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HQ 1.0/12 AIRFOIL (hq1012-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: HQ 1.0/12 AIRFOIL (hq1012-il)
Reynolds number: 500,000
Max Cl/Cd: 75.56 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq1012-il-500000.txt
Download as CSV file: xf-hq1012-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.0/12 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8407   0.08454   0.08171  -0.0297   1.0000   0.0102
 -14.500  -0.8657   0.07486   0.07183  -0.0363   1.0000   0.0101
 -14.250  -0.8851   0.06721   0.06400  -0.0415   1.0000   0.0100
 -14.000  -0.9092   0.05968   0.05630  -0.0463   1.0000   0.0102
 -13.750  -0.9238   0.05425   0.05070  -0.0495   1.0000   0.0102
 -13.500  -0.9358   0.04960   0.04586  -0.0517   1.0000   0.0101
 -13.250  -0.9516   0.04490   0.04099  -0.0534   1.0000   0.0102
 -13.000  -0.9569   0.04176   0.03768  -0.0540   1.0000   0.0101
 -12.750  -0.9664   0.03839   0.03417  -0.0542   1.0000   0.0104
 -12.500  -0.9682   0.03605   0.03172  -0.0538   1.0000   0.0105
 -12.250  -0.9696   0.03391   0.02946  -0.0529   1.0000   0.0107
 -12.000  -0.9674   0.03232   0.02778  -0.0518   1.0000   0.0109
 -11.750  -0.9658   0.03079   0.02614  -0.0501   1.0000   0.0112
 -11.500  -0.9629   0.02955   0.02478  -0.0478   1.0000   0.0115
 -11.250  -0.9591   0.02827   0.02338  -0.0453   1.0000   0.0118
 -11.000  -0.9508   0.02685   0.02180  -0.0433   1.0000   0.0121
 -10.750  -0.9402   0.02549   0.02028  -0.0415   1.0000   0.0125
 -10.500  -0.9276   0.02423   0.01886  -0.0398   1.0000   0.0128
 -10.250  -0.9130   0.02316   0.01765  -0.0383   1.0000   0.0131
 -10.000  -0.9036   0.02137   0.01571  -0.0361   1.0000   0.0136
  -9.750  -0.8905   0.02018   0.01445  -0.0343   1.0000   0.0142
  -9.500  -0.8741   0.01942   0.01365  -0.0328   1.0000   0.0149
  -9.250  -0.8574   0.01870   0.01288  -0.0312   1.0000   0.0157
  -9.000  -0.8412   0.01799   0.01209  -0.0294   1.0000   0.0165
  -8.750  -0.8244   0.01745   0.01147  -0.0276   1.0000   0.0173
  -8.500  -0.8160   0.01643   0.01042  -0.0247   1.0000   0.0188
  -8.250  -0.7906   0.01600   0.00999  -0.0248   0.9981   0.0209
  -8.000  -0.7549   0.01522   0.00913  -0.0270   0.9936   0.0236
  -7.750  -0.7207   0.01456   0.00848  -0.0288   0.9881   0.0278
  -7.500  -0.6850   0.01383   0.00773  -0.0310   0.9838   0.0333
  -7.250  -0.6485   0.01360   0.00746  -0.0330   0.9788   0.0381
  -7.000  -0.6144   0.01293   0.00681  -0.0348   0.9723   0.0447
  -6.750  -0.5793   0.01263   0.00645  -0.0365   0.9653   0.0490
  -6.500  -0.5470   0.01206   0.00589  -0.0378   0.9565   0.0559
  -6.250  -0.5167   0.01180   0.00556  -0.0384   0.9452   0.0605
  -6.000  -0.4901   0.01131   0.00509  -0.0383   0.9329   0.0690
  -5.750  -0.4643   0.01096   0.00472  -0.0380   0.9211   0.0780
  -5.500  -0.4393   0.01064   0.00437  -0.0374   0.9102   0.0893
  -5.250  -0.4153   0.01026   0.00404  -0.0367   0.8989   0.1074
  -5.000  -0.3914   0.00985   0.00372  -0.0361   0.8886   0.1373
  -4.750  -0.3674   0.00943   0.00346  -0.0355   0.8793   0.1826
