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HQ 1.5/10 AIRFOIL (hq1510-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.5/10 AIRFOIL (hq1510-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.01 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1510-il-1000000-n5.txt
Download as CSV file: xf-hq1510-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.5/10 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.9003   0.04939   0.04723  -0.0489   1.0000   0.0022
 -12.750  -0.9164   0.04321   0.04089  -0.0537   1.0000   0.0022
 -12.500  -0.9476   0.03690   0.03433  -0.0569   1.0000   0.0022
 -12.250  -0.9597   0.03400   0.03128  -0.0564   1.0000   0.0022
 -12.000  -0.9700   0.03169   0.02880  -0.0538   1.0000   0.0022
 -11.750  -0.9701   0.02936   0.02626  -0.0522   1.0000   0.0022
 -11.500  -0.9645   0.02731   0.02399  -0.0508   1.0000   0.0022
 -11.250  -0.9577   0.02513   0.02156  -0.0493   1.0000   0.0023
 -11.000  -0.9469   0.02331   0.01953  -0.0479   1.0000   0.0023
 -10.750  -0.9365   0.02132   0.01728  -0.0464   1.0000   0.0024
 -10.500  -0.9201   0.02012   0.01596  -0.0452   1.0000   0.0026
 -10.250  -0.9025   0.01911   0.01481  -0.0441   1.0000   0.0027
 -10.000  -0.8833   0.01833   0.01396  -0.0430   1.0000   0.0028
  -9.750  -0.8601   0.01753   0.01305  -0.0428   0.9987   0.0029
  -9.500  -0.8312   0.01681   0.01225  -0.0437   0.9936   0.0031
  -9.250  -0.8018   0.01603   0.01137  -0.0447   0.9891   0.0032
  -9.000  -0.7706   0.01529   0.01051  -0.0459   0.9848   0.0034
  -8.750  -0.7406   0.01457   0.00969  -0.0469   0.9785   0.0036
  -8.500  -0.7089   0.01396   0.00899  -0.0482   0.9722   0.0038
  -8.250  -0.6789   0.01338   0.00833  -0.0490   0.9630   0.0040
  -8.000  -0.6494   0.01290   0.00776  -0.0497   0.9520   0.0041
  -7.750  -0.6230   0.01226   0.00701  -0.0497   0.9375   0.0044
  -7.500  -0.5979   0.01173   0.00637  -0.0493   0.9220   0.0048
  -7.250  -0.5726   0.01137   0.00592  -0.0489   0.9086   0.0052
  -7.000  -0.5472   0.01105   0.00553  -0.0485   0.8971   0.0057
  -6.750  -0.5216   0.01076   0.00515  -0.0481   0.8864   0.0061
  -6.500  -0.4955   0.01051   0.00483  -0.0479   0.8762   0.0066
  -6.250  -0.4696   0.01019   0.00444  -0.0476   0.8671   0.0071
  -6.000  -0.4438   0.00984   0.00401  -0.0472   0.8587   0.0081
  -5.750  -0.4173   0.00957   0.00368  -0.0470   0.8505   0.0090
  -5.500  -0.3907   0.00934   0.00338  -0.0468   0.8431   0.0101
  -5.250  -0.3640   0.00908   0.00310  -0.0466   0.8352   0.0131
  -5.000  -0.3373   0.00881   0.00285  -0.0465   0.8282   0.0193
  -4.750  -0.3102   0.00863   0.00264  -0.0463   0.8204   0.0244
  -4.500  -0.2831   0.00843   0.00245  -0.0462   0.8134   0.0305
  -4.250  -0.2557   0.00830   0.00227  -0.0462   0.8058   0.0337
  -4.000  -0.2283   0.00813   0.00210  -0.0461   0.7985   0.0407
  -3.750  -0.2011   0.00797   0.00194  -0.0460   0.7908   0.0500
  -3.500  -0.1736   0.00782   0.00180  -0.0460   0.7829   0.0602
  -3.250  -0.1463   0.00765   0.00164  -0.0459   0.7746   0.0754
  -3.000  -0.1189   0.00749   0.00151  -0.0458   0.7656   0.0930
  -2.750  -0.0916   0.00732   0.00138  -0.0458   0.7571   0.1165
  -2.500  -0.0644   0.00712   0.00126  -0.0457   0.7484   0.1513
  -2.250  -0.0372   0.00690   0.00115  -0.0457   0.7392   0.1928
  -2.000  -0.0104   0.00666   0.00104  -0.0456   0.7273   0.2450
  -1.750   0.0162   0.00640   0.00093  -0.0455   0.7134   0.3084
  -1.500   0.0423   0.00603   0.00083  -0.0454   0.7014   0.4056
  -1.250   0.0692   0.00581   0.00077  -0.0453   0.6910   0.4704
  -1.000   0.0966   0.00570   0.00074  -0.0452   0.6793   0.5102
  -0.750   0.1238   0.00558   0.00074  -0.0451   0.6679   0.5590
  -0.500   0.1511   0.00550   0.00074  -0.0450   0.6578   0.6008
  -0.250   0.1789   0.00551   0.00075  -0.0449   0.6449   0.6194
   0.000   0.2066   0.00554   0.00075  -0.0449   0.6300   0.6340
   0.500   0.2621   0.00560   0.00079  -0.0448   0.6020   0.6604
   0.750   0.2897   0.00564   0.00082  -0.0447   0.5849   0.6749
   1.000   0.3171   0.00570   0.00085  -0.0446   0.5670   0.6879
