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HQ 1.5/12 AIRFOIL (hq1512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 1.5/12 AIRFOIL (hq1512-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.92 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq1512-il-1000000.txt
Download as CSV file: xf-hq1512-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.5/12 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8208   0.10024   0.09813  -0.0251   1.0000   0.0068
 -15.500  -0.8530   0.08928   0.08705  -0.0311   1.0000   0.0067
 -15.250  -0.8708   0.08131   0.07898  -0.0358   1.0000   0.0067
 -15.000  -0.8762   0.07583   0.07344  -0.0391   1.0000   0.0066
 -14.750  -0.9190   0.06340   0.06077  -0.0474   1.0000   0.0067
 -14.500  -0.9079   0.06128   0.05864  -0.0488   1.0000   0.0066
 -14.250  -0.9456   0.05157   0.04869  -0.0552   1.0000   0.0065
 -14.000  -0.9540   0.04696   0.04394  -0.0580   1.0000   0.0066
 -13.750  -0.9504   0.04434   0.04125  -0.0595   1.0000   0.0066
 -13.500  -0.9900   0.03687   0.03345  -0.0623   1.0000   0.0067
 -13.250  -1.0079   0.03267   0.02904  -0.0628   1.0000   0.0069
 -13.000  -1.0112   0.03029   0.02654  -0.0623   1.0000   0.0070
 -12.750  -1.0102   0.02858   0.02474  -0.0614   1.0000   0.0072
 -12.500  -1.0147   0.02669   0.02269  -0.0592   1.0000   0.0071
 -12.250  -1.0090   0.02592   0.02188  -0.0569   1.0000   0.0074
 -12.000  -1.0032   0.02496   0.02085  -0.0545   1.0000   0.0075
 -11.750  -0.9917   0.02409   0.01991  -0.0528   1.0000   0.0077
 -11.500  -0.9817   0.02297   0.01868  -0.0509   1.0000   0.0078
 -11.250  -0.9692   0.02201   0.01763  -0.0491   1.0000   0.0080
 -11.000  -0.9540   0.02129   0.01684  -0.0476   1.0000   0.0083
 -10.750  -0.9395   0.02047   0.01593  -0.0459   1.0000   0.0085
 -10.500  -0.9238   0.01978   0.01517  -0.0442   1.0000   0.0088
 -10.250  -0.9096   0.01905   0.01434  -0.0423   1.0000   0.0089
 -10.000  -0.8926   0.01858   0.01381  -0.0407   0.9998   0.0091
  -9.750  -0.8645   0.01676   0.01182  -0.0423   0.9960   0.0097
  -9.500  -0.8334   0.01589   0.01090  -0.0438   0.9917   0.0102
  -9.250  -0.8013   0.01531   0.01029  -0.0452   0.9872   0.0108
  -9.000  -0.7674   0.01471   0.00962  -0.0470   0.9838   0.0113
  -8.750  -0.7343   0.01421   0.00907  -0.0484   0.9785   0.0119
  -8.500  -0.7001   0.01389   0.00871  -0.0500   0.9723   0.0124
  -8.250  -0.6719   0.01274   0.00746  -0.0509   0.9620   0.0137
  -8.000  -0.6424   0.01231   0.00699  -0.0515   0.9501   0.0145
  -7.750  -0.6160   0.01193   0.00654  -0.0514   0.9355   0.0154
  -7.500  -0.5909   0.01162   0.00615  -0.0509   0.9214   0.0161
  -7.250  -0.5670   0.01120   0.00562  -0.0502   0.9088   0.0170
  -7.000  -0.5431   0.01077   0.00513  -0.0495   0.8973   0.0188
  -6.750  -0.5176   0.01052   0.00484  -0.0491   0.8873   0.0204
  -6.500  -0.4917   0.01031   0.00456  -0.0488   0.8783   0.0216
  -6.250  -0.4671   0.00989   0.00410  -0.0482   0.8691   0.0254
  -6.000  -0.4410   0.00964   0.00381  -0.0479   0.8610   0.0293
  -5.750  -0.4153   0.00937   0.00353  -0.0475   0.8530   0.0361
