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HQ 3.0/15 AIRFOIL (hq3015-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/15 AIRFOIL (hq3015-il)
Reynolds number: 500,000
Max Cl/Cd: 84 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3015-il-500000-n5.txt
Download as CSV file: xf-hq3015-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/15 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6994   0.10462   0.10151  -0.0540   1.0000   0.0096
 -16.500  -0.7504   0.09126   0.08798  -0.0611   1.0000   0.0095
 -16.250  -0.7954   0.07924   0.07579  -0.0679   1.0000   0.0093
 -16.000  -0.8296   0.06921   0.06557  -0.0739   1.0000   0.0093
 -15.750  -0.8564   0.06091   0.05709  -0.0791   1.0000   0.0092
 -15.500  -0.8762   0.05457   0.05059  -0.0829   1.0000   0.0092
 -15.250  -0.8899   0.04964   0.04553  -0.0855   1.0000   0.0092
 -15.000  -0.8995   0.04561   0.04137  -0.0874   1.0000   0.0093
 -14.750  -0.9077   0.04201   0.03766  -0.0887   1.0000   0.0094
 -14.500  -0.9125   0.03906   0.03459  -0.0894   1.0000   0.0094
 -14.250  -0.9161   0.03644   0.03187  -0.0897   1.0000   0.0095
 -14.000  -0.9190   0.03410   0.02944  -0.0896   1.0000   0.0096
 -13.750  -0.9210   0.03210   0.02735  -0.0889   1.0000   0.0097
 -13.500  -0.9232   0.03038   0.02554  -0.0877   1.0000   0.0099
 -13.250  -0.9135   0.02856   0.02362  -0.0885   0.9919   0.0100
 -13.000  -0.8927   0.02683   0.02176  -0.0910   0.9835   0.0102
 -12.750  -0.8712   0.02500   0.01982  -0.0939   0.9746   0.0105
 -12.500  -0.8460   0.02352   0.01823  -0.0966   0.9658   0.0109
 -12.250  -0.8201   0.02227   0.01687  -0.0988   0.9555   0.0112
 -12.000  -0.7969   0.02127   0.01576  -0.0998   0.9423   0.0117
 -11.750  -0.7754   0.02044   0.01482  -0.1000   0.9289   0.0122
 -11.500  -0.7552   0.01972   0.01397  -0.0997   0.9168   0.0127
 -11.250  -0.7372   0.01899   0.01316  -0.0989   0.9062   0.0135
 -11.000  -0.7190   0.01837   0.01244  -0.0979   0.8961   0.0144
 -10.750  -0.7002   0.01782   0.01181  -0.0969   0.8871   0.0153
 -10.500  -0.6804   0.01729   0.01121  -0.0960   0.8790   0.0165
 -10.250  -0.6599   0.01682   0.01070  -0.0952   0.8717   0.0182
 -10.000  -0.6383   0.01640   0.01021  -0.0945   0.8647   0.0199
  -9.750  -0.6161   0.01602   0.00978  -0.0938   0.8582   0.0219
  -9.500  -0.5930   0.01568   0.00936  -0.0933   0.8517   0.0238
  -9.250  -0.5700   0.01532   0.00894  -0.0927   0.8462   0.0255
  -9.000  -0.5463   0.01500   0.00859  -0.0922   0.8401   0.0273
  -8.750  -0.5221   0.01471   0.00821  -0.0917   0.8342   0.0289
  -8.500  -0.4983   0.01436   0.00781  -0.0913   0.8289   0.0303
  -8.250  -0.4740   0.01404   0.00747  -0.0909   0.8232   0.0319
  -8.000  -0.4490   0.01378   0.00716  -0.0905   0.8176   0.0338
  -7.750  -0.4237   0.01354   0.00684  -0.0902   0.8125   0.0353
  -7.500  -0.3990   0.01320   0.00648  -0.0898   0.8068   0.0371
  -7.250  -0.3736   0.01295   0.00621  -0.0895   0.8016   0.0394
  -7.000  -0.3477   0.01273   0.00594  -0.0893   0.7966   0.0415
  -6.750  -0.3219   0.01247   0.00565  -0.0890   0.7910   0.0439
  -6.500  -0.2963   0.01220   0.00536  -0.0888   0.7859   0.0466
  -6.250  -0.2702   0.01197   0.00509  -0.0885   0.7811   0.0491
