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HQ 3.0/15 AIRFOIL (hq3015-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/15 AIRFOIL (hq3015-il)
Reynolds number: 100,000
Max Cl/Cd: 51.46 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3015-il-100000-n5.txt
Download as CSV file: xf-hq3015-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4297   0.09578   0.09055  -0.0603   1.0000   0.0351
 -12.000  -0.4896   0.07826   0.07305  -0.0700   1.0000   0.0347
 -11.750  -0.5337   0.06809   0.06281  -0.0764   1.0000   0.0341
 -11.500  -0.5698   0.06172   0.05637  -0.0792   1.0000   0.0337
 -11.250  -0.6039   0.05743   0.05199  -0.0793   1.0000   0.0335
 -11.000  -0.6379   0.05486   0.04939  -0.0765   1.0000   0.0334
 -10.750  -0.6681   0.05246   0.04688  -0.0741   0.9973   0.0333
 -10.500  -0.6770   0.04735   0.04128  -0.0779   0.9838   0.0341
 -10.250  -0.6788   0.04231   0.03552  -0.0801   0.9725   0.0355
 -10.000  -0.6560   0.04088   0.03409  -0.0817   0.9665   0.0369
  -9.750  -0.6359   0.03936   0.03241  -0.0828   0.9592   0.0389
  -9.500  -0.6162   0.03681   0.02935  -0.0843   0.9534   0.0420
  -9.250  -0.5965   0.03540   0.02782  -0.0847   0.9459   0.0445
  -9.000  -0.5681   0.03418   0.02645  -0.0864   0.9415   0.0476
  -8.750  -0.5479   0.03265   0.02448  -0.0864   0.9344   0.0513
  -8.500  -0.5221   0.03138   0.02319  -0.0872   0.9290   0.0541
  -8.250  -0.4920   0.03028   0.02194  -0.0886   0.9252   0.0578
  -8.000  -0.4709   0.02925   0.02061  -0.0880   0.9178   0.0613
  -7.750  -0.4431   0.02804   0.01935  -0.0887   0.9131   0.0645
  -7.500  -0.4117   0.02708   0.01831  -0.0899   0.9097   0.0683
  -7.250  -0.3906   0.02627   0.01736  -0.0890   0.9022   0.0714
  -7.000  -0.3622   0.02535   0.01629  -0.0894   0.8975   0.0750
  -6.750  -0.3320   0.02445   0.01542  -0.0903   0.8940   0.0792
  -6.500  -0.3126   0.02388   0.01478  -0.0891   0.8863   0.0827
  -6.250  -0.2850   0.02320   0.01396  -0.0892   0.8815   0.0871
  -6.000  -0.2576   0.02242   0.01325  -0.0895   0.8775   0.0928
  -5.750  -0.2385   0.02202   0.01279  -0.0882   0.8697   0.0993
  -5.500  -0.2125   0.02138   0.01217  -0.0881   0.8651   0.1073
  -5.250  -0.1875   0.02086   0.01163  -0.0879   0.8601   0.1177
  -5.000  -0.1671   0.02044   0.01124  -0.0868   0.8532   0.1314
  -4.750  -0.1410   0.01982   0.01073  -0.0869   0.8488   0.1540
  -4.500  -0.1186   0.01930   0.01036  -0.0863   0.8432   0.1907
  -4.250  -0.0981   0.01877   0.01004  -0.0855   0.8367   0.2422
  -4.000  -0.0735   0.01801   0.00961  -0.0854   0.8324   0.3190
  -3.750  -0.0552   0.01756   0.00972  -0.0838   0.8264   0.4335
  -3.500  -0.0323   0.01753   0.00985  -0.0826   0.8204   0.5032
  -3.250  -0.0038   0.01754   0.00985  -0.0823   0.8164   0.5465
  -3.000   0.0194   0.01769   0.00997  -0.0812   0.8105   0.5770
  -2.750   0.0436   0.01784   0.01008  -0.0802   0.8045   0.6019
