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HQ 1.5/11 AIRFOIL (hq1511-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.5/11 AIRFOIL (hq1511-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.42 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1511-il-1000000-n5.txt
Download as CSV file: xf-hq1511-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.5/11 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7836   0.09983   0.09784  -0.0207   1.0000   0.0042
 -14.500  -0.8563   0.08049   0.07833  -0.0310   1.0000   0.0041
 -14.250  -0.9110   0.06390   0.06151  -0.0414   1.0000   0.0039
 -14.000  -0.9406   0.05347   0.05089  -0.0493   1.0000   0.0039
 -13.750  -0.9513   0.04784   0.04512  -0.0535   1.0000   0.0040
 -13.500  -0.9716   0.04173   0.03882  -0.0574   1.0000   0.0039
 -13.250  -0.9856   0.03729   0.03420  -0.0594   1.0000   0.0039
 -13.000  -0.9897   0.03447   0.03125  -0.0599   1.0000   0.0040
 -12.750  -0.9934   0.03206   0.02871  -0.0597   1.0000   0.0040
 -12.500  -1.0002   0.02987   0.02638  -0.0583   1.0000   0.0040
 -12.250  -1.0006   0.02855   0.02494  -0.0558   1.0000   0.0041
 -12.000  -0.9969   0.02705   0.02331  -0.0538   1.0000   0.0041
 -11.750  -0.9885   0.02564   0.02176  -0.0522   1.0000   0.0042
 -11.500  -0.9776   0.02432   0.02030  -0.0507   1.0000   0.0042
 -11.250  -0.9641   0.02318   0.01904  -0.0494   1.0000   0.0043
 -11.000  -0.9497   0.02206   0.01779  -0.0481   1.0000   0.0043
 -10.750  -0.9335   0.02112   0.01675  -0.0468   1.0000   0.0044
 -10.500  -0.9168   0.02025   0.01577  -0.0455   1.0000   0.0044
 -10.250  -0.8925   0.01927   0.01467  -0.0458   0.9936   0.0045
 -10.000  -0.8631   0.01835   0.01364  -0.0471   0.9865   0.0045
  -9.750  -0.8327   0.01743   0.01261  -0.0485   0.9790   0.0046
  -9.500  -0.8011   0.01661   0.01170  -0.0500   0.9711   0.0046
  -9.250  -0.7709   0.01590   0.01088  -0.0511   0.9613   0.0047
  -9.000  -0.7429   0.01528   0.01016  -0.0516   0.9495   0.0047
  -8.750  -0.7179   0.01471   0.00950  -0.0515   0.9351   0.0047
  -8.500  -0.6947   0.01410   0.00878  -0.0509   0.9193   0.0048
  -8.250  -0.6720   0.01349   0.00805  -0.0501   0.9036   0.0049
  -8.000  -0.6491   0.01289   0.00733  -0.0494   0.8894   0.0050
  -7.750  -0.6252   0.01242   0.00675  -0.0489   0.8776   0.0051
  -7.500  -0.6008   0.01199   0.00622  -0.0483   0.8676   0.0053
  -7.250  -0.5756   0.01159   0.00575  -0.0480   0.8590   0.0055
  -7.000  -0.5501   0.01125   0.00534  -0.0476   0.8515   0.0056
  -6.750  -0.5241   0.01093   0.00495  -0.0474   0.8438   0.0057
  -6.500  -0.4981   0.01063   0.00458  -0.0471   0.8365   0.0058
  -6.250  -0.4717   0.01036   0.00425  -0.0469   0.8287   0.0060
  -6.000  -0.4453   0.01011   0.00393  -0.0467   0.8211   0.0062
  -5.750  -0.4186   0.00988   0.00365  -0.0465   0.8126   0.0065
  -5.500  -0.3917   0.00966   0.00337  -0.0463   0.8046   0.0068
  -5.250  -0.3649   0.00945   0.00312  -0.0461   0.7954   0.0078
  -5.000  -0.3385   0.00916   0.00284  -0.0459   0.7858   0.0143
  -4.750  -0.3117   0.00896   0.00262  -0.0457   0.7750   0.0207
