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USA-35B AIRFOIL (usa35b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: USA-35B AIRFOIL (usa35b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.1 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-usa35b-il-1000000-n5.txt
Download as CSV file: xf-usa35b-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: USA-35B 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.4664   0.15126   0.14940  -0.0086   1.0000   0.0131
 -15.500  -0.4600   0.14803   0.14617  -0.0100   1.0000   0.0134
 -14.000  -0.8629   0.03452   0.03188  -0.0835   0.9996   0.0206
 -13.750  -0.8468   0.03088   0.02794  -0.0871   0.9942   0.0208
 -13.500  -0.8266   0.02855   0.02538  -0.0890   0.9879   0.0209
 -13.250  -0.8035   0.02658   0.02321  -0.0907   0.9828   0.0210
 -13.000  -0.7819   0.02485   0.02129  -0.0915   0.9754   0.0211
 -12.750  -0.7622   0.02270   0.01891  -0.0922   0.9671   0.0213
 -12.500  -0.7393   0.02149   0.01757  -0.0924   0.9583   0.0215
 -12.250  -0.7166   0.02058   0.01654  -0.0922   0.9482   0.0216
 -12.000  -0.6932   0.01980   0.01566  -0.0919   0.9392   0.0217
 -11.750  -0.6694   0.01910   0.01486  -0.0916   0.9303   0.0219
 -11.500  -0.6451   0.01844   0.01411  -0.0913   0.9217   0.0220
 -11.250  -0.6207   0.01782   0.01337  -0.0910   0.9121   0.0221
 -11.000  -0.5957   0.01722   0.01267  -0.0908   0.9030   0.0223
 -10.750  -0.5705   0.01667   0.01203  -0.0905   0.8940   0.0225
 -10.500  -0.5446   0.01618   0.01144  -0.0903   0.8850   0.0227
 -10.250  -0.5189   0.01569   0.01084  -0.0901   0.8755   0.0229
 -10.000  -0.4930   0.01515   0.01019  -0.0899   0.8650   0.0231
  -9.750  -0.4669   0.01463   0.00955  -0.0897   0.8547   0.0233
  -9.500  -0.4407   0.01413   0.00894  -0.0895   0.8438   0.0234
  -9.250  -0.4140   0.01367   0.00838  -0.0893   0.8336   0.0236
  -9.000  -0.3873   0.01323   0.00783  -0.0891   0.8230   0.0238
  -8.750  -0.3605   0.01284   0.00733  -0.0890   0.8108   0.0240
  -8.500  -0.3334   0.01247   0.00687  -0.0888   0.7977   0.0241
  -8.250  -0.3063   0.01214   0.00643  -0.0887   0.7830   0.0243
  -8.000  -0.2791   0.01185   0.00603  -0.0885   0.7670   0.0244
  -7.750  -0.2518   0.01158   0.00566  -0.0884   0.7496   0.0246
  -7.500  -0.2245   0.01135   0.00532  -0.0882   0.7299   0.0247
  -7.000  -0.1704   0.01076   0.00449  -0.0878   0.6860   0.0252
  -6.750  -0.1431   0.01053   0.00415  -0.0877   0.6656   0.0255
  -6.500  -0.1155   0.01034   0.00389  -0.0876   0.6488   0.0258
  -6.250  -0.0876   0.01019   0.00368  -0.0876   0.6361   0.0261
  -6.000  -0.0595   0.01005   0.00348  -0.0875   0.6252   0.0265
  -5.750  -0.0313   0.00990   0.00328  -0.0875   0.6159   0.0269
  -5.250   0.0253   0.00962   0.00290  -0.0875   0.5979   0.0275
  -5.000   0.0535   0.00951   0.00273  -0.0875   0.5882   0.0279
  -4.750   0.0819   0.00940   0.00258  -0.0875   0.5781   0.0282
  -4.500   0.1102   0.00931   0.00243  -0.0875   0.5685   0.0286
