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HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.66 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq3014-il-1000000.txt
Download as CSV file: xf-hq3014-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7161   0.09514   0.09290  -0.0538   1.0000   0.0085
 -15.750  -0.7654   0.08183   0.07942  -0.0613   1.0000   0.0084
 -15.500  -0.8110   0.06943   0.06684  -0.0689   1.0000   0.0082
 -15.250  -0.8372   0.06061   0.05786  -0.0747   1.0000   0.0082
 -15.000  -0.8586   0.05351   0.05060  -0.0795   1.0000   0.0082
 -14.750  -0.8705   0.04841   0.04538  -0.0827   1.0000   0.0083
 -14.500  -0.8855   0.04342   0.04025  -0.0855   1.0000   0.0083
 -14.250  -0.8934   0.03972   0.03642  -0.0872   1.0000   0.0083
 -14.000  -0.8988   0.03658   0.03317  -0.0882   1.0000   0.0084
 -13.750  -0.9037   0.03381   0.03029  -0.0886   1.0000   0.0084
 -13.500  -0.9056   0.03164   0.02802  -0.0884   1.0000   0.0085
 -13.250  -0.9117   0.02955   0.02583  -0.0873   1.0000   0.0085
 -13.000  -0.9205   0.02811   0.02432  -0.0846   1.0000   0.0086
 -12.750  -0.9047   0.02621   0.02230  -0.0869   0.9967   0.0086
 -12.500  -0.8818   0.02472   0.02068  -0.0893   0.9893   0.0087
 -12.250  -0.8633   0.02201   0.01774  -0.0920   0.9833   0.0090
 -12.000  -0.8386   0.02050   0.01610  -0.0938   0.9770   0.0092
 -11.750  -0.8096   0.01922   0.01473  -0.0960   0.9717   0.0095
 -11.500  -0.7823   0.01831   0.01373  -0.0972   0.9634   0.0098
 -11.250  -0.7552   0.01749   0.01282  -0.0981   0.9545   0.0101
 -11.000  -0.7328   0.01684   0.01207  -0.0978   0.9422   0.0103
 -10.750  -0.7119   0.01624   0.01138  -0.0971   0.9297   0.0106
 -10.500  -0.6902   0.01575   0.01078  -0.0964   0.9190   0.0109
 -10.250  -0.6683   0.01528   0.01020  -0.0956   0.9097   0.0112
 -10.000  -0.6461   0.01484   0.00968  -0.0949   0.9007   0.0114
  -9.750  -0.6269   0.01406   0.00879  -0.0939   0.8924   0.0118
  -9.500  -0.6050   0.01351   0.00815  -0.0931   0.8846   0.0123
  -9.250  -0.5818   0.01306   0.00764  -0.0926   0.8780   0.0129
  -9.000  -0.5578   0.01265   0.00717  -0.0920   0.8711   0.0134
  -8.750  -0.5334   0.01230   0.00673  -0.0916   0.8649   0.0141
  -8.500  -0.5092   0.01185   0.00624  -0.0911   0.8587   0.0153
  -8.250  -0.4846   0.01148   0.00585  -0.0907   0.8528   0.0176
  -8.000  -0.4591   0.01118   0.00555  -0.0904   0.8472   0.0221
  -7.750  -0.4328   0.01095   0.00535  -0.0902   0.8415   0.0267
  -7.500  -0.4063   0.01078   0.00513  -0.0900   0.8361   0.0296
  -7.250  -0.3797   0.01058   0.00494  -0.0899   0.8309   0.0323
  -7.000  -0.3526   0.01043   0.00476  -0.0898   0.8254   0.0341
  -6.750  -0.3256   0.01028   0.00455  -0.0896   0.8202   0.0354
  -6.500  -0.2994   0.00998   0.00424  -0.0895   0.8150   0.0380
  -6.250  -0.2723   0.00979   0.00405  -0.0894   0.8095   0.0400
  -6.000  -0.2451   0.00965   0.00385  -0.0893   0.8044   0.0417
  -5.750  -0.2174   0.00953   0.00370  -0.0892   0.7993   0.0430
  -5.500  -0.1908   0.00925   0.00341  -0.0891   0.7938   0.0468
  -5.250  -0.1636   0.00909   0.00323  -0.0890   0.7886   0.0501
