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HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.91 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3014-il-1000000-n5.txt
Download as CSV file: xf-hq3014-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/14 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7330   0.10517   0.10279  -0.0488   1.0000   0.0060
 -16.500  -0.8116   0.08685   0.08428  -0.0589   1.0000   0.0059
 -16.250  -0.9056   0.06572   0.06283  -0.0715   1.0000   0.0057
 -16.000  -0.9399   0.05580   0.05272  -0.0782   1.0000   0.0056
 -15.750  -0.9617   0.04911   0.04586  -0.0826   1.0000   0.0056
 -15.500  -0.9763   0.04405   0.04066  -0.0856   1.0000   0.0056
 -15.250  -0.9853   0.04010   0.03660  -0.0875   1.0000   0.0056
 -15.000  -0.9917   0.03674   0.03312  -0.0888   1.0000   0.0057
 -14.750  -0.9941   0.03406   0.03034  -0.0895   1.0000   0.0057
 -14.500  -0.9951   0.03174   0.02793  -0.0897   1.0000   0.0058
 -14.250  -0.9965   0.02962   0.02572  -0.0894   1.0000   0.0058
 -14.000  -0.9974   0.02786   0.02387  -0.0885   1.0000   0.0059
 -13.750  -0.9887   0.02612   0.02202  -0.0891   0.9913   0.0060
 -13.500  -0.9668   0.02449   0.02028  -0.0918   0.9834   0.0061
 -13.250  -0.9414   0.02304   0.01872  -0.0946   0.9759   0.0062
 -13.000  -0.9126   0.02187   0.01744  -0.0971   0.9683   0.0063
 -12.750  -0.8853   0.02080   0.01625  -0.0989   0.9566   0.0063
 -12.500  -0.8607   0.01996   0.01530  -0.0998   0.9412   0.0064
 -12.250  -0.8413   0.01924   0.01445  -0.0993   0.9236   0.0065
 -12.000  -0.8249   0.01853   0.01361  -0.0982   0.9085   0.0065
 -11.500  -0.7916   0.01710   0.01196  -0.0958   0.8852   0.0070
 -11.250  -0.7721   0.01653   0.01130  -0.0949   0.8766   0.0072
 -11.000  -0.7514   0.01602   0.01072  -0.0941   0.8685   0.0074
 -10.750  -0.7300   0.01553   0.01015  -0.0934   0.8614   0.0076
 -10.500  -0.7078   0.01508   0.00961  -0.0927   0.8543   0.0078
 -10.250  -0.6853   0.01464   0.00909  -0.0921   0.8483   0.0080
 -10.000  -0.6619   0.01421   0.00861  -0.0916   0.8423   0.0082
  -9.750  -0.6382   0.01383   0.00815  -0.0911   0.8362   0.0084
  -9.500  -0.6140   0.01345   0.00771  -0.0907   0.8308   0.0086
  -9.250  -0.5895   0.01308   0.00728  -0.0904   0.8251   0.0088
  -9.000  -0.5653   0.01268   0.00682  -0.0899   0.8197   0.0094
  -8.750  -0.5404   0.01232   0.00642  -0.0896   0.8144   0.0099
  -8.500  -0.5151   0.01199   0.00605  -0.0893   0.8087   0.0106
  -8.000  -0.4642   0.01134   0.00534  -0.0887   0.7983   0.0134
  -7.750  -0.4386   0.01102   0.00501  -0.0885   0.7925   0.0167
  -7.500  -0.4127   0.01076   0.00476  -0.0883   0.7875   0.0212
  -7.250  -0.3859   0.01054   0.00452  -0.0882   0.7825   0.0237
  -7.000  -0.3592   0.01033   0.00430  -0.0881   0.7770   0.0259
  -6.750  -0.3322   0.01017   0.00408  -0.0879   0.7720   0.0276
  -6.500  -0.3049   0.00999   0.00387  -0.0879   0.7670   0.0288
  -6.250  -0.2779   0.00979   0.00366  -0.0878   0.7616   0.0308
  -6.000  -0.2509   0.00963   0.00347  -0.0877   0.7566   0.0325
  -5.750  -0.2233   0.00946   0.00329  -0.0877   0.7517   0.0342
  -5.500  -0.1959   0.00930   0.00311  -0.0876   0.7463   0.0367