  -5.500  -0.3892   0.00908   0.00326  -0.0473   0.8453   0.0458
  -5.250  -0.3631   0.00883   0.00303  -0.0470   0.8378   0.0568
  -5.000  -0.3365   0.00859   0.00282  -0.0468   0.8305   0.0701
  -4.750  -0.3103   0.00833   0.00261  -0.0466   0.8232   0.0899
  -4.250  -0.2571   0.00783   0.00224  -0.0462   0.8088   0.1375
  -4.000  -0.2306   0.00756   0.00207  -0.0461   0.8018   0.1707
  -3.750  -0.2042   0.00727   0.00191  -0.0459   0.7945   0.2128
  -3.500  -0.1779   0.00696   0.00176  -0.0457   0.7875   0.2605
  -3.250  -0.1519   0.00661   0.00159  -0.0455   0.7802   0.3187
  -3.000  -0.1261   0.00621   0.00144  -0.0453   0.7732   0.3979
  -2.750  -0.0997   0.00593   0.00134  -0.0451   0.7659   0.4620
  -2.500  -0.0727   0.00576   0.00128  -0.0450   0.7589   0.5083
  -2.250  -0.0452   0.00566   0.00123  -0.0448   0.7505   0.5409
  -2.000  -0.0174   0.00560   0.00120  -0.0448   0.7423   0.5669
  -1.750   0.0104   0.00556   0.00117  -0.0447   0.7342   0.5871
  -1.500   0.0386   0.00553   0.00115  -0.0447   0.7264   0.6021
  -1.250   0.0667   0.00553   0.00113  -0.0446   0.7190   0.6150
  -1.000   0.0951   0.00553   0.00112  -0.0447   0.7111   0.6264
  -0.750   0.1231   0.00553   0.00111  -0.0446   0.7035   0.6390
  -0.500   0.1514   0.00552   0.00111  -0.0446   0.6958   0.6499
  -0.250   0.1796   0.00555   0.00111  -0.0446   0.6874   0.6591
   0.000   0.2078   0.00555   0.00112  -0.0446   0.6782   0.6691
   0.250   0.2359   0.00557   0.00113  -0.0445   0.6704   0.6786
   0.750   0.2923   0.00560   0.00117  -0.0445   0.6536   0.6959
   1.000   0.3204   0.00565   0.00119  -0.0445   0.6444   0.7039
   1.250   0.3485   0.00566   0.00122  -0.0445   0.6355   0.7120
   1.500   0.3765   0.00570   0.00125  -0.0444   0.6254   0.7199
   1.750   0.4042   0.00574   0.00129  -0.0444   0.6136   0.7270
   2.000   0.4323   0.00580   0.00133  -0.0443   0.6012   0.7335
   2.250   0.4599   0.00584   0.00137  -0.0442   0.5868   0.7402
   2.500   0.4873   0.00594   0.00142  -0.0441   0.5698   0.7473
   2.750   0.5144   0.00602   0.00149  -0.0439   0.5490   0.7542
   3.000   0.5411   0.00618   0.00157  -0.0437   0.5220   0.7619
   3.250   0.5668   0.00637   0.00167  -0.0433   0.4874   0.7695
   3.500   0.5919   0.00666   0.00181  -0.0428   0.4444   0.7779
   3.750   0.6152   0.00706   0.00200  -0.0421   0.3851   0.7864
   4.000   0.6385   0.00750   0.00221  -0.0414   0.3266   0.7952
   4.250   0.6628   0.00785   0.00241  -0.0409   0.2903   0.8049
   4.500   0.6882   0.00806   0.00259  -0.0405   0.2705   0.8147
   4.750   0.7139   0.00824   0.00276  -0.0401   0.2556   0.8255
   5.000   0.7395   0.00842   0.00293  -0.0397   0.2427   0.8376
   5.500   0.7894   0.00874   0.00329  -0.0387   0.2167   0.8680
   5.750   0.8132   0.00887   0.00346  -0.0379   0.2026   0.8930
   6.000   0.8398   0.00898   0.00366  -0.0377   0.1869   0.9484
   6.250   0.8791   0.00936   0.00394  -0.0406   0.1592   1.0000
   6.500   0.9019   0.00980   0.00422  -0.0399   0.1313   1.0000
   6.750   0.9240   0.01030   0.00457  -0.0390   0.1040   1.0000
   7.000   0.9458   0.01081   0.00495  -0.0382   0.0815   1.0000