  -2.500   0.0721   0.01793   0.01013  -0.0798   0.8005   0.6265
  -2.250   0.0946   0.01815   0.01032  -0.0783   0.7944   0.6462
  -2.000   0.1189   0.01828   0.01041  -0.0773   0.7885   0.6622
  -1.750   0.1486   0.01825   0.01030  -0.0772   0.7845   0.6751
  -1.500   0.1711   0.01837   0.01037  -0.0761   0.7778   0.6862
  -1.250   0.1966   0.01842   0.01038  -0.0753   0.7720   0.6967
  -1.000   0.2265   0.01836   0.01025  -0.0753   0.7681   0.7085
  -0.750   0.2473   0.01849   0.01036  -0.0740   0.7605   0.7188
  -0.500   0.2748   0.01844   0.01028  -0.0737   0.7553   0.7260
  -0.250   0.3065   0.01830   0.01005  -0.0742   0.7516   0.7330
   0.000   0.3264   0.01844   0.01019  -0.0729   0.7432   0.7394
   0.250   0.3556   0.01835   0.01005  -0.0730   0.7383   0.7453
   0.500   0.3818   0.01836   0.01002  -0.0728   0.7321   0.7529
   0.750   0.4065   0.01838   0.01005  -0.0721   0.7254   0.7588
   1.000   0.4380   0.01824   0.00986  -0.0725   0.7208   0.7658
   1.250   0.4591   0.01831   0.00996  -0.0714   0.7117   0.7727
   1.500   0.4908   0.01805   0.00964  -0.0716   0.7050   0.7799
   1.750   0.5126   0.01805   0.00966  -0.0704   0.6943   0.7876
   2.000   0.5410   0.01789   0.00947  -0.0702   0.6863   0.7951
   2.250   0.5653   0.01789   0.00949  -0.0695   0.6773   0.8033
   2.500   0.5921   0.01783   0.00944  -0.0691   0.6699   0.8117
   2.750   0.6170   0.01781   0.00945  -0.0685   0.6610   0.8204
   3.000   0.6420   0.01780   0.00947  -0.0678   0.6523   0.8301
   3.250   0.6685   0.01771   0.00940  -0.0673   0.6435   0.8396
   3.500   0.6907   0.01775   0.00950  -0.0663   0.6330   0.8508
   3.750   0.7169   0.01766   0.00944  -0.0657   0.6232   0.8628
   4.000   0.7413   0.01759   0.00943  -0.0649   0.6118   0.8761
   4.250   0.7647   0.01759   0.00951  -0.0640   0.5988   0.8931
   4.500   0.7933   0.01756   0.00955  -0.0641   0.5847   0.9137
   4.750   0.8291   0.01755   0.00960  -0.0657   0.5690   0.9478
   5.000   0.8592   0.01762   0.00965  -0.0665   0.5531   1.0000
   5.250   0.8828   0.01778   0.00976  -0.0659   0.5369   1.0000
   5.500   0.9059   0.01797   0.00990  -0.0653   0.5199   1.0000
   5.750   0.9284   0.01820   0.01005  -0.0645   0.5022   1.0000
   6.000   0.9491   0.01849   0.01028  -0.0634   0.4829   1.0000
   6.250   0.9690   0.01883   0.01056  -0.0622   0.4633   1.0000
   6.500   0.9880   0.01921   0.01085  -0.0609   0.4432   1.0000
   6.750   1.0062   0.01965   0.01118  -0.0594   0.4237   1.0000
   7.000   1.0229   0.02013   0.01160  -0.0578   0.4045   1.0000
   7.250   1.0377   0.02065   0.01206  -0.0559   0.3858   1.0000
   7.500   1.0519   0.02122   0.01255  -0.0539   0.3683   1.0000
   7.750   1.0657   0.02183   0.01310  -0.0519   0.3517   1.0000
   8.000   1.0795   0.02248   0.01370  -0.0501   0.3363   1.0000
   8.250   1.0932   0.02317   0.01435  -0.0483   0.3219   1.0000