  -6.000  -0.2438   0.01175   0.00483  -0.0884   0.7757   0.0512
  -5.750  -0.2177   0.01150   0.00454  -0.0881   0.7706   0.0543
  -5.500  -0.1913   0.01127   0.00430  -0.0879   0.7661   0.0582
  -5.250  -0.1644   0.01109   0.00408  -0.0878   0.7607   0.0618
  -5.000  -0.1379   0.01087   0.00386  -0.0876   0.7556   0.0671
  -4.750  -0.1109   0.01070   0.00365  -0.0875   0.7511   0.0730
  -4.500  -0.0840   0.01049   0.00347  -0.0874   0.7459   0.0809
  -4.250  -0.0570   0.01031   0.00329  -0.0873   0.7407   0.0907
  -3.750  -0.0032   0.00991   0.00296  -0.0872   0.7308   0.1228
  -3.500   0.0233   0.00965   0.00280  -0.0871   0.7253   0.1529
  -3.250   0.0497   0.00940   0.00264  -0.0869   0.7200   0.1928
  -3.000   0.0763   0.00911   0.00251  -0.0869   0.7141   0.2355
  -2.750   0.1025   0.00881   0.00235  -0.0868   0.7083   0.2872
  -2.500   0.1274   0.00831   0.00218  -0.0866   0.7033   0.3830
  -2.250   0.1539   0.00805   0.00213  -0.0864   0.6980   0.4553
  -2.000   0.1813   0.00796   0.00211  -0.0863   0.6928   0.4892
  -1.750   0.2092   0.00794   0.00208  -0.0863   0.6880   0.5103
  -1.500   0.2370   0.00788   0.00209  -0.0863   0.6828   0.5336
  -1.250   0.2648   0.00787   0.00210  -0.0862   0.6770   0.5577
  -1.000   0.2924   0.00788   0.00211  -0.0860   0.6707   0.5763
  -0.750   0.3202   0.00789   0.00212  -0.0859   0.6630   0.5873
  -0.500   0.3478   0.00792   0.00211  -0.0858   0.6555   0.5953
  -0.250   0.3756   0.00794   0.00212  -0.0858   0.6469   0.6027
   0.000   0.4032   0.00798   0.00212  -0.0857   0.6394   0.6099
   0.250   0.4309   0.00801   0.00215  -0.0856   0.6313   0.6183
   0.500   0.4584   0.00806   0.00218  -0.0854   0.6244   0.6269
   0.750   0.4861   0.00809   0.00222  -0.0854   0.6168   0.6351
   1.000   0.5135   0.00815   0.00225  -0.0852   0.6092   0.6413
   1.250   0.5410   0.00819   0.00229  -0.0851   0.6003   0.6467
   1.500   0.5681   0.00825   0.00233  -0.0850   0.5912   0.6520
   1.750   0.5949   0.00833   0.00237  -0.0847   0.5803   0.6569
   2.000   0.6211   0.00842   0.00243  -0.0844   0.5660   0.6618
   2.250   0.6469   0.00853   0.00250  -0.0840   0.5506   0.6674
   2.500   0.6728   0.00865   0.00257  -0.0836   0.5362   0.6730
   2.750   0.6982   0.00877   0.00268  -0.0832   0.5211   0.6784
   3.000   0.7232   0.00893   0.00278  -0.0826   0.5046   0.6842
   3.250   0.7477   0.00911   0.00290  -0.0820   0.4871   0.6897
   3.500   0.7717   0.00930   0.00305  -0.0813   0.4697   0.6956
   3.750   0.7954   0.00951   0.00320  -0.0806   0.4504   0.7020
   4.000   0.8183   0.00976   0.00338  -0.0797   0.4297   0.7078
   4.250   0.8408   0.01001   0.00357  -0.0788   0.4103   0.7142
   4.750   0.8847   0.01056   0.00401  -0.0768   0.3697   0.7275
   5.000   0.9057   0.01088   0.00424  -0.0757   0.3484   0.7346
   5.250   0.9260   0.01120   0.00450  -0.0744   0.3284   0.7413
   5.500   0.9468   0.01149   0.00476  -0.0732   0.3128   0.7491
   5.750   0.9669   0.01179   0.00502  -0.0720   0.2986   0.7567
   6.000   0.9868   0.01209   0.00530  -0.0706   0.2848   0.7650
   6.250   1.0066   0.01237   0.00557  -0.0693   0.2735   0.7729
   6.500   1.0248   0.01263   0.00585  -0.0676   0.2641   0.7823
