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HQ 3.0/13 AIRFOIL (hq3013-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/13 AIRFOIL (hq3013-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.93 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3013-il-1000000-n5.txt
Download as CSV file: xf-hq3013-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6834   0.10018   0.09797  -0.0474   1.0000   0.0052
 -15.250  -0.7287   0.08771   0.08541  -0.0541   1.0000   0.0051
 -15.000  -0.8635   0.05768   0.05498  -0.0728   1.0000   0.0049
 -14.750  -0.8859   0.04987   0.04701  -0.0784   1.0000   0.0049
 -14.500  -0.9124   0.04277   0.03973  -0.0833   1.0000   0.0049
 -14.250  -0.9230   0.03856   0.03539  -0.0856   1.0000   0.0049
 -14.000  -0.9327   0.03493   0.03162  -0.0871   1.0000   0.0049
 -13.750  -0.9287   0.03306   0.02968  -0.0873   1.0000   0.0050
 -13.500  -0.9398   0.03025   0.02674  -0.0871   1.0000   0.0050
 -13.000  -0.9223   0.02672   0.02300  -0.0889   0.9877   0.0050
 -12.750  -0.8995   0.02511   0.02125  -0.0912   0.9822   0.0051
 -12.500  -0.8788   0.02307   0.01902  -0.0935   0.9746   0.0053
 -12.250  -0.8547   0.02153   0.01733  -0.0953   0.9673   0.0055
 -12.000  -0.8295   0.02038   0.01607  -0.0965   0.9578   0.0056
 -11.750  -0.8067   0.01946   0.01504  -0.0969   0.9451   0.0057
 -11.500  -0.7852   0.01868   0.01414  -0.0967   0.9307   0.0058
 -11.250  -0.7647   0.01799   0.01334  -0.0961   0.9170   0.0059
 -11.000  -0.7445   0.01733   0.01256  -0.0953   0.9049   0.0061
 -10.750  -0.7236   0.01674   0.01186  -0.0946   0.8940   0.0062
 -10.250  -0.6803   0.01561   0.01050  -0.0933   0.8738   0.0065
 -10.000  -0.6576   0.01511   0.00990  -0.0927   0.8657   0.0066
  -9.750  -0.6344   0.01462   0.00932  -0.0922   0.8580   0.0068
  -9.500  -0.6107   0.01418   0.00879  -0.0918   0.8511   0.0069
  -9.250  -0.5863   0.01375   0.00829  -0.0914   0.8443   0.0071
  -8.750  -0.5375   0.01287   0.00724  -0.0907   0.8320   0.0076
  -8.500  -0.5127   0.01245   0.00675  -0.0903   0.8257   0.0078
  -8.250  -0.4874   0.01207   0.00631  -0.0900   0.8202   0.0082
  -8.000  -0.4616   0.01172   0.00592  -0.0898   0.8141   0.0084
  -7.750  -0.4358   0.01141   0.00555  -0.0896   0.8084   0.0088
  -7.500  -0.4094   0.01112   0.00520  -0.0894   0.8031   0.0091
  -7.250  -0.3830   0.01084   0.00487  -0.0892   0.7974   0.0095
  -7.000  -0.3565   0.01059   0.00456  -0.0890   0.7922   0.0100
  -6.750  -0.3299   0.01029   0.00423  -0.0889   0.7869   0.0112
  -6.500  -0.3032   0.01003   0.00394  -0.0888   0.7817   0.0129
  -6.250  -0.2767   0.00976   0.00367  -0.0887   0.7768   0.0172
  -6.000  -0.2496   0.00952   0.00346  -0.0886   0.7719   0.0233
  -5.750  -0.2222   0.00935   0.00328  -0.0886   0.7670   0.0268
  -5.500  -0.1947   0.00921   0.00310  -0.0885   0.7623   0.0288
  -5.250  -0.1671   0.00903   0.00292  -0.0885   0.7576   0.0315
  -5.000  -0.1394   0.00889   0.00276  -0.0885   0.7527   0.0336
  -4.500  -0.0839   0.00860   0.00245  -0.0885   0.7431   0.0406