  -5.000  -0.1357   0.00897   0.00308  -0.0890   0.7835   0.0527
  -4.750  -0.1087   0.00873   0.00285  -0.0889   0.7779   0.0595
  -4.500  -0.0812   0.00861   0.00269  -0.0888   0.7727   0.0645
  -4.250  -0.0538   0.00838   0.00251  -0.0888   0.7670   0.0746
  -4.000  -0.0265   0.00820   0.00234  -0.0887   0.7610   0.0868
  -3.750   0.0008   0.00802   0.00219  -0.0886   0.7554   0.1060
  -3.500   0.0278   0.00772   0.00204  -0.0886   0.7497   0.1411
  -3.250   0.0545   0.00742   0.00189  -0.0886   0.7444   0.1952
  -3.000   0.0814   0.00714   0.00177  -0.0886   0.7393   0.2473
  -2.750   0.1085   0.00683   0.00164  -0.0886   0.7340   0.3048
  -2.500   0.1337   0.00631   0.00150  -0.0884   0.7287   0.4290
  -2.250   0.1612   0.00613   0.00147  -0.0884   0.7237   0.4830
  -2.000   0.1893   0.00605   0.00144  -0.0884   0.7179   0.5131
  -1.750   0.2173   0.00603   0.00142  -0.0884   0.7117   0.5333
  -1.500   0.2457   0.00599   0.00141  -0.0884   0.7051   0.5538
  -1.250   0.2737   0.00599   0.00140  -0.0884   0.6982   0.5706
  -1.000   0.3021   0.00599   0.00140  -0.0884   0.6919   0.5811
  -0.750   0.3303   0.00599   0.00140  -0.0884   0.6851   0.5945
  -0.500   0.3583   0.00601   0.00142  -0.0884   0.6785   0.6100
  -0.250   0.3866   0.00602   0.00145  -0.0884   0.6719   0.6224
   0.250   0.4432   0.00607   0.00147  -0.0884   0.6591   0.6367
   0.500   0.4712   0.00611   0.00149  -0.0884   0.6521   0.6440
   0.750   0.4994   0.00614   0.00152  -0.0884   0.6443   0.6513
   1.000   0.5268   0.00620   0.00154  -0.0883   0.6345   0.6596
   1.250   0.5548   0.00622   0.00158  -0.0883   0.6249   0.6675
   1.500   0.5824   0.00627   0.00162  -0.0882   0.6160   0.6748
   1.750   0.6101   0.00634   0.00165  -0.0881   0.6057   0.6808
   2.000   0.6376   0.00638   0.00170  -0.0881   0.5954   0.6869
   2.250   0.6650   0.00646   0.00176  -0.0880   0.5848   0.6932
   2.500   0.6918   0.00654   0.00182  -0.0877   0.5720   0.6991
   2.750   0.7184   0.00665   0.00189  -0.0875   0.5573   0.7054
   3.000   0.7449   0.00677   0.00197  -0.0872   0.5415   0.7117
   3.250   0.7708   0.00689   0.00207  -0.0869   0.5238   0.7182
   3.500   0.7965   0.00706   0.00217  -0.0865   0.5046   0.7253
   3.750   0.8211   0.00726   0.00231  -0.0859   0.4829   0.7319
   4.000   0.8461   0.00745   0.00245  -0.0854   0.4622   0.7392
   4.250   0.8706   0.00766   0.00260  -0.0849   0.4411   0.7464
   4.500   0.8945   0.00791   0.00278  -0.0842   0.4192   0.7543
   4.750   0.9183   0.00816   0.00295  -0.0835   0.3963   0.7619
   5.000   0.9415   0.00843   0.00315  -0.0827   0.3744   0.7703
   5.250   0.9644   0.00870   0.00336  -0.0819   0.3496   0.7787
   5.500   0.9865   0.00902   0.00359  -0.0810   0.3254   0.7880
   5.750   1.0088   0.00929   0.00382  -0.0801   0.3062   0.7973
   6.000   1.0309   0.00957   0.00406  -0.0791   0.2892   0.8077
   6.250   1.0528   0.00985   0.00430  -0.0781   0.2737   0.8195
   6.500   1.0747   0.01008   0.00453  -0.0771   0.2608   0.8328
   6.750   1.0958   0.01031   0.00477  -0.0760   0.2474   0.8488
   7.000   1.1144   0.01055   0.00503  -0.0743   0.2301   0.8748
   7.250   1.1436   0.01074   0.00532  -0.0750   0.2137   1.0000