   1.250   0.3445   0.00579   0.00090  -0.0445   0.5462   0.6966
   1.750   0.3986   0.00606   0.00102  -0.0442   0.4923   0.7120
   2.000   0.4254   0.00625   0.00110  -0.0440   0.4600   0.7197
   2.250   0.4518   0.00646   0.00121  -0.0438   0.4249   0.7279
   2.500   0.4778   0.00671   0.00133  -0.0435   0.3838   0.7361
   2.750   0.5033   0.00704   0.00148  -0.0432   0.3327   0.7452
   3.000   0.5280   0.00744   0.00167  -0.0428   0.2756   0.7542
   3.250   0.5536   0.00774   0.00185  -0.0425   0.2415   0.7636
   3.500   0.5804   0.00789   0.00198  -0.0423   0.2265   0.7732
   3.750   0.6072   0.00804   0.00211  -0.0422   0.2138   0.7826
   4.000   0.6338   0.00819   0.00226  -0.0420   0.2007   0.7924
   4.500   0.6858   0.00860   0.00260  -0.0415   0.1603   0.8145
   4.750   0.7102   0.00896   0.00284  -0.0410   0.1248   0.8271
   5.000   0.7334   0.00944   0.00316  -0.0403   0.0846   0.8416
   5.250   0.7576   0.00974   0.00344  -0.0397   0.0653   0.8590
   5.500   0.7813   0.00995   0.00368  -0.0390   0.0531   0.8857
   5.750   0.8084   0.01011   0.00395  -0.0389   0.0420   0.9564
   6.000   0.8414   0.01042   0.00423  -0.0403   0.0349   1.0000
   6.250   0.8668   0.01070   0.00449  -0.0400   0.0293   1.0000
   6.500   0.8919   0.01103   0.00480  -0.0396   0.0239   1.0000
   6.750   0.9167   0.01137   0.00511  -0.0392   0.0180   1.0000
   7.000   0.9414   0.01173   0.00544  -0.0388   0.0139   1.0000
   7.250   0.9648   0.01222   0.00588  -0.0382   0.0059   1.0000
   7.500   0.9885   0.01267   0.00633  -0.0376   0.0041   1.0000
   7.750   1.0128   0.01306   0.00674  -0.0371   0.0035   1.0000
   8.000   1.0366   0.01347   0.00722  -0.0366   0.0032   1.0000
   8.250   1.0599   0.01393   0.00772  -0.0360   0.0029   1.0000
   8.500   1.0827   0.01444   0.00829  -0.0353   0.0025   1.0000
   8.750   1.1049   0.01499   0.00891  -0.0345   0.0023   1.0000
   9.000   1.1265   0.01560   0.00959  -0.0336   0.0021   1.0000
   9.250   1.1484   0.01614   0.01019  -0.0329   0.0021   1.0000
   9.500   1.1699   0.01669   0.01080  -0.0320   0.0020   1.0000
   9.750   1.1909   0.01727   0.01144  -0.0312   0.0020   1.0000
  10.000   1.2109   0.01792   0.01218  -0.0302   0.0019   1.0000
  10.250   1.2304   0.01858   0.01292  -0.0291   0.0019   1.0000
  10.500   1.2492   0.01927   0.01368  -0.0280   0.0018   1.0000
  10.750   1.2669   0.02002   0.01451  -0.0267   0.0018   1.0000
  11.000   1.2833   0.02081   0.01539  -0.0252   0.0017   1.0000
  11.250   1.2988   0.02162   0.01629  -0.0237   0.0016   1.0000
  11.500   1.3115   0.02250   0.01726  -0.0218   0.0016   1.0000
  11.750   1.3205   0.02341   0.01827  -0.0192   0.0015   1.0000
  12.000   1.3285   0.02437   0.01932  -0.0167   0.0015   1.0000
  12.250   1.3360   0.02540   0.02045  -0.0143   0.0015   1.0000
  12.500   1.3433   0.02648   0.02164  -0.0122   0.0014   1.0000
  12.750   1.3457   0.02796   0.02325  -0.0098   0.0014   1.0000
  13.000   1.3507   0.02934   0.02472  -0.0080   0.0014   1.0000
  13.250   1.3521   0.03109   0.02660  -0.0061   0.0013   1.0000
  13.500   1.3559   0.03274   0.02834  -0.0048   0.0013   1.0000
  13.750   1.3544   0.03497   0.03071  -0.0035   0.0013   1.0000
  14.000   1.3522   0.03741   0.03328  -0.0025   0.0013   1.0000
  14.250   1.3552   0.03949   0.03544  -0.0021   0.0012   1.0000
  14.500   1.3487   0.04273   0.03882  -0.0019   0.0012   1.0000
  14.750   1.3425   0.04616   0.04238  -0.0021   0.0012   1.0000
  15.000   1.3309   0.05055   0.04693  -0.0030   0.0012   1.0000
  15.250   1.3215   0.05499   0.05151  -0.0045   0.0012   1.0000
  15.500   1.3061   0.06073   0.05741  -0.0069   0.0012   1.0000
  15.750   1.2910   0.06696   0.06378  -0.0101   0.0011   1.0000
  16.000   1.2693   0.07494   0.07195  -0.0144   0.0012   1.0000
  16.250   1.2478   0.08361   0.08076  -0.0195   0.0011   1.0000
  16.500   1.2259   0.09273   0.09004  -0.0248   0.0012   1.0000
  16.750   1.1937   0.10439   0.10188  -0.0314   0.0012   1.0000
  17.000   1.1660   0.11526   0.11287  -0.0375   0.0012   1.0000
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