0.7369   0.01250   0.00591  -0.0052   1.0000   0.0230
  -6.500  -0.7115   0.01209   0.00549  -0.0047   1.0000   0.0254
  -6.250  -0.6857   0.01174   0.00508  -0.0043   1.0000   0.0276
  -6.000  -0.6603   0.01132   0.00467  -0.0038   1.0000   0.0323
  -5.750  -0.6344   0.01101   0.00434  -0.0033   1.0000   0.0370
  -5.500  -0.6088   0.01067   0.00402  -0.0029   1.0000   0.0429
  -5.250  -0.5828   0.01041   0.00374  -0.0024   1.0000   0.0481
  -5.000  -0.5570   0.01012   0.00345  -0.0019   1.0000   0.0543
  -4.750  -0.5312   0.00987   0.00320  -0.0015   1.0000   0.0606
  -4.500  -0.5055   0.00959   0.00297  -0.0010   1.0000   0.0699
  -4.250  -0.4799   0.00932   0.00276  -0.0005   1.0000   0.0814
  -4.000  -0.4545   0.00905   0.00256   0.0001   1.0000   0.0965
  -3.750  -0.4290   0.00880   0.00236   0.0006   1.0000   0.1121
  -3.250  -0.3783   0.00835   0.00204   0.0018   1.0000   0.1439
  -3.000  -0.3530   0.00814   0.00190   0.0024   1.0000   0.1603
  -2.750  -0.3277   0.00795   0.00177   0.0030   1.0000   0.1780
  -2.500  -0.2982   0.00775   0.00166   0.0027   0.9974   0.1992
  -2.250  -0.2615   0.00752   0.00156   0.0007   0.9879   0.2308
  -2.000  -0.2252   0.00730   0.00146  -0.0010   0.9728   0.2621
  -1.750  -0.1890   0.00706   0.00138  -0.0028   0.9497   0.3024
  -1.500  -0.1518   0.00684   0.00129  -0.0046   0.9059   0.3507
  -1.250  -0.1259   0.00681   0.00119  -0.0037   0.8399   0.3864
  -1.000  -0.1017   0.00685   0.00112  -0.0026   0.7791   0.4176
  -0.750  -0.0767   0.00687   0.00108  -0.0018   0.7274   0.4553
  -0.500  -0.0512   0.00687   0.00104  -0.0012   0.6817   0.4964
  -0.250  -0.0256   0.00683   0.00103  -0.0006   0.6390   0.5431
   0.000   0.0000   0.00679   0.00102   0.0000   0.5956   0.5954
   0.250   0.0255   0.00683   0.00103   0.0006   0.5433   0.6392
   0.500   0.0512   0.00687   0.00105   0.0012   0.4962   0.6820
   0.750   0.0767   0.00687   0.00108   0.0018   0.4555   0.7274
   1.000   0.1017   0.00685   0.00112   0.0026   0.4178   0.7791
   1.250   0.1259   0.00681   0.00119   0.0037   0.3864   0.8401
   1.500   0.1518   0.00684   0.00129   0.0046   0.3506   0.9062
   1.750   0.1890   0.00706   0.00138   0.0028   0.3023   0.9496
   2.000   0.2253   0.00730   0.00147   0.0010   0.2623   0.9729
   2.250   0.2614   0.00752   0.00156  -0.0007   0.2312   0.9878
   2.500   0.2981   0.00775   0.00166  -0.0027   0.1993   0.9973
   2.750   0.3278   0.00795   0.00177  -0.0030   0.1781   1.0000
   3.000   0.3531   0.00814   0.00190  -0.0024   0.1603   1.0000
   3.250   0.3784   0.00835   0.00204  -0.0018   0.1438   1.0000
   3.500   0.4038   0.00857   0.00219  -0.0012   0.1281   1.0000
   3.750   0.4292   0.00880   0.00236  -0.0007   0.1120   1.0000
   4.000   0.4546   0.00905   0.00256  -0.0001   0.0964   1.0000
   4.250   0.4800   0.00932   0.00276   0.0004   0.0815   1.0000
   4.500   0.5056   0.00959   0.00297   0.0009   0.0701   1.0000
   4.750   0.5312   0.00987   0.00320   0.0014   0.0606   1.0000
   5.000   0.5571   0.01012   0.00345   0.0019   0.0543   1.0000
   5.250   0.5829   0.01041   0.00374   0.0024   0.0481   1.0000
   5.500   0.6088   0.01067   0.00402   0.0029   0.0428   1.0000
   5.750   0.6344   0.01101   0.00434   0.0033   0.0370   1.0000
   6.000   0.6603   0.01132   0.00467   0.0038   0.0322   1.0000
   6.250   0.6857   0.01174   0.00508   0.0043   0.0276   1.0000
   6.500   0.7114   0.01209   0.00549   0.0047   0.0254   1.0000
   6.750   0.7368   0.01250   0.00591   0.0052   0.0231   1.0000
   7.000   0.7618   0.01302   0.00646   0.0057   0.0209   1.0000
   7.250   0.7867   0.01357   0.00708   0.0062   0.0198   1.0000
   7.500   0.8118   0.01405   0.00764   0.0067   0.0192   1.0000
   7.750   0.8366   0.01458   0.00827   0.0072   0.0185   1.0000
   8.000   0.8611   0.01515   0.00893   0.0078   0.0179   1.0000
   8.250   0.8854   0.01575   0.00961   0.0083   0.0172   1.0000
   8.500   0.9097   0.01633   0.01026   0.0088   0.0165   1.0000
   8.750   0.9336   0.01694   0.01094   0.0093   0.0157   1.0000
   9.000   0.9565   0.01776   0.01185   0.0099   0.0150   1.0000
   9.250   0.9766   0.01908   0.01334   0.0108   0.0141   1.0000
   9.500   1.0004   0.01964   0.01400   0.0113   0.0138   1.0000
   9.750   1.0239   0.02022   0.01469   0.0117   0.0132   1.0000
  10.000   1.0467   0.02088   0.01545   0.0123   0.0125   1.0000
  10.250   1.0694   0.02152   0.01619   0.0128   0.0118   1.0000
  10.500   1.0919   0.02214   0.01688   0.0133   0.0111   1.0000
  10.750   1.1135   0.02287   0.01768   0.0138   0.0105   1.0000
  11.000   1.1311   0.02419   0.01912   0.0146   0.0098   1.0000
  11.250   1.1515   0.02504   0.02013   0.0153   0.0095   1.0000
  11.500   1.1719   0.02583   0.02105   0.0159   0.0089   1.0000
  11.750   1.1907   0.02677   0.02213   0.0166   0.0083   1.0000
  12.000   1.2082   0.02783   0.02332   0.0173   0.0078   1.0000
  12.250   1.2252   0.02886   0.02446   0.0181   0.0074   1.0000
  12.500   1.2407   0.02999   0.02569   0.0189   0.0070   1.0000
  12.750   1.2517   0.03153   0.02735   0.0198   0.0066   1.0000
  13.000   1.2588   0.03331   0.02930   0.0210   0.0063   1.0000
  13.250   1.2594   0.03524   0.03141   0.0227   0.0061   1.0000
  13.500   1.2515   0.03758   0.03392   0.0244   0.0059   1.0000
  13.750   1.2344   0.04158   0.03811   0.0235   0.0060   1.0000
  14.000   1.2129   0.04841   0.04516   0.0181   0.0059   1.0000
  14.250   1.1718   0.06157   0.05857   0.0071   0.0062   1.0000
  14.750   1.0205   0.10009   0.09758  -0.0172   0.0075   1.0000
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