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HQ 3.0/15 AIRFOIL (hq3015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/15 AIRFOIL (hq3015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.53 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3015-il-1000000-n5.txt
Download as CSV file: xf-hq3015-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7819   0.10658   0.10399  -0.0519   1.0000   0.0066
 -17.500  -0.8786   0.08544   0.08255  -0.0636   1.0000   0.0064
 -17.250  -0.9367   0.07136   0.06822  -0.0719   1.0000   0.0063
 -17.000  -0.9718   0.06152   0.05817  -0.0781   1.0000   0.0062
 -16.750  -0.9935   0.05474   0.05124  -0.0823   1.0000   0.0062
 -16.500  -1.0105   0.04925   0.04562  -0.0855   1.0000   0.0063
 -16.250  -1.0228   0.04476   0.04101  -0.0877   1.0000   0.0063
 -16.000  -1.0287   0.04131   0.03746  -0.0892   1.0000   0.0064
 -15.750  -1.0335   0.03817   0.03422  -0.0903   1.0000   0.0064
 -15.500  -1.0379   0.03526   0.03121  -0.0910   1.0000   0.0064
 -15.250  -1.0377   0.03298   0.02885  -0.0913   1.0000   0.0065
 -15.000  -1.0369   0.03090   0.02669  -0.0912   1.0000   0.0066
 -14.750  -1.0359   0.02901   0.02472  -0.0908   1.0000   0.0066
 -14.500  -1.0333   0.02745   0.02309  -0.0900   1.0000   0.0067
 -14.250  -1.0224   0.02581   0.02138  -0.0905   0.9902   0.0068
 -14.000  -0.9992   0.02424   0.01972  -0.0932   0.9820   0.0069
 -13.750  -0.9709   0.02292   0.01831  -0.0963   0.9743   0.0071
 -13.500  -0.9389   0.02162   0.01692  -0.1000   0.9668   0.0073
 -13.000  -0.8815   0.01956   0.01465  -0.1048   0.9330   0.0076
 -12.750  -0.8683   0.01890   0.01384  -0.1034   0.9110   0.0077
 -12.500  -0.8573   0.01839   0.01321  -0.1012   0.8963   0.0078
 -12.250  -0.8424   0.01785   0.01257  -0.0997   0.8851   0.0079
 -12.000  -0.8277   0.01722   0.01185  -0.0981   0.8752   0.0082
 -11.750  -0.8103   0.01668   0.01123  -0.0969   0.8663   0.0084
 -11.500  -0.7917   0.01618   0.01066  -0.0958   0.8592   0.0087
 -11.250  -0.7719   0.01570   0.01012  -0.0948   0.8523   0.0091
 -11.000  -0.7514   0.01526   0.00961  -0.0939   0.8460   0.0095
 -10.750  -0.7295   0.01484   0.00913  -0.0933   0.8399   0.0098
 -10.500  -0.7073   0.01446   0.00868  -0.0926   0.8337   0.0102
 -10.250  -0.6854   0.01401   0.00819  -0.0919   0.8284   0.0111
 -10.000  -0.6624   0.01360   0.00776  -0.0913   0.8225   0.0122
  -9.750  -0.6392   0.01324   0.00734  -0.0907   0.8166   0.0135
  -9.500  -0.6156   0.01285   0.00694  -0.0903   0.8115   0.0155
  -9.250  -0.5913   0.01251   0.00659  -0.0898   0.8059   0.0182
  -9.000  -0.5667   0.01222   0.00629  -0.0895   0.8004   0.0208
  -8.750  -0.5412   0.01197   0.00601  -0.0892   0.7952   0.0230
  -8.500  -0.5153   0.01175   0.00575  -0.0889   0.7896   0.0242
  -8.250  -0.4899   0.01149   0.00547  -0.0886   0.7844   0.0258
  -8.000  -0.4638   0.01126   0.00522  -0.0884   0.7795   0.0274
  -7.750  -0.4374   0.01106   0.00498  -0.0883   0.7739   0.0286
  -7.500  -0.4110   0.01089   0.00475  -0.0881   0.7687   0.0294
  -7.250  -0.3847   0.01065   0.00450  -0.0879   0.7640   0.0310
  -7.000  -0.3580   0.01044   0.00428  -0.0878   0.7587   0.0324
  -6.750  -0.3314   0.01026   0.00407  -0.0876   0.7536   0.0341