  -5.250  -0.1687   0.00915   0.00295  -0.0875   0.7412   0.0399
  -5.000  -0.1409   0.00901   0.00279  -0.0876   0.7363   0.0425
  -4.750  -0.1134   0.00885   0.00264  -0.0875   0.7307   0.0472
  -4.500  -0.0858   0.00872   0.00250  -0.0875   0.7255   0.0516
  -4.250  -0.0580   0.00859   0.00236  -0.0875   0.7195   0.0559
  -4.000  -0.0305   0.00847   0.00223  -0.0875   0.7128   0.0615
  -3.750  -0.0026   0.00836   0.00211  -0.0875   0.7066   0.0672
  -3.500   0.0251   0.00824   0.00200  -0.0875   0.7002   0.0758
  -3.250   0.0527   0.00812   0.00189  -0.0874   0.6950   0.0876
  -3.000   0.0807   0.00797   0.00179  -0.0875   0.6897   0.1033
  -2.750   0.1082   0.00782   0.00168  -0.0875   0.6843   0.1256
  -2.500   0.1354   0.00761   0.00159  -0.0875   0.6793   0.1646
  -2.250   0.1630   0.00739   0.00150  -0.0876   0.6739   0.2068
  -2.000   0.1903   0.00722   0.00142  -0.0876   0.6676   0.2465
  -1.750   0.2178   0.00705   0.00135  -0.0876   0.6608   0.2854
  -1.500   0.2432   0.00658   0.00124  -0.0874   0.6525   0.4060
  -1.250   0.2703   0.00640   0.00121  -0.0874   0.6446   0.4673
  -1.000   0.2981   0.00638   0.00120  -0.0874   0.6362   0.4883
  -0.750   0.3260   0.00633   0.00121  -0.0874   0.6283   0.5146
  -0.500   0.3534   0.00631   0.00123  -0.0873   0.6191   0.5440
  -0.250   0.3814   0.00630   0.00125  -0.0873   0.6104   0.5658
   0.000   0.4093   0.00633   0.00126  -0.0872   0.6024   0.5747
   0.250   0.4374   0.00638   0.00128  -0.0872   0.5927   0.5825
   0.500   0.4651   0.00642   0.00131  -0.0872   0.5829   0.5903
   0.750   0.4926   0.00650   0.00135  -0.0871   0.5703   0.5991
   1.000   0.5193   0.00659   0.00140  -0.0869   0.5519   0.6086
   1.250   0.5459   0.00671   0.00146  -0.0866   0.5337   0.6180
   1.500   0.5726   0.00682   0.00153  -0.0864   0.5170   0.6259
   1.750   0.5991   0.00697   0.00160  -0.0861   0.4994   0.6317
   2.000   0.6253   0.00711   0.00169  -0.0859   0.4815   0.6371
   2.250   0.6517   0.00725   0.00178  -0.0856   0.4652   0.6428
   2.500   0.6777   0.00743   0.00188  -0.0853   0.4467   0.6479
   2.750   0.7031   0.00762   0.00200  -0.0849   0.4258   0.6530
   3.000   0.7285   0.00782   0.00214  -0.0845   0.4067   0.6587
   3.500   0.7787   0.00824   0.00242  -0.0836   0.3657   0.6702
   3.750   0.8028   0.00850   0.00259  -0.0830   0.3421   0.6763
   4.000   0.8270   0.00876   0.00276  -0.0824   0.3195   0.6820
   4.250   0.8513   0.00899   0.00294  -0.0818   0.3028   0.6886
   4.500   0.8757   0.00922   0.00312  -0.0812   0.2874   0.6950
   4.750   0.8998   0.00944   0.00331  -0.0807   0.2734   0.7014
   5.000   0.9244   0.00964   0.00349  -0.0801   0.2629   0.7086
   5.250   0.9484   0.00986   0.00368  -0.0795   0.2519   0.7153
   5.500   0.9720   0.01009   0.00389  -0.0789   0.2394   0.7228
   5.750   0.9962   0.01028   0.00407  -0.0783   0.2299   0.7297
   6.000   1.0194   0.01052   0.00429  -0.0775   0.2188   0.7376
   6.250   1.0417   0.01078   0.00453  -0.0766   0.2060   0.7455
   6.500   1.0636   0.01106   0.00477  -0.0757   0.1943   0.7539
   6.750   1.0853   0.01133   0.00502  -0.0747   0.1829   0.7618
   7.000   1.1047   0.01169   0.00533  -0.0733   0.1672   0.7713
