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HQ 3.0/13 AIRFOIL (hq3013-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/13 AIRFOIL (hq3013-il)
Reynolds number: 500,000
Max Cl/Cd: 86.8 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3013-il-500000-n5.txt
Download as CSV file: xf-hq3013-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/13 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6730   0.07714   0.07427  -0.0602   1.0000   0.0072
 -13.750  -0.7175   0.06373   0.06068  -0.0686   1.0000   0.0072
 -13.500  -0.7498   0.05359   0.05035  -0.0759   1.0000   0.0070
 -13.250  -0.7657   0.04776   0.04435  -0.0798   1.0000   0.0071
 -13.000  -0.7840   0.04255   0.03898  -0.0828   1.0000   0.0071
 -12.750  -0.7939   0.03899   0.03527  -0.0841   1.0000   0.0072
 -12.500  -0.8078   0.03573   0.03189  -0.0843   1.0000   0.0071
 -12.250  -0.8200   0.03351   0.02955  -0.0828   1.0000   0.0072
 -12.000  -0.8119   0.03096   0.02682  -0.0853   0.9910   0.0072
 -11.750  -0.7974   0.02817   0.02379  -0.0883   0.9822   0.0074
 -11.500  -0.7781   0.02602   0.02145  -0.0904   0.9745   0.0075
 -11.250  -0.7546   0.02439   0.01967  -0.0922   0.9682   0.0077
 -11.000  -0.7307   0.02306   0.01820  -0.0934   0.9603   0.0079
 -10.750  -0.7058   0.02193   0.01695  -0.0943   0.9522   0.0082
 -10.500  -0.6810   0.02087   0.01573  -0.0951   0.9433   0.0084
 -10.250  -0.6579   0.01998   0.01473  -0.0952   0.9330   0.0086
 -10.000  -0.6343   0.01918   0.01380  -0.0952   0.9236   0.0090
  -9.750  -0.6114   0.01842   0.01290  -0.0950   0.9141   0.0093
  -9.500  -0.5892   0.01771   0.01205  -0.0945   0.9044   0.0095
  -9.250  -0.5665   0.01705   0.01125  -0.0940   0.8957   0.0098
  -9.000  -0.5448   0.01630   0.01038  -0.0934   0.8869   0.0101
  -8.750  -0.5222   0.01564   0.00962  -0.0929   0.8790   0.0105
  -8.500  -0.4986   0.01510   0.00899  -0.0924   0.8711   0.0108
  -8.250  -0.4745   0.01461   0.00840  -0.0920   0.8643   0.0113
  -8.000  -0.4500   0.01416   0.00786  -0.0916   0.8574   0.0118
  -7.750  -0.4251   0.01373   0.00732  -0.0912   0.8513   0.0125
  -7.500  -0.4001   0.01331   0.00683  -0.0909   0.8448   0.0133
  -7.250  -0.3750   0.01290   0.00637  -0.0906   0.8389   0.0148
  -7.000  -0.3495   0.01253   0.00598  -0.0903   0.8331   0.0173
  -6.750  -0.3235   0.01222   0.00565  -0.0901   0.8271   0.0214
  -6.500  -0.2972   0.01197   0.00536  -0.0899   0.8220   0.0257
  -6.250  -0.2706   0.01172   0.00507  -0.0898   0.8162   0.0287
  -6.000  -0.2440   0.01148   0.00482  -0.0896   0.8107   0.0320
  -5.750  -0.2171   0.01129   0.00456  -0.0895   0.8057   0.0344
  -5.500  -0.1903   0.01106   0.00429  -0.0894   0.8001   0.0371
  -5.250  -0.1634   0.01085   0.00407  -0.0893   0.7949   0.0406
  -5.000  -0.1360   0.01070   0.00388  -0.0892   0.7899   0.0443
  -4.750  -0.1091   0.01046   0.00366  -0.0892   0.7845   0.0498
  -4.500  -0.0818   0.01031   0.00345  -0.0891   0.7795   0.0545