   6.750   1.0420   0.01290   0.00612  -0.0658   0.2544   0.7919
   7.000   1.0595   0.01318   0.00643  -0.0640   0.2449   0.8027
   7.250   1.0755   0.01351   0.00677  -0.0620   0.2348   0.8148
   7.500   1.0916   0.01382   0.00711  -0.0601   0.2242   0.8291
   7.750   1.1074   0.01413   0.00746  -0.0581   0.2146   0.8474
   8.250   1.1514   0.01481   0.00830  -0.0571   0.1931   1.0000
   8.500   1.1683   0.01526   0.00873  -0.0556   0.1846   1.0000
   8.750   1.1835   0.01579   0.00923  -0.0539   0.1758   1.0000
   9.000   1.1987   0.01633   0.00975  -0.0523   0.1661   1.0000
   9.250   1.2141   0.01689   0.01029  -0.0508   0.1588   1.0000
   9.500   1.2269   0.01759   0.01094  -0.0490   0.1481   1.0000
   9.750   1.2432   0.01814   0.01150  -0.0477   0.1421   1.0000
  10.000   1.2563   0.01887   0.01220  -0.0461   0.1339   1.0000
  10.250   1.2708   0.01955   0.01288  -0.0446   0.1260   1.0000
  10.500   1.2838   0.02033   0.01364  -0.0431   0.1190   1.0000
  10.750   1.2972   0.02111   0.01442  -0.0417   0.1116   1.0000
  11.000   1.3092   0.02200   0.01528  -0.0403   0.1039   1.0000
  11.250   1.3204   0.02296   0.01623  -0.0388   0.0961   1.0000
  11.500   1.3313   0.02397   0.01722  -0.0374   0.0872   1.0000
  11.750   1.3416   0.02505   0.01828  -0.0360   0.0804   1.0000
  12.000   1.3522   0.02614   0.01937  -0.0347   0.0739   1.0000
  12.250   1.3619   0.02731   0.02055  -0.0334   0.0684   1.0000
  12.500   1.3713   0.02854   0.02178  -0.0321   0.0628   1.0000
  12.750   1.3800   0.02985   0.02310  -0.0309   0.0579   1.0000
  13.000   1.3877   0.03126   0.02453  -0.0298   0.0527   1.0000
  13.250   1.3956   0.03271   0.02599  -0.0287   0.0486   1.0000
  13.500   1.4035   0.03419   0.02751  -0.0277   0.0450   1.0000
  13.750   1.4089   0.03591   0.02924  -0.0267   0.0409   1.0000
  14.000   1.4160   0.03755   0.03092  -0.0258   0.0378   1.0000
  14.250   1.4199   0.03953   0.03290  -0.0250   0.0342   1.0000
  14.500   1.4256   0.04139   0.03483  -0.0243   0.0312   1.0000
  14.750   1.4286   0.04356   0.03702  -0.0237   0.0281   1.0000
  15.000   1.4342   0.04555   0.03907  -0.0232   0.0263   1.0000
  15.250   1.4389   0.04769   0.04128  -0.0228   0.0248   1.0000
  15.500   1.4396   0.05029   0.04392  -0.0225   0.0218   1.0000
  15.750   1.4428   0.05270   0.04640  -0.0223   0.0202   1.0000
  16.000   1.4422   0.05562   0.04937  -0.0223   0.0176   1.0000
  16.250   1.4416   0.05864   0.05245  -0.0224   0.0154   1.0000
  16.500   1.4372   0.06219   0.05605  -0.0227   0.0123   1.0000
  16.750   1.4339   0.06572   0.05966  -0.0232   0.0102   1.0000
  17.000   1.4222   0.07050   0.06448  -0.0241   0.0064   1.0000
  17.250   1.4155   0.07476   0.06884  -0.0251   0.0055   1.0000
  17.500   1.4101   0.07896   0.07314  -0.0262   0.0052   1.0000
  17.750   1.4017   0.08373   0.07802  -0.0276   0.0048   1.0000
  18.000   1.3951   0.08836   0.08276  -0.0292   0.0047   1.0000
  18.250   1.3850   0.09363   0.08814  -0.0311   0.0044   1.0000
  18.500   1.3791   0.09834   0.09297  -0.0330   0.0044   1.0000
  18.750   1.3703   0.10360   0.09836  -0.0351   0.0043   1.0000
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