   7.250   1.1254   0.01196   0.00560  -0.0722   0.1577   0.7807
   7.500   1.1436   0.01229   0.00590  -0.0706   0.1451   0.7909
   7.750   1.1604   0.01259   0.00619  -0.0687   0.1365   0.8023
   8.000   1.1783   0.01283   0.00648  -0.0670   0.1302   0.8158
   8.250   1.1932   0.01319   0.00683  -0.0648   0.1199   0.8327
   8.500   1.2058   0.01359   0.00724  -0.0622   0.1070   0.8576
   9.000   1.2435   0.01442   0.00817  -0.0600   0.0845   1.0000
   9.250   1.2587   0.01492   0.00864  -0.0582   0.0760   1.0000
   9.500   1.2733   0.01545   0.00914  -0.0564   0.0683   1.0000
   9.750   1.2865   0.01608   0.00972  -0.0544   0.0598   1.0000
  10.000   1.2986   0.01678   0.01038  -0.0524   0.0510   1.0000
  10.250   1.3120   0.01745   0.01101  -0.0506   0.0445   1.0000
  10.500   1.3244   0.01818   0.01173  -0.0488   0.0384   1.0000
  10.750   1.3349   0.01905   0.01256  -0.0468   0.0313   1.0000
  11.000   1.3474   0.01983   0.01333  -0.0451   0.0278   1.0000
  11.250   1.3586   0.02072   0.01422  -0.0434   0.0226   1.0000
  11.500   1.3687   0.02171   0.01519  -0.0417   0.0179   1.0000
  11.750   1.3785   0.02275   0.01622  -0.0400   0.0142   1.0000
  12.000   1.3890   0.02377   0.01726  -0.0385   0.0114   1.0000
  12.250   1.3900   0.02550   0.01897  -0.0362   0.0041   1.0000
  12.500   1.4003   0.02661   0.02012  -0.0348   0.0038   1.0000
  12.750   1.4095   0.02784   0.02140  -0.0335   0.0034   1.0000
  13.000   1.4194   0.02904   0.02265  -0.0323   0.0033   1.0000
  13.250   1.4284   0.03034   0.02401  -0.0312   0.0031   1.0000
  13.500   1.4378   0.03164   0.02537  -0.0301   0.0030   1.0000
  13.750   1.4459   0.03308   0.02688  -0.0291   0.0029   1.0000
  14.000   1.4537   0.03458   0.02844  -0.0281   0.0028   1.0000
  14.250   1.4608   0.03619   0.03012  -0.0273   0.0028   1.0000
  14.500   1.4674   0.03790   0.03189  -0.0265   0.0027   1.0000
  14.750   1.4735   0.03970   0.03376  -0.0257   0.0027   1.0000
  15.000   1.4784   0.04167   0.03581  -0.0251   0.0026   1.0000
  15.250   1.4818   0.04386   0.03807  -0.0246   0.0025   1.0000
  15.500   1.4843   0.04622   0.04051  -0.0241   0.0024   1.0000
  15.750   1.4880   0.04851   0.04288  -0.0238   0.0024   1.0000
  16.000   1.4878   0.05131   0.04577  -0.0237   0.0023   1.0000
  16.250   1.4875   0.05422   0.04877  -0.0237   0.0022   1.0000
  16.500   1.4845   0.05757   0.05222  -0.0238   0.0022   1.0000
  16.750   1.4819   0.06095   0.05570  -0.0242   0.0021   1.0000
  17.000   1.4775   0.06471   0.05957  -0.0248   0.0021   1.0000
  17.250   1.4720   0.06875   0.06371  -0.0257   0.0021   1.0000
  17.500   1.4673   0.07280   0.06786  -0.0267   0.0020   1.0000
  17.750   1.4610   0.07720   0.07237  -0.0280   0.0020   1.0000
  18.000   1.4547   0.08174   0.07702  -0.0294   0.0020   1.0000
  18.250   1.4469   0.08663   0.08202  -0.0312   0.0020   1.0000
  18.500   1.4369   0.09202   0.08753  -0.0333   0.0020   1.0000
  18.750   1.4272   0.09746   0.09308  -0.0356   0.0020   1.0000
  19.000   1.4166   0.10319   0.09892  -0.0381   0.0020   1.0000
  19.250   1.4031   0.10958   0.10544  -0.0411   0.0019   1.0000
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