  -4.250  -0.0545   0.01011   0.00323  -0.0890   0.7746   0.0601
  -4.000  -0.0271   0.00993   0.00305  -0.0890   0.7692   0.0662
  -3.750   0.0003   0.00977   0.00287  -0.0889   0.7642   0.0746
  -3.500   0.0277   0.00959   0.00270  -0.0889   0.7589   0.0871
  -3.250   0.0550   0.00940   0.00255  -0.0888   0.7530   0.1047
  -3.000   0.0822   0.00920   0.00239  -0.0888   0.7474   0.1306
  -2.750   0.1091   0.00892   0.00225  -0.0888   0.7405   0.1740
  -2.500   0.1359   0.00865   0.00211  -0.0887   0.7341   0.2263
  -2.250   0.1627   0.00833   0.00198  -0.0887   0.7280   0.2896
  -2.000   0.1879   0.00773   0.00186  -0.0887   0.7221   0.4347
  -1.750   0.2151   0.00759   0.00184  -0.0886   0.7167   0.4909
  -1.500   0.2429   0.00752   0.00184  -0.0885   0.7106   0.5228
  -1.250   0.2708   0.00751   0.00182  -0.0884   0.7048   0.5411
  -1.000   0.2987   0.00749   0.00182  -0.0884   0.6986   0.5623
  -0.750   0.3260   0.00748   0.00185  -0.0882   0.6907   0.5879
  -0.500   0.3537   0.00749   0.00185  -0.0881   0.6820   0.6009
  -0.250   0.3813   0.00753   0.00183  -0.0880   0.6726   0.6093
   0.000   0.4088   0.00755   0.00184  -0.0878   0.6628   0.6192
   0.250   0.4363   0.00758   0.00186  -0.0877   0.6545   0.6299
   0.500   0.4640   0.00762   0.00188  -0.0876   0.6463   0.6384
   0.750   0.4917   0.00765   0.00191  -0.0875   0.6384   0.6442
   1.000   0.5190   0.00771   0.00193  -0.0874   0.6289   0.6501
   1.500   0.5732   0.00783   0.00201  -0.0870   0.6029   0.6626
   1.750   0.5997   0.00792   0.00205  -0.0867   0.5872   0.6696
   2.000   0.6261   0.00801   0.00211  -0.0864   0.5720   0.6760
   2.250   0.6523   0.00812   0.00219  -0.0861   0.5558   0.6831
   2.500   0.6782   0.00825   0.00227  -0.0857   0.5396   0.6903
   2.750   0.7038   0.00839   0.00238  -0.0853   0.5203   0.6986
   3.000   0.7287   0.00857   0.00250  -0.0847   0.4988   0.7066
   3.250   0.7531   0.00878   0.00264  -0.0841   0.4760   0.7152
   3.500   0.7770   0.00902   0.00281  -0.0834   0.4518   0.7237
   3.750   0.8008   0.00928   0.00299  -0.0827   0.4274   0.7335
   4.250   0.8480   0.00977   0.00339  -0.0813   0.3850   0.7539
   4.500   0.8711   0.01005   0.00361  -0.0805   0.3626   0.7648
   4.750   0.8938   0.01034   0.00384  -0.0796   0.3388   0.7764
   5.000   0.9161   0.01063   0.00409  -0.0787   0.3176   0.7888
   5.250   0.9383   0.01092   0.00434  -0.0778   0.2994   0.8023
   5.500   0.9601   0.01120   0.00460  -0.0768   0.2817   0.8168
   5.750   0.9818   0.01146   0.00487  -0.0757   0.2673   0.8331
   6.250   1.0222   0.01189   0.00540  -0.0730   0.2412   0.8897
   6.500   1.0539   0.01217   0.00572  -0.0742   0.2250   1.0000
   6.750   1.0754   0.01253   0.00602  -0.0732   0.2110   1.0000
   7.000   1.0963   0.01291   0.00634  -0.0722   0.1976   1.0000
   7.500   1.1359   0.01374   0.00705  -0.0698   0.1706   1.0000
   7.750   1.1535   0.01420   0.00745  -0.0682   0.1562   1.0000