  -4.500  -0.2847   0.00880   0.00244  -0.0456   0.7650   0.0251
  -4.250  -0.2574   0.00862   0.00228  -0.0455   0.7565   0.0316
  -4.000  -0.2301   0.00849   0.00213  -0.0455   0.7488   0.0371
  -3.750  -0.2025   0.00833   0.00198  -0.0454   0.7412   0.0443
  -3.250  -0.1475   0.00802   0.00172  -0.0454   0.7271   0.0660
  -3.000  -0.1201   0.00789   0.00159  -0.0453   0.7188   0.0790
  -2.750  -0.0927   0.00769   0.00146  -0.0453   0.7106   0.1033
  -2.500  -0.0667   0.00726   0.00131  -0.0452   0.7032   0.1866
  -2.250  -0.0392   0.00707   0.00121  -0.0452   0.6961   0.2204
  -2.000  -0.0117   0.00689   0.00112  -0.0452   0.6901   0.2537
  -1.750   0.0154   0.00660   0.00101  -0.0452   0.6843   0.3154
  -1.500   0.0417   0.00623   0.00093  -0.0451   0.6767   0.4087
  -1.250   0.0692   0.00607   0.00087  -0.0451   0.6682   0.4518
  -1.000   0.0963   0.00591   0.00083  -0.0450   0.6567   0.5010
  -0.750   0.1233   0.00576   0.00082  -0.0449   0.6446   0.5574
  -0.500   0.1509   0.00570   0.00083  -0.0448   0.6331   0.5923
  -0.250   0.1789   0.00571   0.00083  -0.0448   0.6206   0.6076
   0.000   0.2069   0.00573   0.00084  -0.0448   0.6081   0.6218
   0.250   0.2348   0.00576   0.00086  -0.0447   0.5945   0.6344
   0.500   0.2625   0.00583   0.00088  -0.0447   0.5755   0.6454
   0.750   0.2900   0.00592   0.00091  -0.0446   0.5525   0.6547
   1.000   0.3172   0.00605   0.00095  -0.0444   0.5244   0.6623
   1.250   0.3442   0.00621   0.00101  -0.0443   0.4933   0.6698
   1.500   0.3713   0.00637   0.00108  -0.0442   0.4679   0.6757
   1.750   0.3986   0.00650   0.00116  -0.0441   0.4481   0.6818
   2.000   0.4261   0.00663   0.00124  -0.0440   0.4309   0.6881
   2.250   0.4530   0.00678   0.00134  -0.0439   0.4094   0.6956
   2.500   0.4789   0.00708   0.00146  -0.0436   0.3583   0.7026
   2.750   0.5031   0.00753   0.00165  -0.0431   0.2935   0.7083
   3.000   0.5291   0.00781   0.00181  -0.0428   0.2624   0.7146
   3.250   0.5557   0.00799   0.00194  -0.0427   0.2435   0.7210
   3.500   0.5827   0.00813   0.00207  -0.0426   0.2327   0.7288
   3.750   0.6098   0.00826   0.00220  -0.0424   0.2236   0.7365
   4.000   0.6368   0.00839   0.00233  -0.0423   0.2162   0.7454
   4.250   0.6637   0.00850   0.00247  -0.0422   0.2099   0.7547
   4.500   0.6904   0.00863   0.00263  -0.0420   0.2020   0.7654
   4.750   0.7167   0.00880   0.00279  -0.0418   0.1889   0.7766
   5.000   0.7415   0.00911   0.00298  -0.0413   0.1526   0.7876
   5.250   0.7652   0.00953   0.00327  -0.0408   0.1189   0.7986
   5.500   0.7895   0.00988   0.00355  -0.0403   0.0971   0.8097
   5.750   0.8144   0.01015   0.00381  -0.0398   0.0837   0.8220
   6.000   0.8392   0.01039   0.00406  -0.0393   0.0732   0.8363
   6.250   0.8634   0.01063   0.00432  -0.0387   0.0631   0.8534
   6.500   0.8866   0.01089   0.00461  -0.0379   0.0525   0.8767
   6.750   0.9082   0.01108   0.00490  -0.0367   0.0432   0.9259
   7.000   0.9437   0.01145   0.00526  -0.0387   0.0334   1.0000
   7.250   0.9678   0.01182   0.00561  -0.0382   0.0272   1.0000
   7.500   0.9918   0.01220   0.00596  -0.0377   0.0230   1.0000