  -4.250   0.1387   0.00922   0.00230  -0.0875   0.5597   0.0288
  -4.000   0.1671   0.00912   0.00216  -0.0875   0.5531   0.0293
  -3.750   0.1958   0.00899   0.00202  -0.0875   0.5473   0.0300
  -3.500   0.2243   0.00890   0.00192  -0.0875   0.5415   0.0308
  -3.250   0.2529   0.00884   0.00184  -0.0876   0.5363   0.0316
  -3.000   0.2817   0.00877   0.00176  -0.0876   0.5310   0.0325
  -2.750   0.3103   0.00872   0.00170  -0.0877   0.5251   0.0335
  -2.500   0.3389   0.00868   0.00164  -0.0877   0.5199   0.0354
  -2.250   0.3677   0.00861   0.00159  -0.0877   0.5155   0.0379
  -2.000   0.3963   0.00856   0.00155  -0.0878   0.5100   0.0427
  -1.750   0.4247   0.00850   0.00153  -0.0878   0.5040   0.0577
  -1.500   0.4534   0.00843   0.00152  -0.0879   0.4990   0.0747
  -1.250   0.4820   0.00839   0.00151  -0.0879   0.4936   0.0881
  -1.000   0.5105   0.00836   0.00151  -0.0879   0.4881   0.1057
  -0.750   0.5389   0.00822   0.00153  -0.0880   0.4828   0.1605
  -0.500   0.5672   0.00812   0.00156  -0.0881   0.4755   0.2134
  -0.250   0.5954   0.00805   0.00159  -0.0882   0.4670   0.2620
   0.000   0.6232   0.00784   0.00164  -0.0883   0.4569   0.3780
   0.250   0.6506   0.00763   0.00172  -0.0883   0.4433   0.5100
   0.500   0.6765   0.00728   0.00183  -0.0881   0.4255   0.7008
   0.750   0.6952   0.00687   0.00197  -0.0858   0.4092   0.9195
   1.000   0.7305   0.00698   0.00203  -0.0872   0.3887   1.0000
   1.250   0.7574   0.00719   0.00213  -0.0870   0.3690   1.0000
   1.500   0.7844   0.00739   0.00224  -0.0868   0.3523   1.0000
   1.750   0.8114   0.00759   0.00235  -0.0866   0.3385   1.0000
   2.000   0.8386   0.00778   0.00247  -0.0864   0.3270   1.0000
   2.250   0.8660   0.00793   0.00258  -0.0863   0.3181   1.0000
   2.500   0.8931   0.00812   0.00272  -0.0861   0.3089   1.0000
   2.750   0.9206   0.00827   0.00284  -0.0860   0.3011   1.0000
   3.000   0.9476   0.00847   0.00298  -0.0858   0.2926   1.0000
   3.250   0.9749   0.00862   0.00311  -0.0857   0.2848   1.0000
   3.500   1.0014   0.00886   0.00328  -0.0854   0.2722   1.0000
   3.750   1.0274   0.00913   0.00347  -0.0851   0.2559   1.0000
   4.000   1.0532   0.00942   0.00367  -0.0848   0.2387   1.0000
   4.250   1.0787   0.00974   0.00389  -0.0844   0.2206   1.0000
   4.750   1.1276   0.01054   0.00445  -0.0834   0.1790   1.0000
   5.000   1.1521   0.01091   0.00475  -0.0828   0.1640   1.0000
   5.250   1.1770   0.01124   0.00502  -0.0824   0.1538   1.0000
   5.500   1.2018   0.01156   0.00529  -0.0819   0.1453   1.0000
   5.750   1.2270   0.01183   0.00555  -0.0815   0.1390   1.0000
   6.000   1.2515   0.01215   0.00584  -0.0810   0.1321   1.0000
   6.250   1.2760   0.01246   0.00613  -0.0805   0.1250   1.0000
   6.500   1.2996   0.01284   0.00645  -0.0798   0.1168   1.0000
   6.750   1.3239   0.01314   0.00675  -0.0793   0.1116   1.0000
   7.000   1.3467   0.01354   0.00710  -0.0785   0.1037   1.0000
   7.250   1.3691   0.01396   0.00748  -0.0777   0.0931   1.0000