   8.000   1.1713   0.01459   0.00782  -0.0667   0.1457   1.0000
   8.250   1.1882   0.01502   0.00822  -0.0650   0.1359   1.0000
   8.500   1.2040   0.01551   0.00867  -0.0631   0.1246   1.0000
   8.750   1.2190   0.01606   0.00916  -0.0613   0.1125   1.0000
   9.000   1.2335   0.01664   0.00969  -0.0594   0.1008   1.0000
   9.250   1.2472   0.01729   0.01027  -0.0575   0.0881   1.0000
   9.500   1.2611   0.01794   0.01088  -0.0557   0.0774   1.0000
   9.750   1.2742   0.01866   0.01156  -0.0538   0.0669   1.0000
  10.000   1.2875   0.01937   0.01225  -0.0520   0.0589   1.0000
  10.250   1.2999   0.02016   0.01303  -0.0502   0.0518   1.0000
  10.500   1.3118   0.02101   0.01386  -0.0485   0.0447   1.0000
  10.750   1.3241   0.02186   0.01471  -0.0468   0.0391   1.0000
  11.000   1.3346   0.02284   0.01568  -0.0451   0.0334   1.0000
  11.250   1.3464   0.02377   0.01663  -0.0435   0.0294   1.0000
  11.500   1.3568   0.02482   0.01769  -0.0420   0.0255   1.0000
  11.750   1.3654   0.02603   0.01890  -0.0403   0.0204   1.0000
  12.000   1.3752   0.02718   0.02009  -0.0389   0.0171   1.0000
  12.250   1.3825   0.02856   0.02148  -0.0374   0.0129   1.0000
  12.500   1.3848   0.03039   0.02330  -0.0356   0.0062   1.0000
  12.750   1.3905   0.03201   0.02497  -0.0342   0.0052   1.0000
  13.000   1.3967   0.03363   0.02665  -0.0330   0.0046   1.0000
  13.250   1.4033   0.03526   0.02837  -0.0319   0.0043   1.0000
  13.500   1.4094   0.03697   0.03017  -0.0309   0.0042   1.0000
  13.750   1.4128   0.03900   0.03229  -0.0299   0.0039   1.0000
  14.000   1.4163   0.04107   0.03447  -0.0291   0.0037   1.0000
  14.250   1.4214   0.04306   0.03656  -0.0285   0.0037   1.0000
  14.500   1.4235   0.04543   0.03904  -0.0279   0.0036   1.0000
  14.750   1.4240   0.04807   0.04179  -0.0275   0.0035   1.0000
  15.000   1.4223   0.05106   0.04490  -0.0272   0.0033   1.0000
  15.250   1.4227   0.05393   0.04788  -0.0272   0.0033   1.0000
  15.500   1.4227   0.05694   0.05100  -0.0274   0.0033   1.0000
  15.750   1.4204   0.06034   0.05454  -0.0278   0.0033   1.0000
  16.000   1.4176   0.06395   0.05827  -0.0284   0.0032   1.0000
  16.250   1.4135   0.06789   0.06234  -0.0293   0.0032   1.0000
  16.500   1.4089   0.07204   0.06661  -0.0304   0.0032   1.0000
  16.750   1.4011   0.07680   0.07152  -0.0319   0.0031   1.0000
  17.000   1.3934   0.08174   0.07660  -0.0336   0.0031   1.0000
  17.250   1.3839   0.08714   0.08213  -0.0357   0.0030   1.0000
  17.500   1.3728   0.09296   0.08810  -0.0381   0.0030   1.0000
  17.750   1.3604   0.09918   0.09447  -0.0409   0.0030   1.0000
  18.000   1.3498   0.10521   0.10064  -0.0437   0.0030   1.0000
  18.250   1.3350   0.11218   0.10776  -0.0471   0.0029   1.0000
  18.500   1.3222   0.11890   0.11462  -0.0505   0.0030   1.0000
  18.750   1.3075   0.12613   0.12199  -0.0543   0.0029   1.0000
  19.000   1.2928   0.13348   0.12947  -0.0583   0.0030   1.0000
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