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HQ 3.0/15 AIRFOIL (hq3015-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/15 AIRFOIL (hq3015-il)
Reynolds number: 200,000
Max Cl/Cd: 67.73 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3015-il-200000-n5.txt
Download as CSV file: xf-hq3015-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6411   0.07194   0.06772  -0.0740   1.0000   0.0181
 -13.750  -0.6840   0.06118   0.05669  -0.0811   1.0000   0.0178
 -13.500  -0.7084   0.05488   0.05021  -0.0846   1.0000   0.0178
 -13.250  -0.7260   0.05020   0.04536  -0.0866   1.0000   0.0179
 -13.000  -0.7404   0.04641   0.04142  -0.0875   1.0000   0.0181
 -12.750  -0.7530   0.04325   0.03811  -0.0875   1.0000   0.0184
 -12.500  -0.7648   0.04063   0.03537  -0.0866   1.0000   0.0186
 -12.250  -0.7784   0.03855   0.03318  -0.0845   1.0000   0.0188
 -12.000  -0.7829   0.03624   0.03069  -0.0841   0.9961   0.0192
 -11.750  -0.7685   0.03364   0.02784  -0.0869   0.9857   0.0199
 -11.500  -0.7494   0.03195   0.02606  -0.0893   0.9770   0.0205
 -11.250  -0.7266   0.03048   0.02445  -0.0915   0.9701   0.0214
 -11.000  -0.7067   0.02901   0.02280  -0.0925   0.9611   0.0227
 -10.750  -0.6817   0.02740   0.02094  -0.0941   0.9552   0.0243
 -10.500  -0.6604   0.02650   0.02000  -0.0946   0.9460   0.0255
 -10.250  -0.6331   0.02555   0.01891  -0.0959   0.9403   0.0276
 -10.000  -0.6117   0.02461   0.01779  -0.0959   0.9316   0.0298
  -9.750  -0.5853   0.02388   0.01701  -0.0968   0.9256   0.0316
  -9.500  -0.5628   0.02318   0.01619  -0.0966   0.9176   0.0338
  -9.250  -0.5378   0.02237   0.01521  -0.0968   0.9115   0.0360
  -9.000  -0.5150   0.02184   0.01465  -0.0967   0.9045   0.0380
  -8.750  -0.4910   0.02136   0.01406  -0.0965   0.8977   0.0407
  -8.500  -0.4665   0.02082   0.01337  -0.0963   0.8917   0.0433
  -8.250  -0.4450   0.02035   0.01290  -0.0957   0.8843   0.0459
  -8.000  -0.4202   0.01991   0.01236  -0.0955   0.8788   0.0487
  -7.750  -0.3974   0.01947   0.01180  -0.0949   0.8719   0.0511
  -7.500  -0.3751   0.01882   0.01110  -0.0943   0.8657   0.0534
  -7.250  -0.3515   0.01832   0.01056  -0.0938   0.8604   0.0559
  -7.000  -0.3288   0.01788   0.01007  -0.0931   0.8539   0.0585
  -6.750  -0.3046   0.01742   0.00950  -0.0926   0.8485   0.0609
  -6.500  -0.2816   0.01693   0.00896  -0.0920   0.8429   0.0637
  -6.250  -0.2586   0.01648   0.00851  -0.0914   0.8368   0.0673
  -6.000  -0.2337   0.01609   0.00804  -0.0910   0.8319   0.0711
  -5.750  -0.2097   0.01573   0.00762  -0.0905   0.8262   0.0751
  -5.500  -0.1858   0.01532   0.00722  -0.0900   0.8204   0.0806
  -5.000  -0.1357   0.01466   0.00651  -0.0893   0.8102   0.0968
  -4.750  -0.1109   0.01432   0.00619  -0.0889   0.8046   0.1094
  -4.500  -0.0852   0.01397   0.00586  -0.0887   0.8002   0.1282
  -4.250  -0.0608   0.01359   0.00561  -0.0883   0.7948   0.1586
  -4.000  -0.0364   0.01318   0.00536  -0.0880   0.7892   0.2036