   7.750   1.4008   0.01572   0.00893  -0.0743   0.0471   1.0000
   8.000   1.4211   0.01620   0.00941  -0.0732   0.0430   1.0000
   8.250   1.4403   0.01673   0.00993  -0.0719   0.0395   1.0000
   8.500   1.4601   0.01717   0.01040  -0.0707   0.0375   1.0000
   8.750   1.4777   0.01766   0.01090  -0.0692   0.0356   1.0000
   9.000   1.4931   0.01821   0.01146  -0.0673   0.0337   1.0000
   9.250   1.5096   0.01872   0.01200  -0.0656   0.0326   1.0000
   9.500   1.5255   0.01927   0.01258  -0.0640   0.0315   1.0000
   9.750   1.5403   0.01990   0.01323  -0.0622   0.0303   1.0000
  10.000   1.5541   0.02061   0.01396  -0.0605   0.0291   1.0000
  10.250   1.5678   0.02135   0.01474  -0.0588   0.0282   1.0000
  10.500   1.5822   0.02207   0.01551  -0.0573   0.0275   1.0000
  10.750   1.5956   0.02288   0.01636  -0.0558   0.0266   1.0000
  11.000   1.6079   0.02379   0.01731  -0.0542   0.0257   1.0000
  11.250   1.6191   0.02483   0.01838  -0.0527   0.0248   1.0000
  11.500   1.6289   0.02600   0.01960  -0.0512   0.0239   1.0000
  11.750   1.6406   0.02708   0.02074  -0.0500   0.0234   1.0000
  12.000   1.6511   0.02829   0.02201  -0.0488   0.0228   1.0000
  12.250   1.6605   0.02964   0.02340  -0.0476   0.0220   1.0000
  12.500   1.6687   0.03114   0.02496  -0.0465   0.0212   1.0000
  12.750   1.6753   0.03284   0.02670  -0.0454   0.0205   1.0000
  13.000   1.6817   0.03461   0.02854  -0.0445   0.0198   1.0000
  13.250   1.6882   0.03644   0.03044  -0.0437   0.0193   1.0000
  13.500   1.6934   0.03846   0.03252  -0.0431   0.0187   1.0000
  13.750   1.6973   0.04067   0.03480  -0.0425   0.0181   1.0000
  14.000   1.6995   0.04311   0.03730  -0.0421   0.0175   1.0000
  14.250   1.7005   0.04578   0.04003  -0.0417   0.0169   1.0000
  14.500   1.7015   0.04850   0.04284  -0.0415   0.0165   1.0000
  14.750   1.7017   0.05137   0.04579  -0.0414   0.0161   1.0000
  15.000   1.7007   0.05444   0.04894  -0.0415   0.0156   1.0000
  15.250   1.6984   0.05772   0.05230  -0.0416   0.0151   1.0000
  15.500   1.6947   0.06122   0.05587  -0.0418   0.0147   1.0000
  15.750   1.6893   0.06496   0.05970  -0.0422   0.0143   1.0000
  16.000   1.6827   0.06894   0.06376  -0.0427   0.0139   1.0000
  16.250   1.6766   0.07293   0.06784  -0.0433   0.0136   1.0000
  16.500   1.6697   0.07707   0.07208  -0.0440   0.0134   1.0000
  16.750   1.6617   0.08142   0.07653  -0.0448   0.0131   1.0000
  17.000   1.6528   0.08598   0.08118  -0.0458   0.0129   1.0000
  17.250   1.6431   0.09074   0.08604  -0.0470   0.0126   1.0000
  17.500   1.6324   0.09569   0.09109  -0.0483   0.0124   1.0000
  17.750   1.6210   0.10082   0.09631  -0.0498   0.0122   1.0000
  18.000   1.6090   0.10613   0.10172  -0.0515   0.0120   1.0000
  18.250   1.5965   0.11160   0.10729  -0.0534   0.0118   1.0000
  18.500   1.5833   0.11721   0.11300  -0.0554   0.0116   1.0000
  18.750   1.5698   0.12296   0.11884  -0.0577   0.0114   1.0000
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