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HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 131.6 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq300gd2-il-1000000-n5.txt
Download as CSV file: xf-hq300gd2-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HORSTMANN AND QUAST HQ-300 GD(MOD 2) 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9565   0.05040   0.04756  -0.0814   1.0000   0.0068
 -16.000  -0.9681   0.04548   0.04249  -0.0843   1.0000   0.0068
 -15.750  -0.9721   0.04165   0.03844  -0.0868   0.9335   0.0069
 -15.500  -0.9770   0.03881   0.03534  -0.0871   0.8970   0.0069
 -15.250  -0.9770   0.03641   0.03274  -0.0873   0.8754   0.0070
 -14.750  -0.9692   0.03241   0.02840  -0.0872   0.8458   0.0072
 -14.500  -0.9624   0.03072   0.02657  -0.0869   0.8336   0.0073
 -14.250  -0.9538   0.02923   0.02492  -0.0866   0.8223   0.0073
 -14.000  -0.9436   0.02787   0.02342  -0.0862   0.8112   0.0075
 -13.750  -0.9320   0.02660   0.02202  -0.0857   0.8015   0.0076
 -13.500  -0.9190   0.02546   0.02074  -0.0852   0.7927   0.0077
 -13.250  -0.9049   0.02439   0.01956  -0.0847   0.7843   0.0078
 -13.000  -0.8910   0.02347   0.01850  -0.0840   0.7761   0.0079
 -12.750  -0.8744   0.02258   0.01751  -0.0836   0.7681   0.0080
 -12.500  -0.8549   0.02175   0.01655  -0.0836   0.7606   0.0081
 -12.250  -0.8337   0.02098   0.01566  -0.0838   0.7537   0.0082
 -12.000  -0.8129   0.02010   0.01468  -0.0839   0.7471   0.0084
 -11.750  -0.7903   0.01939   0.01388  -0.0840   0.7414   0.0086
 -11.500  -0.7665   0.01881   0.01324  -0.0842   0.7351   0.0089
 -11.000  -0.7171   0.01781   0.01210  -0.0846   0.7234   0.0093
 -10.750  -0.6917   0.01734   0.01156  -0.0848   0.7175   0.0096
 -10.500  -0.6662   0.01689   0.01103  -0.0850   0.7125   0.0098
 -10.250  -0.6400   0.01644   0.01053  -0.0853   0.7079   0.0101
 -10.000  -0.6136   0.01602   0.01004  -0.0856   0.7029   0.0104
  -9.750  -0.5870   0.01564   0.00958  -0.0859   0.6978   0.0107
  -9.500  -0.5604   0.01517   0.00904  -0.0862   0.6934   0.0110
  -9.250  -0.5332   0.01476   0.00860  -0.0866   0.6886   0.0114
  -9.000  -0.5057   0.01444   0.00824  -0.0870   0.6841   0.0118
  -8.750  -0.4779   0.01414   0.00789  -0.0874   0.6801   0.0122
  -8.500  -0.4497   0.01383   0.00754  -0.0879   0.6765   0.0126
  -8.250  -0.4215   0.01351   0.00718  -0.0884   0.6723   0.0130
  -8.000  -0.3932   0.01322   0.00683  -0.0889   0.6680   0.0134
  -7.750  -0.3647   0.01295   0.00650  -0.0894   0.6641   0.0137
  -7.500  -0.3360   0.01259   0.00610  -0.0899   0.6606   0.0142
  -7.250  -0.3070   0.01231   0.00581  -0.0905   0.6570   0.0148
  -7.000  -0.2779   0.01210   0.00558  -0.0911   0.6533   0.0154
  -6.750  -0.2487   0.01189   0.00533  -0.0917   0.6497   0.0161
  -6.500  -0.2192   0.01165   0.00505  -0.0924   0.6465   0.0166
  -6.250  -0.1895   0.01142   0.00480  -0.0930   0.6429   0.0171
  -6.000  -0.1597   0.01123   0.00457  -0.0937   0.6393   0.0175
  -5.750  -0.1298   0.01092   0.00423  -0.0945   0.6360   0.0184
  -5.500  -0.0999   0.01073   0.00402  -0.0952   0.6329   0.0193