  -3.750  -0.0113   0.01274   0.00509  -0.0878   0.7847   0.2586
  -3.500   0.0125   0.01225   0.00485  -0.0874   0.7795   0.3232
  -3.250   0.0349   0.01175   0.00480  -0.0867   0.7738   0.4371
  -3.000   0.0614   0.01162   0.00477  -0.0863   0.7693   0.4922
  -2.750   0.0881   0.01159   0.00476  -0.0860   0.7641   0.5243
  -2.500   0.1146   0.01158   0.00477  -0.0856   0.7583   0.5494
  -2.250   0.1423   0.01158   0.00474  -0.0853   0.7535   0.5725
  -2.000   0.1691   0.01162   0.00478  -0.0849   0.7479   0.5939
  -1.750   0.1955   0.01167   0.00484  -0.0844   0.7419   0.6135
  -1.500   0.2235   0.01169   0.00480  -0.0843   0.7370   0.6265
  -1.250   0.2506   0.01172   0.00481  -0.0840   0.7313   0.6359
  -1.000   0.2778   0.01174   0.00481  -0.0838   0.7255   0.6443
  -0.750   0.3062   0.01175   0.00475  -0.0838   0.7208   0.6534
  -0.500   0.3327   0.01179   0.00481  -0.0834   0.7148   0.6620
  -0.250   0.3601   0.01183   0.00481  -0.0832   0.7090   0.6720
   0.000   0.3881   0.01184   0.00479  -0.0831   0.7041   0.6785
   0.250   0.4144   0.01186   0.00481  -0.0827   0.6959   0.6849
   0.500   0.4426   0.01184   0.00471  -0.0826   0.6886   0.6903
   0.750   0.4683   0.01184   0.00473  -0.0821   0.6783   0.6951
   1.000   0.4955   0.01185   0.00469  -0.0819   0.6699   0.7012
   1.250   0.5222   0.01188   0.00471  -0.0817   0.6620   0.7070
   1.500   0.5493   0.01191   0.00474  -0.0814   0.6551   0.7126
   1.750   0.5758   0.01195   0.00478  -0.0811   0.6468   0.7190
   2.000   0.6025   0.01199   0.00482  -0.0808   0.6390   0.7245
   2.250   0.6285   0.01204   0.00489  -0.0804   0.6301   0.7309
   2.500   0.6548   0.01210   0.00493  -0.0801   0.6210   0.7378
   2.750   0.6806   0.01214   0.00498  -0.0796   0.6112   0.7436
   3.000   0.7057   0.01221   0.00506  -0.0791   0.5994   0.7508
   3.250   0.7305   0.01227   0.00513  -0.0784   0.5866   0.7574
   3.500   0.7550   0.01235   0.00520  -0.0777   0.5729   0.7648
   3.750   0.7793   0.01245   0.00530  -0.0770   0.5590   0.7720
   4.000   0.8030   0.01256   0.00540  -0.0762   0.5445   0.7796
   4.250   0.8265   0.01269   0.00552  -0.0754   0.5288   0.7878
   4.500   0.8491   0.01284   0.00566  -0.0744   0.5114   0.7964
   4.750   0.8708   0.01302   0.00581  -0.0732   0.4934   0.8051
   5.000   0.8916   0.01323   0.00598  -0.0719   0.4744   0.8151
   5.500   0.9300   0.01373   0.00641  -0.0688   0.4341   0.8378
   5.750   0.9484   0.01402   0.00667  -0.0671   0.4139   0.8519
   6.000   0.9660   0.01432   0.00695  -0.0654   0.3943   0.8701
   6.250   0.9850   0.01462   0.00727  -0.0639   0.3748   0.9002
   6.500   1.0122   0.01500   0.00764  -0.0644   0.3530   1.0000
   6.750   1.0286   0.01546   0.00801  -0.0627   0.3356   1.0000
   7.000   1.0433   0.01592   0.00841  -0.0607   0.3202   1.0000
   7.250   1.0576   0.01643   0.00885  -0.0586   0.3061   1.0000
   7.500   1.0719   0.01696   0.00932  -0.0567   0.2933   1.0000