  -6.500  -0.3042   0.01011   0.00388  -0.0875   0.7490   0.0355
  -6.250  -0.2774   0.00989   0.00368  -0.0874   0.7439   0.0387
  -6.000  -0.2504   0.00973   0.00350  -0.0873   0.7387   0.0410
  -5.750  -0.2231   0.00959   0.00332  -0.0872   0.7341   0.0428
  -5.500  -0.1958   0.00940   0.00314  -0.0872   0.7291   0.0464
  -5.250  -0.1685   0.00925   0.00299  -0.0871   0.7239   0.0501
  -5.000  -0.1410   0.00913   0.00283  -0.0871   0.7191   0.0536
  -4.750  -0.1134   0.00896   0.00268  -0.0871   0.7142   0.0583
  -4.500  -0.0857   0.00885   0.00255  -0.0870   0.7087   0.0621
  -4.250  -0.0584   0.00871   0.00242  -0.0870   0.7033   0.0689
  -4.000  -0.0306   0.00859   0.00229  -0.0870   0.6972   0.0753
  -3.750  -0.0032   0.00846   0.00218  -0.0869   0.6910   0.0851
  -3.500   0.0244   0.00833   0.00207  -0.0869   0.6858   0.0972
  -3.250   0.0522   0.00818   0.00196  -0.0870   0.6807   0.1127
  -3.000   0.0795   0.00802   0.00185  -0.0869   0.6757   0.1350
  -2.750   0.1069   0.00784   0.00176  -0.0869   0.6711   0.1648
  -2.500   0.1344   0.00763   0.00167  -0.0870   0.6663   0.2011
  -2.250   0.1615   0.00743   0.00158  -0.0870   0.6610   0.2431
  -2.000   0.1885   0.00721   0.00149  -0.0869   0.6550   0.2902
  -1.750   0.2142   0.00677   0.00137  -0.0868   0.6479   0.3885
  -1.500   0.2410   0.00661   0.00133  -0.0867   0.6408   0.4448
  -1.250   0.2690   0.00654   0.00131  -0.0867   0.6330   0.4717
  -1.000   0.2966   0.00652   0.00131  -0.0867   0.6254   0.4956
  -0.750   0.3245   0.00646   0.00132  -0.0867   0.6173   0.5257
  -0.500   0.3520   0.00646   0.00134  -0.0866   0.6086   0.5463
  -0.250   0.3803   0.00647   0.00135  -0.0866   0.6005   0.5585
   0.000   0.4081   0.00650   0.00137  -0.0866   0.5934   0.5670
   0.250   0.4364   0.00654   0.00139  -0.0866   0.5851   0.5741
   0.500   0.4640   0.00659   0.00142  -0.0866   0.5758   0.5814
   0.750   0.4917   0.00665   0.00145  -0.0865   0.5657   0.5892
   1.000   0.5190   0.00671   0.00150  -0.0864   0.5535   0.5977
   1.250   0.5456   0.00683   0.00156  -0.0861   0.5363   0.6067
   1.500   0.5716   0.00696   0.00163  -0.0858   0.5175   0.6139
   1.750   0.5982   0.00709   0.00170  -0.0855   0.5018   0.6199
   2.000   0.6245   0.00723   0.00178  -0.0853   0.4857   0.6250
   2.250   0.6504   0.00738   0.00188  -0.0849   0.4674   0.6302
   2.500   0.6762   0.00754   0.00198  -0.0846   0.4501   0.6355
   2.750   0.7020   0.00772   0.00209  -0.0842   0.4334   0.6400
   3.000   0.7271   0.00790   0.00222  -0.0837   0.4147   0.6448
   3.250   0.7517   0.00812   0.00236  -0.0832   0.3944   0.6501
   3.500   0.7762   0.00835   0.00251  -0.0826   0.3744   0.6552
   3.750   0.8003   0.00858   0.00267  -0.0820   0.3532   0.6605
   4.000   0.8240   0.00883   0.00284  -0.0813   0.3322   0.6663
   4.250   0.8471   0.00912   0.00303  -0.0806   0.3111   0.6716
   4.500   0.8709   0.00934   0.00321  -0.0799   0.2967   0.6771
   4.750   0.8949   0.00955   0.00339  -0.0793   0.2847   0.6834
   5.250   0.9424   0.00996   0.00376  -0.0779   0.2632   0.6952
   5.500   0.9654   0.01019   0.00396  -0.0771   0.2527   0.7019
   5.750   0.9893   0.01036   0.00414  -0.0765   0.2449   0.7081