   7.750   1.0161   0.01254   0.00630  -0.0372   0.0203   1.0000
   8.000   1.0400   0.01290   0.00667  -0.0367   0.0183   1.0000
   8.250   1.0633   0.01332   0.00709  -0.0361   0.0163   1.0000
   8.500   1.0870   0.01367   0.00747  -0.0356   0.0155   1.0000
   8.750   1.1104   0.01404   0.00787  -0.0350   0.0146   1.0000
   9.000   1.1331   0.01445   0.00830  -0.0343   0.0136   1.0000
   9.250   1.1551   0.01491   0.00877  -0.0335   0.0126   1.0000
   9.500   1.1767   0.01540   0.00930  -0.0327   0.0119   1.0000
   9.750   1.1987   0.01581   0.00976  -0.0319   0.0115   1.0000
  10.000   1.2201   0.01625   0.01024  -0.0311   0.0109   1.0000
  10.250   1.2408   0.01672   0.01075  -0.0302   0.0104   1.0000
  10.500   1.2608   0.01722   0.01127  -0.0292   0.0098   1.0000
  10.750   1.2796   0.01779   0.01187  -0.0280   0.0093   1.0000
  11.000   1.2963   0.01847   0.01261  -0.0265   0.0088   1.0000
  11.250   1.3143   0.01898   0.01318  -0.0252   0.0085   1.0000
  11.500   1.3300   0.01950   0.01376  -0.0235   0.0083   1.0000
  11.750   1.3437   0.02006   0.01437  -0.0215   0.0080   1.0000
  12.000   1.3571   0.02065   0.01501  -0.0196   0.0076   1.0000
  12.250   1.3692   0.02133   0.01575  -0.0176   0.0073   1.0000
  12.500   1.3811   0.02206   0.01652  -0.0157   0.0070   1.0000
  12.750   1.3915   0.02290   0.01743  -0.0138   0.0068   1.0000
  13.000   1.4003   0.02389   0.01848  -0.0119   0.0065   1.0000
  13.250   1.4073   0.02504   0.01971  -0.0099   0.0063   1.0000
  13.500   1.4166   0.02609   0.02083  -0.0084   0.0061   1.0000
  13.750   1.4254   0.02721   0.02204  -0.0069   0.0060   1.0000
  14.000   1.4339   0.02840   0.02331  -0.0056   0.0058   1.0000
  14.250   1.4398   0.02986   0.02485  -0.0043   0.0057   1.0000
  14.500   1.4468   0.03128   0.02635  -0.0032   0.0055   1.0000
  14.750   1.4512   0.03299   0.02816  -0.0021   0.0054   1.0000
  15.000   1.4560   0.03474   0.02999  -0.0013   0.0052   1.0000
  15.250   1.4592   0.03673   0.03207  -0.0006   0.0051   1.0000
  15.500   1.4619   0.03884   0.03427  -0.0002   0.0049   1.0000
  15.750   1.4625   0.04127   0.03679   0.0001   0.0048   1.0000
  16.000   1.4605   0.04409   0.03971   0.0002   0.0047   1.0000
  16.250   1.4584   0.04705   0.04277   0.0000   0.0046   1.0000
  16.500   1.4531   0.05056   0.04638  -0.0006   0.0044   1.0000
  16.750   1.4450   0.05463   0.05057  -0.0016   0.0044   1.0000
  17.000   1.4339   0.05943   0.05551  -0.0032   0.0043   1.0000
  17.250   1.4252   0.06418   0.06038  -0.0051   0.0042   1.0000
  17.500   1.4113   0.07004   0.06638  -0.0078   0.0042   1.0000
  17.750   1.3993   0.07589   0.07237  -0.0107   0.0042   1.0000
  18.000   1.3792   0.08340   0.08003  -0.0146   0.0042   1.0000
  18.250   1.3591   0.09125   0.08803  -0.0189   0.0042   1.0000
  18.500   1.3340   0.10041   0.09735  -0.0239   0.0042   1.0000
  18.750   1.3117   0.10922   0.10630  -0.0289   0.0042   1.0000
  19.000   1.2825   0.11965   0.11688  -0.0349   0.0042   1.0000
  19.250   1.2526   0.13040   0.12777  -0.0413   0.0042   1.0000
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