   7.750   1.0860   0.01753   0.00984  -0.0548   0.2818   1.0000
   8.000   1.1010   0.01808   0.01038  -0.0530   0.2707   1.0000
   8.250   1.1160   0.01866   0.01094  -0.0514   0.2598   1.0000
   8.500   1.1298   0.01929   0.01155  -0.0496   0.2495   1.0000
   8.750   1.1442   0.01993   0.01218  -0.0480   0.2393   1.0000
   9.000   1.1586   0.02058   0.01284  -0.0465   0.2289   1.0000
   9.250   1.1716   0.02132   0.01356  -0.0448   0.2195   1.0000
   9.500   1.1854   0.02204   0.01430  -0.0433   0.2100   1.0000
   9.750   1.1988   0.02281   0.01508  -0.0419   0.2013   1.0000
  10.000   1.2102   0.02371   0.01595  -0.0403   0.1925   1.0000
  10.250   1.2238   0.02452   0.01681  -0.0389   0.1841   1.0000
  10.500   1.2342   0.02553   0.01780  -0.0374   0.1765   1.0000
  10.750   1.2472   0.02642   0.01874  -0.0362   0.1686   1.0000
  11.000   1.2570   0.02753   0.01984  -0.0347   0.1616   1.0000
  11.250   1.2696   0.02850   0.02087  -0.0336   0.1545   1.0000
  11.500   1.2779   0.02977   0.02214  -0.0322   0.1482   1.0000
  11.750   1.2906   0.03079   0.02325  -0.0312   0.1416   1.0000
  12.000   1.2991   0.03211   0.02458  -0.0300   0.1356   1.0000
  12.250   1.3096   0.03333   0.02587  -0.0289   0.1293   1.0000
  12.500   1.3173   0.03478   0.02734  -0.0279   0.1225   1.0000
  12.750   1.3260   0.03619   0.02881  -0.0269   0.1160   1.0000
  13.000   1.3316   0.03789   0.03051  -0.0259   0.1086   1.0000
  13.250   1.3397   0.03944   0.03214  -0.0251   0.1028   1.0000
  13.500   1.3439   0.04136   0.03406  -0.0243   0.0957   1.0000
  13.750   1.3506   0.04312   0.03589  -0.0236   0.0900   1.0000
  14.000   1.3545   0.04519   0.03799  -0.0230   0.0842   1.0000
  14.250   1.3592   0.04725   0.04012  -0.0225   0.0799   1.0000
  14.500   1.3634   0.04941   0.04235  -0.0221   0.0749   1.0000
  14.750   1.3642   0.05200   0.04497  -0.0218   0.0704   1.0000
  15.000   1.3686   0.05428   0.04737  -0.0216   0.0673   1.0000
  15.250   1.3704   0.05691   0.05008  -0.0215   0.0637   1.0000
  15.500   1.3688   0.06001   0.05322  -0.0216   0.0604   1.0000
  15.750   1.3707   0.06277   0.05609  -0.0218   0.0571   1.0000
  16.000   1.3702   0.06592   0.05933  -0.0222   0.0539   1.0000
  16.250   1.3672   0.06948   0.06296  -0.0228   0.0514   1.0000
  16.500   1.3652   0.07300   0.06658  -0.0235   0.0490   1.0000
  16.750   1.3640   0.07649   0.07020  -0.0243   0.0469   1.0000
  17.000   1.3607   0.08038   0.07421  -0.0253   0.0450   1.0000
  17.250   1.3557   0.08462   0.07855  -0.0266   0.0434   1.0000
  17.500   1.3490   0.08920   0.08325  -0.0282   0.0422   1.0000
  17.750   1.3439   0.09364   0.08782  -0.0298   0.0408   1.0000
  18.000   1.3393   0.09809   0.09241  -0.0315   0.0394   1.0000
  18.250   1.3330   0.10289   0.09735  -0.0334   0.0380   1.0000
  18.500   1.3253   0.10801   0.10259  -0.0357   0.0367   1.0000
  18.750   1.3156   0.11356   0.10825  -0.0383   0.0355   1.0000
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