  -4.500  -0.3429   0.00907   0.00322  -0.0350   0.8699   0.2268
  -4.250  -0.3182   0.00871   0.00299  -0.0346   0.8614   0.2711
  -4.000  -0.2943   0.00826   0.00275  -0.0340   0.8532   0.3321
  -3.750  -0.2703   0.00781   0.00257  -0.0335   0.8449   0.4084
  -3.500  -0.2455   0.00751   0.00243  -0.0329   0.8375   0.4718
  -3.250  -0.2198   0.00730   0.00237  -0.0325   0.8295   0.5222
  -3.000  -0.1934   0.00720   0.00232  -0.0321   0.8226   0.5589
  -2.750  -0.1662   0.00714   0.00228  -0.0319   0.8147   0.5842
  -2.500  -0.1391   0.00712   0.00224  -0.0316   0.8078   0.6040
  -2.250  -0.1117   0.00709   0.00222  -0.0314   0.8002   0.6231
  -2.000  -0.0842   0.00710   0.00219  -0.0311   0.7935   0.6406
  -1.750  -0.0566   0.00710   0.00219  -0.0309   0.7865   0.6555
  -1.500  -0.0291   0.00710   0.00218  -0.0307   0.7793   0.6700
  -1.250  -0.0016   0.00709   0.00217  -0.0304   0.7710   0.6808
  -1.000   0.0261   0.00710   0.00212  -0.0303   0.7627   0.6899
  -0.750   0.0538   0.00709   0.00211  -0.0301   0.7540   0.6986
  -0.500   0.0815   0.00710   0.00209  -0.0299   0.7468   0.7076
  -0.250   0.1094   0.00711   0.00209  -0.0298   0.7383   0.7176
   0.000   0.1369   0.00711   0.00209  -0.0296   0.7304   0.7261
   0.250   0.1647   0.00711   0.00210  -0.0294   0.7218   0.7349
   0.500   0.1923   0.00712   0.00211  -0.0292   0.7131   0.7439
   0.750   0.2198   0.00713   0.00211  -0.0290   0.7042   0.7526
   1.000   0.2477   0.00714   0.00213  -0.0289   0.6957   0.7612
   1.250   0.2752   0.00715   0.00214  -0.0287   0.6878   0.7678
   1.500   0.3031   0.00716   0.00217  -0.0286   0.6778   0.7754
   1.750   0.3306   0.00716   0.00219  -0.0285   0.6685   0.7822
   2.000   0.3581   0.00720   0.00222  -0.0283   0.6585   0.7901
   2.250   0.3854   0.00720   0.00225  -0.0281   0.6467   0.7974
   2.500   0.4128   0.00723   0.00229  -0.0279   0.6339   0.8060
   2.750   0.4395   0.00724   0.00233  -0.0275   0.6189   0.8138
   3.000   0.4663   0.00729   0.00237  -0.0272   0.6017   0.8228
   3.250   0.4925   0.00734   0.00242  -0.0268   0.5824   0.8315
   3.500   0.5184   0.00741   0.00248  -0.0263   0.5580   0.8409
   3.750   0.5434   0.00756   0.00255  -0.0257   0.5243   0.8516
   4.000   0.5673   0.00774   0.00266  -0.0249   0.4852   0.8625
   4.250   0.5906   0.00799   0.00280  -0.0240   0.4438   0.8749
   4.500   0.6128   0.00831   0.00299  -0.0229   0.3961   0.8902
   4.750   0.6348   0.00865   0.00321  -0.0218   0.3497   0.9093
   5.000   0.6598   0.00900   0.00346  -0.0214   0.3095   0.9349
   5.250   0.6944   0.00943   0.00377  -0.0232   0.2772   0.9629
   5.500   0.7342   0.00980   0.00407  -0.0261   0.2530   0.9872
   5.750   0.7653   0.01015   0.00434  -0.0272   0.2341   1.0000
   6.000   0.7885   0.01045   0.00458  -0.0265   0.2181   1.0000
   6.250   0.8123   0.01075   0.00484  -0.0259   0.2002   1.0000
   6.500   0.8357   0.01110   0.00511  -0.0253   0.1779   1.0000
   6.750   0.8583   0.01152   0.00542  -0.0246   0.1531   1.0000
   7.000   0.8800   0.01203   0.00579  -0.0238   0.1277   1.0000