  -5.250  -0.0696   0.01055   0.00383  -0.0960   0.6301   0.0201
  -5.000  -0.0392   0.01037   0.00362  -0.0968   0.6268   0.0209
  -4.750  -0.0088   0.01021   0.00344  -0.0975   0.6233   0.0215
  -4.500   0.0216   0.01004   0.00324  -0.0983   0.6200   0.0227
  -4.250   0.0522   0.00989   0.00307  -0.0991   0.6171   0.0241
  -4.000   0.0830   0.00974   0.00293  -0.1000   0.6146   0.0254
  -3.750   0.1137   0.00962   0.00279  -0.1008   0.6116   0.0268
  -3.500   0.1446   0.00948   0.00266  -0.1017   0.6084   0.0297
  -3.250   0.1754   0.00937   0.00255  -0.1025   0.6052   0.0341
  -3.000   0.2062   0.00926   0.00246  -0.1034   0.6024   0.0422
  -2.750   0.2374   0.00913   0.00237  -0.1043   0.5999   0.0537
  -2.500   0.2688   0.00899   0.00229  -0.1053   0.5971   0.0709
  -2.250   0.3009   0.00877   0.00219  -0.1066   0.5940   0.1112
  -2.000   0.3387   0.00803   0.00202  -0.1098   0.5909   0.2905
  -1.750   0.3759   0.00753   0.00191  -0.1127   0.5878   0.4227
  -1.500   0.4163   0.00694   0.00181  -0.1163   0.5849   0.5806
  -1.250   0.4515   0.00671   0.00188  -0.1182   0.5822   0.6760
  -1.000   0.4825   0.00673   0.00195  -0.1189   0.5791   0.7079
  -0.750   0.5128   0.00678   0.00200  -0.1195   0.5759   0.7194
  -0.500   0.5432   0.00685   0.00202  -0.1202   0.5726   0.7270
  -0.250   0.5733   0.00690   0.00205  -0.1208   0.5693   0.7310
   0.000   0.6036   0.00694   0.00209  -0.1214   0.5655   0.7350
   0.250   0.6338   0.00700   0.00212  -0.1220   0.5607   0.7392
   0.500   0.6639   0.00708   0.00214  -0.1226   0.5560   0.7432
   0.750   0.6937   0.00714   0.00221  -0.1232   0.5519   0.7472
   1.000   0.7234   0.00721   0.00228  -0.1237   0.5473   0.7528
   1.250   0.7533   0.00730   0.00234  -0.1243   0.5426   0.7578
   1.500   0.7831   0.00738   0.00239  -0.1248   0.5384   0.7606
   1.750   0.8127   0.00743   0.00245  -0.1254   0.5342   0.7626
   2.000   0.8423   0.00750   0.00252  -0.1259   0.5294   0.7645
   2.250   0.8715   0.00760   0.00260  -0.1264   0.5245   0.7664
   2.500   0.9012   0.00767   0.00267  -0.1270   0.5201   0.7682
   2.750   0.9307   0.00775   0.00274  -0.1275   0.5146   0.7701
   3.000   0.9598   0.00786   0.00282  -0.1280   0.5091   0.7720
   3.250   0.9894   0.00794   0.00291  -0.1286   0.5033   0.7737
   3.500   1.0185   0.00806   0.00300  -0.1291   0.4962   0.7752
   3.750   1.0474   0.00817   0.00310  -0.1295   0.4892   0.7767
   4.000   1.0757   0.00829   0.00322  -0.1299   0.4806   0.7782
   4.250   1.1041   0.00843   0.00334  -0.1302   0.4713   0.7796
   4.500   1.1319   0.00861   0.00349  -0.1305   0.4608   0.7810
   4.750   1.1594   0.00881   0.00366  -0.1308   0.4483   0.7826
   5.000   1.1865   0.00903   0.00384  -0.1309   0.4337   0.7842
   5.250   1.2131   0.00930   0.00405  -0.1310   0.4178   0.7857
   5.500   1.2392   0.00960   0.00428  -0.1311   0.4010   0.7872
   5.750   1.2648   0.00992   0.00454  -0.1311   0.3834   0.7887
   6.000   1.2899   0.01027   0.00482  -0.1309   0.3651   0.7902
   6.250   1.3146   0.01065   0.00511  -0.1308   0.3477   0.7916
   6.500   1.3388   0.01101   0.00543  -0.1305   0.3315   0.7930