   6.000   1.0117   0.01059   0.00436  -0.0756   0.2353   0.7149
   6.500   1.0555   0.01105   0.00479  -0.0736   0.2150   0.7286
   6.750   1.0758   0.01134   0.00504  -0.0724   0.2034   0.7363
   7.000   1.0941   0.01160   0.00529  -0.0707   0.1931   0.7439
   7.250   1.1122   0.01184   0.00553  -0.0690   0.1842   0.7518
   7.500   1.1287   0.01215   0.00582  -0.0671   0.1746   0.7600
   8.000   1.1620   0.01279   0.00646  -0.0633   0.1572   0.7792
   8.250   1.1764   0.01321   0.00685  -0.0612   0.1457   0.7893
   8.500   1.1924   0.01358   0.00722  -0.0593   0.1378   0.8007
   8.750   1.2087   0.01391   0.00759  -0.0576   0.1322   0.8145
   9.000   1.2229   0.01432   0.00802  -0.0555   0.1236   0.8313
   9.250   1.2361   0.01472   0.00847  -0.0533   0.1151   0.8561
   9.750   1.2760   0.01568   0.00957  -0.0521   0.0967   1.0000
  10.000   1.2911   0.01623   0.01010  -0.0505   0.0903   1.0000
  10.250   1.3036   0.01693   0.01076  -0.0487   0.0818   1.0000
  10.500   1.3160   0.01766   0.01145  -0.0469   0.0734   1.0000
  10.750   1.3281   0.01844   0.01220  -0.0452   0.0655   1.0000
  11.000   1.3393   0.01930   0.01302  -0.0434   0.0583   1.0000
  11.250   1.3502   0.02020   0.01389  -0.0418   0.0517   1.0000
  11.500   1.3616   0.02110   0.01478  -0.0402   0.0458   1.0000
  11.750   1.3707   0.02217   0.01582  -0.0385   0.0393   1.0000
  12.250   1.3922   0.02421   0.01785  -0.0356   0.0316   1.0000
  12.500   1.4016   0.02535   0.01900  -0.0342   0.0282   1.0000
  12.750   1.4123   0.02643   0.02010  -0.0330   0.0255   1.0000
  13.000   1.4188   0.02786   0.02152  -0.0315   0.0206   1.0000
  13.250   1.4252   0.02932   0.02298  -0.0301   0.0167   1.0000
  13.500   1.4326   0.03076   0.02443  -0.0290   0.0144   1.0000
  13.750   1.4372   0.03247   0.02616  -0.0277   0.0106   1.0000
  14.000   1.4360   0.03472   0.02841  -0.0262   0.0050   1.0000
  14.250   1.4405   0.03657   0.03032  -0.0253   0.0041   1.0000
  14.500   1.4455   0.03844   0.03224  -0.0244   0.0036   1.0000
  14.750   1.4502   0.04040   0.03427  -0.0237   0.0033   1.0000
  15.000   1.4561   0.04228   0.03621  -0.0231   0.0032   1.0000
  15.250   1.4618   0.04424   0.03823  -0.0226   0.0032   1.0000
  15.500   1.4642   0.04662   0.04068  -0.0221   0.0029   1.0000
  16.000   1.4719   0.05120   0.04540  -0.0217   0.0029   1.0000
  16.250   1.4747   0.05370   0.04799  -0.0216   0.0028   1.0000
  16.500   1.4765   0.05638   0.05075  -0.0216   0.0027   1.0000
  16.750   1.4779   0.05919   0.05364  -0.0218   0.0027   1.0000
  17.000   1.4774   0.06229   0.05682  -0.0221   0.0027   1.0000
  17.250   1.4767   0.06549   0.06011  -0.0225   0.0026   1.0000
  17.500   1.4752   0.06889   0.06359  -0.0232   0.0026   1.0000
  17.750   1.4713   0.07271   0.06751  -0.0240   0.0025   1.0000
  18.000   1.4674   0.07662   0.07152  -0.0250   0.0025   1.0000
  18.250   1.4607   0.08104   0.07604  -0.0263   0.0024   1.0000
  18.500   1.4558   0.08529   0.08039  -0.0276   0.0024   1.0000
  18.750   1.4488   0.08999   0.08520  -0.0293   0.0024   1.0000
  19.000   1.4384   0.09529   0.09061  -0.0313   0.0023   1.0000
  19.250   1.4309   0.10023   0.09566  -0.0333   0.0023   1.0000
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