   7.250   0.9014   0.01257   0.00622  -0.0229   0.1077   1.0000
   7.500   0.9230   0.01309   0.00667  -0.0220   0.0932   1.0000
   7.750   0.9450   0.01357   0.00712  -0.0212   0.0823   1.0000
   8.000   0.9670   0.01403   0.00758  -0.0204   0.0736   1.0000
   8.250   0.9879   0.01458   0.00809  -0.0195   0.0654   1.0000
   8.500   1.0096   0.01504   0.00855  -0.0186   0.0581   1.0000
   8.750   1.0309   0.01552   0.00905  -0.0178   0.0521   1.0000
   9.000   1.0513   0.01606   0.00957  -0.0168   0.0464   1.0000
   9.250   1.0721   0.01654   0.01008  -0.0158   0.0413   1.0000
   9.500   1.0912   0.01714   0.01066  -0.0147   0.0363   1.0000
   9.750   1.1106   0.01769   0.01125  -0.0136   0.0320   1.0000
  10.000   1.1267   0.01845   0.01200  -0.0121   0.0274   1.0000
  10.250   1.1446   0.01903   0.01264  -0.0107   0.0240   1.0000
  10.500   1.1551   0.02000   0.01360  -0.0084   0.0203   1.0000
  10.750   1.1686   0.02065   0.01433  -0.0064   0.0182   1.0000
  11.000   1.1764   0.02165   0.01534  -0.0038   0.0161   1.0000
  11.250   1.1828   0.02276   0.01655  -0.0011   0.0146   1.0000
  11.500   1.1929   0.02369   0.01755   0.0008   0.0135   1.0000
  11.750   1.2004   0.02483   0.01874   0.0028   0.0123   1.0000
  12.000   1.1997   0.02658   0.02058   0.0053   0.0117   1.0000
  12.250   1.2061   0.02794   0.02205   0.0069   0.0111   1.0000
  12.500   1.2116   0.02944   0.02367   0.0084   0.0107   1.0000
  12.750   1.2154   0.03115   0.02548   0.0097   0.0106   1.0000
  13.000   1.2199   0.03288   0.02731   0.0108   0.0099   1.0000
  13.250   1.2218   0.03492   0.02945   0.0118   0.0096   1.0000
  13.500   1.2248   0.03694   0.03154   0.0124   0.0093   1.0000
  13.750   1.2237   0.03946   0.03417   0.0130   0.0092   1.0000
  14.000   1.2212   0.04224   0.03706   0.0133   0.0090   1.0000
  14.250   1.2173   0.04532   0.04025   0.0132   0.0089   1.0000
  14.500   1.2086   0.04908   0.04413   0.0130   0.0087   1.0000
  14.750   1.1934   0.05386   0.04907   0.0122   0.0084   1.0000
  15.000   1.1878   0.05767   0.05302   0.0112   0.0084   1.0000
  15.250   1.1827   0.06169   0.05719   0.0098   0.0083   1.0000
  15.500   1.1759   0.06613   0.06178   0.0081   0.0083   1.0000
  15.750   1.1668   0.07114   0.06694   0.0060   0.0083   1.0000
  16.000   1.1581   0.07641   0.07236   0.0034   0.0082   1.0000
  16.250   1.1472   0.08214   0.07824   0.0006   0.0082   1.0000
  16.500   1.1347   0.08851   0.08476  -0.0028   0.0082   1.0000
  16.750   1.1220   0.09507   0.09147  -0.0064   0.0082   1.0000
  17.000   1.1078   0.10222   0.09877  -0.0104   0.0081   1.0000
  17.250   1.0939   0.10954   0.10623  -0.0146   0.0081   1.0000
  17.500   1.0779   0.11734   0.11417  -0.0190   0.0082   1.0000
  17.750   1.0628   0.12530   0.12226  -0.0237   0.0082   1.0000
  18.000   1.0446   0.13422   0.13133  -0.0291   0.0082   1.0000
  18.250   1.0285   0.14289   0.14012  -0.0343   0.0082   1.0000
  18.500   1.0090   0.15264   0.14999  -0.0401   0.0083   1.0000
  18.750   0.9834   0.16449   0.16199  -0.0472   0.0084   1.0000
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