   7.500   1.1640   0.01109   0.00560  -0.0738   0.1993   1.0000
   7.750   1.1841   0.01143   0.00589  -0.0726   0.1873   1.0000
   8.000   1.2027   0.01177   0.00619  -0.0711   0.1772   1.0000
   8.250   1.2186   0.01217   0.00651  -0.0691   0.1651   1.0000
   8.500   1.2345   0.01257   0.00685  -0.0672   0.1533   1.0000
   8.750   1.2516   0.01292   0.00719  -0.0655   0.1446   1.0000
   9.000   1.2674   0.01335   0.00758  -0.0636   0.1356   1.0000
   9.250   1.2832   0.01379   0.00798  -0.0618   0.1263   1.0000
   9.500   1.2994   0.01422   0.00839  -0.0601   0.1183   1.0000
   9.750   1.3137   0.01475   0.00888  -0.0582   0.1090   1.0000
  10.000   1.3276   0.01532   0.00940  -0.0562   0.0994   1.0000
  10.250   1.3420   0.01588   0.00994  -0.0545   0.0912   1.0000
  10.500   1.3544   0.01656   0.01057  -0.0525   0.0817   1.0000
  10.750   1.3654   0.01734   0.01130  -0.0504   0.0714   1.0000
  11.000   1.3773   0.01810   0.01202  -0.0486   0.0639   1.0000
  11.250   1.3881   0.01896   0.01284  -0.0467   0.0553   1.0000
  11.500   1.3990   0.01983   0.01369  -0.0449   0.0486   1.0000
  11.750   1.4079   0.02086   0.01468  -0.0430   0.0414   1.0000
  12.000   1.4201   0.02172   0.01555  -0.0415   0.0378   1.0000
  12.250   1.4287   0.02283   0.01664  -0.0397   0.0322   1.0000
  12.500   1.4383   0.02392   0.01773  -0.0381   0.0283   1.0000
  12.750   1.4466   0.02513   0.01892  -0.0366   0.0233   1.0000
  13.000   1.4550   0.02636   0.02016  -0.0351   0.0200   1.0000
  13.250   1.4586   0.02800   0.02178  -0.0333   0.0142   1.0000
  13.500   1.4601   0.02985   0.02362  -0.0316   0.0083   1.0000
  13.750   1.4613   0.03181   0.02560  -0.0300   0.0055   1.0000
  14.000   1.4675   0.03342   0.02727  -0.0289   0.0051   1.0000
  14.250   1.4733   0.03510   0.02901  -0.0278   0.0048   1.0000
  14.500   1.4778   0.03697   0.03095  -0.0268   0.0045   1.0000
  14.750   1.4834   0.03879   0.03284  -0.0261   0.0044   1.0000
  15.000   1.4878   0.04078   0.03491  -0.0253   0.0042   1.0000
  15.250   1.4912   0.04294   0.03715  -0.0247   0.0041   1.0000
  15.500   1.4933   0.04532   0.03962  -0.0242   0.0040   1.0000
  15.750   1.4974   0.04754   0.04191  -0.0239   0.0040   1.0000
  16.000   1.4968   0.05035   0.04483  -0.0236   0.0038   1.0000
  16.250   1.4963   0.05325   0.04783  -0.0235   0.0038   1.0000
  16.500   1.4927   0.05664   0.05132  -0.0236   0.0036   1.0000
  16.750   1.4905   0.05995   0.05473  -0.0240   0.0036   1.0000
  17.000   1.4869   0.06357   0.05845  -0.0245   0.0036   1.0000
  17.250   1.4819   0.06748   0.06246  -0.0252   0.0035   1.0000
  17.500   1.4738   0.07199   0.06710  -0.0263   0.0034   1.0000
  17.750   1.4678   0.07631   0.07152  -0.0276   0.0035   1.0000
  18.000   1.4509   0.08248   0.07783  -0.0296   0.0033   1.0000
  18.250   1.4419   0.08761   0.08308  -0.0315   0.0033   1.0000
  18.500   1.4318   0.09305   0.08864  -0.0336   0.0034   1.0000
  18.750   1.4183   0.09919   0.09491  -0.0362   0.0033   1.0000
  19.000   1.4064   0.10521   0.10105  -0.0390   0.0033   1.0000
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