   8.500   1.1068   0.02390   0.01504  -0.0465   0.3086   1.0000
   8.750   1.1202   0.02467   0.01575  -0.0448   0.2963   1.0000
   9.000   1.1334   0.02548   0.01653  -0.0432   0.2844   1.0000
   9.250   1.1468   0.02630   0.01739  -0.0416   0.2730   1.0000
   9.500   1.1599   0.02716   0.01825  -0.0401   0.2626   1.0000
   9.750   1.1718   0.02809   0.01914  -0.0385   0.2525   1.0000
  10.000   1.1843   0.02901   0.02013  -0.0371   0.2420   1.0000
  10.250   1.1962   0.02999   0.02113  -0.0357   0.2328   1.0000
  10.500   1.2069   0.03104   0.02221  -0.0342   0.2236   1.0000
  10.750   1.2182   0.03210   0.02334  -0.0329   0.2145   1.0000
  11.250   1.2379   0.03443   0.02577  -0.0302   0.1978   1.0000
  11.500   1.2464   0.03573   0.02706  -0.0289   0.1904   1.0000
  11.750   1.2553   0.03706   0.02849  -0.0277   0.1823   1.0000
  12.000   1.2628   0.03849   0.02994  -0.0265   0.1755   1.0000
  12.250   1.2706   0.03996   0.03154  -0.0254   0.1679   1.0000
  12.500   1.2766   0.04158   0.03315  -0.0243   0.1616   1.0000
  12.750   1.2834   0.04322   0.03494  -0.0234   0.1544   1.0000
  13.000   1.2877   0.04505   0.03676  -0.0224   0.1487   1.0000
  13.250   1.2938   0.04686   0.03874  -0.0217   0.1421   1.0000
  13.500   1.2970   0.04890   0.04085  -0.0209   0.1364   1.0000
  13.750   1.3012   0.05096   0.04300  -0.0203   0.1310   1.0000
  14.000   1.3039   0.05321   0.04539  -0.0198   0.1252   1.0000
  14.250   1.3048   0.05562   0.04780  -0.0193   0.1207   1.0000
  14.500   1.3075   0.05810   0.05047  -0.0191   0.1154   1.0000
  14.750   1.3077   0.06081   0.05329  -0.0190   0.1107   1.0000
  15.000   1.3075   0.06360   0.05607  -0.0189   0.1069   1.0000
  15.250   1.3077   0.06660   0.05928  -0.0191   0.1024   1.0000
  15.500   1.3063   0.06978   0.06259  -0.0194   0.0984   1.0000
  15.750   1.3042   0.07305   0.06589  -0.0198   0.0951   1.0000
  16.000   1.3017   0.07663   0.06966  -0.0205   0.0914   1.0000
  16.250   1.2976   0.08051   0.07369  -0.0214   0.0878   1.0000
  16.500   1.2928   0.08450   0.07777  -0.0225   0.0847   1.0000
  16.750   1.2892   0.08834   0.08162  -0.0236   0.0819   1.0000
  17.000   1.2816   0.09314   0.08667  -0.0253   0.0789   1.0000
  17.250   1.2739   0.09803   0.09172  -0.0272   0.0760   1.0000
  17.500   1.2670   0.10279   0.09658  -0.0292   0.0735   1.0000
  17.750   1.2626   0.10707   0.10084  -0.0311   0.0709   1.0000
  18.000   1.2517   0.11291   0.10691  -0.0338   0.0689   1.0000
  18.250   1.2395   0.11911   0.11332  -0.0369   0.0667   1.0000
  18.500   1.2290   0.12504   0.11940  -0.0400   0.0648   1.0000
  18.750   1.2203   0.13067   0.12513  -0.0431   0.0628   1.0000
  19.000   1.2183   0.13485   0.12931  -0.0455   0.0606   1.0000
  19.250   1.2060   0.14144   0.13605  -0.0493   0.0591   1.0000
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