  -4.250  -0.0560   0.00848   0.00232  -0.0886   0.7376   0.0439
  -4.000  -0.0284   0.00836   0.00218  -0.0885   0.7320   0.0490
  -3.750  -0.0004   0.00823   0.00206  -0.0886   0.7251   0.0545
  -3.500   0.0271   0.00812   0.00193  -0.0885   0.7178   0.0625
  -3.250   0.0552   0.00800   0.00182  -0.0886   0.7108   0.0708
  -2.750   0.1107   0.00773   0.00161  -0.0886   0.6990   0.1014
  -2.500   0.1385   0.00758   0.00152  -0.0887   0.6929   0.1245
  -2.250   0.1660   0.00740   0.00143  -0.0887   0.6874   0.1601
  -2.000   0.1937   0.00719   0.00135  -0.0887   0.6815   0.2035
  -1.750   0.2209   0.00700   0.00127  -0.0887   0.6742   0.2529
  -1.500   0.2483   0.00681   0.00120  -0.0888   0.6659   0.3004
  -1.250   0.2741   0.00638   0.00111  -0.0887   0.6578   0.4258
  -1.000   0.3015   0.00623   0.00111  -0.0887   0.6489   0.4873
  -0.750   0.3292   0.00622   0.00111  -0.0886   0.6396   0.5080
  -0.500   0.3570   0.00621   0.00112  -0.0886   0.6299   0.5306
  -0.250   0.3849   0.00618   0.00115  -0.0886   0.6224   0.5582
   0.000   0.4127   0.00621   0.00117  -0.0885   0.6136   0.5712
   0.250   0.4408   0.00625   0.00118  -0.0885   0.6037   0.5785
   0.500   0.4684   0.00630   0.00121  -0.0885   0.5918   0.5872
   0.750   0.4954   0.00639   0.00125  -0.0883   0.5734   0.5979
   1.000   0.5221   0.00650   0.00130  -0.0880   0.5548   0.6080
   1.250   0.5490   0.00661   0.00136  -0.0879   0.5375   0.6148
   1.500   0.5759   0.00673   0.00142  -0.0877   0.5192   0.6206
   2.000   0.6287   0.00702   0.00158  -0.0872   0.4803   0.6311
   2.250   0.6548   0.00720   0.00168  -0.0869   0.4587   0.6373
   2.500   0.6806   0.00739   0.00179  -0.0865   0.4375   0.6433
   2.750   0.7062   0.00759   0.00192  -0.0862   0.4155   0.6500
   3.250   0.7569   0.00801   0.00220  -0.0854   0.3718   0.6629
   3.500   0.7825   0.00821   0.00234  -0.0850   0.3523   0.6701
   3.750   0.8071   0.00846   0.00251  -0.0845   0.3289   0.6777
   4.000   0.8315   0.00872   0.00269  -0.0840   0.3056   0.6860
   4.250   0.8563   0.00894   0.00286  -0.0835   0.2894   0.6941
   4.750   0.9059   0.00937   0.00323  -0.0825   0.2605   0.7119
   5.000   0.9307   0.00957   0.00342  -0.0820   0.2486   0.7217
   5.250   0.9553   0.00978   0.00361  -0.0815   0.2373   0.7322
   5.500   0.9793   0.01000   0.00383  -0.0809   0.2244   0.7427
   5.750   1.0029   0.01025   0.00405  -0.0803   0.2102   0.7533
   6.000   1.0260   0.01051   0.00428  -0.0795   0.1962   0.7655
   6.250   1.0487   0.01079   0.00453  -0.0787   0.1829   0.7783
   6.500   1.0705   0.01110   0.00481  -0.0778   0.1672   0.7916
   6.750   1.0916   0.01142   0.00510  -0.0767   0.1518   0.8053
   7.000   1.1127   0.01173   0.00539  -0.0756   0.1398   0.8204
   7.250   1.1329   0.01203   0.00569  -0.0744   0.1275   0.8392
   7.500   1.1524   0.01228   0.00598  -0.0729   0.1173   0.8655
   7.750   1.1775   0.01254   0.00636  -0.0728   0.1028   1.0000
   8.000   1.1957   0.01301   0.00674  -0.0714   0.0887   1.0000