   6.750   1.3624   0.01140   0.00576  -0.1301   0.3158   0.7943
   7.000   1.3858   0.01178   0.00610  -0.1297   0.3016   0.7956
   7.250   1.4087   0.01217   0.00646  -0.1292   0.2879   0.7969
   7.500   1.4310   0.01258   0.00683  -0.1287   0.2749   0.7984
   7.750   1.4524   0.01302   0.00722  -0.1279   0.2619   0.8000
   8.000   1.4720   0.01353   0.00767  -0.1269   0.2459   0.8016
   8.250   1.4881   0.01420   0.00824  -0.1254   0.2242   0.8032
   8.500   1.4984   0.01508   0.00896  -0.1229   0.1968   0.8048
   8.750   1.5025   0.01595   0.00972  -0.1192   0.1757   0.8064
   9.000   1.5132   0.01677   0.01048  -0.1170   0.1615   0.8079
   9.250   1.5241   0.01764   0.01132  -0.1150   0.1493   0.8096
   9.500   1.5338   0.01863   0.01229  -0.1129   0.1367   0.8113
   9.750   1.5430   0.01975   0.01337  -0.1110   0.1245   0.8128
  10.000   1.5514   0.02099   0.01459  -0.1092   0.1127   0.8144
  10.250   1.5601   0.02229   0.01588  -0.1076   0.1023   0.8159
  10.500   1.5668   0.02379   0.01735  -0.1059   0.0912   0.8174
  10.750   1.5724   0.02545   0.01897  -0.1043   0.0802   0.8190
  11.000   1.5764   0.02727   0.02076  -0.1026   0.0691   0.8207
  11.250   1.5796   0.02922   0.02268  -0.1010   0.0587   0.8223
  11.500   1.5826   0.03123   0.02466  -0.0995   0.0497   0.8237
  11.750   1.5847   0.03334   0.02676  -0.0980   0.0416   0.8250
  12.000   1.5867   0.03548   0.02891  -0.0966   0.0348   0.8263
  12.250   1.5889   0.03765   0.03108  -0.0953   0.0292   0.8276
  12.500   1.5912   0.03982   0.03327  -0.0940   0.0250   0.8289
  12.750   1.5952   0.04190   0.03540  -0.0929   0.0218   0.8302
  13.000   1.5986   0.04411   0.03763  -0.0919   0.0191   0.8316
  13.250   1.6021   0.04633   0.03990  -0.0910   0.0171   0.8331
  13.500   1.6065   0.04851   0.04212  -0.0902   0.0156   0.8346
  13.750   1.6109   0.05073   0.04440  -0.0895   0.0144   0.8360
  14.000   1.6137   0.05318   0.04688  -0.0888   0.0132   0.8372
  14.250   1.6183   0.05545   0.04921  -0.0882   0.0125   0.8384
  14.500   1.6217   0.05788   0.05170  -0.0877   0.0117   0.8394
  14.750   1.6240   0.06046   0.05433  -0.0871   0.0110   0.8406
  15.000   1.6260   0.06309   0.05703  -0.0866   0.0103   0.8417
  15.250   1.6287   0.06570   0.05972  -0.0863   0.0098   0.8429
  15.500   1.6310   0.06836   0.06246  -0.0859   0.0094   0.8441
  15.750   1.6321   0.07119   0.06535  -0.0856   0.0089   0.8453
  16.000   1.6319   0.07421   0.06844  -0.0854   0.0085   0.8467
  16.250   1.6316   0.07729   0.07159  -0.0852   0.0081   0.8481
  16.500   1.6320   0.08033   0.07471  -0.0851   0.0079   0.8494
  16.750   1.6322   0.08342   0.07787  -0.0851   0.0076   0.8507
  17.000   1.6319   0.08656   0.08109  -0.0851   0.0073   0.8520
  17.250   1.6301   0.08996   0.08458  -0.0853   0.0071   0.8531
  17.500   1.6283   0.09339   0.08807  -0.0855   0.0068   0.8541
  17.750   1.6256   0.09698   0.09174  -0.0858   0.0066   0.8551
  18.000   1.6215   0.10081   0.09565  -0.0863   0.0064   0.8562
  18.250   1.6170   0.10470   0.09963  -0.0868   0.0062   0.8573
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