   7.250   0.9683   0.01126   0.00532  -0.0374   0.0662   1.0000
   7.500   0.9908   0.01171   0.00569  -0.0367   0.0552   1.0000
   7.750   1.0146   0.01203   0.00601  -0.0361   0.0507   1.0000
   8.000   1.0366   0.01250   0.00644  -0.0352   0.0443   1.0000
   8.250   1.0607   0.01276   0.00673  -0.0347   0.0423   1.0000
   8.500   1.0835   0.01312   0.00709  -0.0340   0.0393   1.0000
   8.750   1.1048   0.01360   0.00755  -0.0331   0.0354   1.0000
   9.000   1.1277   0.01393   0.00791  -0.0324   0.0341   1.0000
   9.250   1.1506   0.01423   0.00824  -0.0317   0.0325   1.0000
   9.500   1.1723   0.01461   0.00864  -0.0309   0.0307   1.0000
   9.750   1.1927   0.01507   0.00909  -0.0298   0.0284   1.0000
  10.000   1.2126   0.01553   0.00958  -0.0287   0.0265   1.0000
  10.250   1.2342   0.01585   0.00993  -0.0279   0.0256   1.0000
  10.500   1.2548   0.01620   0.01030  -0.0269   0.0239   1.0000
  10.750   1.2736   0.01665   0.01075  -0.0257   0.0224   1.0000
  11.000   1.2895   0.01715   0.01127  -0.0239   0.0203   1.0000
  11.250   1.3062   0.01753   0.01169  -0.0223   0.0191   1.0000
  11.500   1.3197   0.01809   0.01221  -0.0203   0.0158   1.0000
  11.750   1.3318   0.01874   0.01286  -0.0181   0.0123   1.0000
  12.000   1.3406   0.01961   0.01371  -0.0157   0.0083   1.0000
  12.250   1.3487   0.02057   0.01469  -0.0133   0.0064   1.0000
  12.500   1.3587   0.02145   0.01562  -0.0112   0.0058   1.0000
  12.750   1.3677   0.02243   0.01666  -0.0093   0.0053   1.0000
  13.000   1.3764   0.02346   0.01777  -0.0075   0.0051   1.0000
  13.250   1.3830   0.02470   0.01909  -0.0056   0.0047   1.0000
  13.500   1.3888   0.02606   0.02053  -0.0038   0.0045   1.0000
  13.750   1.3933   0.02757   0.02214  -0.0022   0.0043   1.0000
  14.000   1.3999   0.02898   0.02363  -0.0009   0.0043   1.0000
  14.250   1.4035   0.03069   0.02545   0.0005   0.0042   1.0000
  14.500   1.4092   0.03230   0.02714   0.0015   0.0041   1.0000
  14.750   1.4117   0.03426   0.02920   0.0024   0.0041   1.0000
  15.000   1.4134   0.03637   0.03141   0.0032   0.0040   1.0000
  15.250   1.4148   0.03861   0.03375   0.0037   0.0040   1.0000
  15.500   1.4120   0.04138   0.03664   0.0041   0.0039   1.0000
  15.750   1.4098   0.04421   0.03958   0.0042   0.0039   1.0000
  16.000   1.4046   0.04752   0.04302   0.0040   0.0038   1.0000
  16.250   1.4009   0.05083   0.04644   0.0035   0.0037   1.0000
  16.500   1.3919   0.05502   0.05076   0.0025   0.0038   1.0000
  16.750   1.3869   0.05889   0.05473   0.0014   0.0037   1.0000
  17.000   1.3734   0.06422   0.06021  -0.0006   0.0037   1.0000
  17.250   1.3600   0.06983   0.06596  -0.0030   0.0037   1.0000
  17.500   1.3451   0.07602   0.07228  -0.0058   0.0037   1.0000
  17.750   1.3305   0.08243   0.07883  -0.0090   0.0037   1.0000
  18.000   1.3103   0.09009   0.08664  -0.0130   0.0037   1.0000
  18.250   1.2910   0.09791   0.09461  -0.0171   0.0037   1.0000
  18.500   1.2665   0.10695   0.10380  -0.0221   0.0038   1.0000
  18.750   1.2466   0.11525   0.11223  -0.0267   0.0037   1.0000
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