   8.250   1.2126   0.01345   0.00712  -0.0696   0.0773   1.0000
   8.500   1.2268   0.01397   0.00756  -0.0674   0.0643   1.0000
   8.750   1.2419   0.01445   0.00800  -0.0653   0.0551   1.0000
   9.000   1.2570   0.01494   0.00846  -0.0634   0.0472   1.0000
   9.250   1.2697   0.01558   0.00903  -0.0611   0.0371   1.0000
   9.500   1.2843   0.01613   0.00955  -0.0592   0.0314   1.0000
   9.750   1.2964   0.01683   0.01021  -0.0570   0.0233   1.0000
  10.000   1.3100   0.01746   0.01082  -0.0551   0.0190   1.0000
  10.250   1.3222   0.01820   0.01154  -0.0531   0.0139   1.0000
  10.500   1.3287   0.01930   0.01260  -0.0505   0.0046   1.0000
  10.750   1.3408   0.02010   0.01343  -0.0486   0.0038   1.0000
  11.000   1.3543   0.02083   0.01419  -0.0471   0.0034   1.0000
  11.250   1.3678   0.02158   0.01499  -0.0456   0.0032   1.0000
  11.500   1.3810   0.02237   0.01582  -0.0441   0.0031   1.0000
  11.750   1.3934   0.02323   0.01675  -0.0426   0.0030   1.0000
  12.000   1.4056   0.02414   0.01770  -0.0412   0.0029   1.0000
  12.250   1.4162   0.02517   0.01880  -0.0397   0.0027   1.0000
  12.500   1.4263   0.02628   0.01997  -0.0383   0.0026   1.0000
  12.750   1.4364   0.02742   0.02117  -0.0369   0.0026   1.0000
  13.000   1.4448   0.02871   0.02253  -0.0356   0.0025   1.0000
  13.250   1.4523   0.03012   0.02401  -0.0342   0.0024   1.0000
  13.500   1.4596   0.03159   0.02555  -0.0330   0.0023   1.0000
  13.750   1.4634   0.03340   0.02746  -0.0316   0.0022   1.0000
  14.000   1.4713   0.03489   0.02902  -0.0307   0.0021   1.0000
  14.250   1.4784   0.03650   0.03069  -0.0298   0.0021   1.0000
  14.500   1.4836   0.03835   0.03261  -0.0290   0.0021   1.0000
  14.750   1.4872   0.04040   0.03475  -0.0282   0.0020   1.0000
  15.000   1.4904   0.04257   0.03701  -0.0275   0.0019   1.0000
  15.250   1.4938   0.04480   0.03931  -0.0271   0.0019   1.0000
  15.500   1.4960   0.04724   0.04183  -0.0267   0.0019   1.0000
  15.750   1.4960   0.05000   0.04469  -0.0265   0.0019   1.0000
  16.000   1.4953   0.05297   0.04776  -0.0265   0.0018   1.0000
  16.250   1.4944   0.05607   0.05096  -0.0267   0.0018   1.0000
  16.500   1.4921   0.05945   0.05444  -0.0271   0.0018   1.0000
  16.750   1.4867   0.06338   0.05849  -0.0277   0.0018   1.0000
  17.000   1.4833   0.06719   0.06240  -0.0286   0.0017   1.0000
  17.250   1.4766   0.07161   0.06693  -0.0298   0.0017   1.0000
  17.500   1.4680   0.07646   0.07190  -0.0313   0.0017   1.0000
  17.750   1.4583   0.08169   0.07725  -0.0332   0.0017   1.0000
  18.000   1.4501   0.08682   0.08250  -0.0352   0.0017   1.0000
  18.250   1.4375   0.09285   0.08866  -0.0378   0.0016   1.0000
  18.500   1.4249   0.09904   0.09498  -0.0405   0.0017   1.0000
  18.750   1.4100   0.10583   0.10190  -0.0437   0.0016   1.0000
  19.000   1.3924   0.11331   0.10952  -0.0475   0.0016   1.0000
  19.250   1.3764   0.12060   0.11694  -0.0512   0.0016   1.0000
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