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HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 139.79 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq300gd2-il-1000000.txt
Download as CSV file: xf-hq300gd2-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6394   0.05459   0.05232  -0.0817   0.8857   0.0103
 -13.000  -0.6919   0.04404   0.04131  -0.0883   0.8659   0.0103
 -12.750  -0.7192   0.03839   0.03529  -0.0897   0.8500   0.0103
 -12.500  -0.7324   0.03460   0.03119  -0.0896   0.8367   0.0104
 -12.250  -0.7361   0.03185   0.02816  -0.0890   0.8250   0.0105
 -12.000  -0.7327   0.02981   0.02589  -0.0883   0.8144   0.0106
 -11.750  -0.7257   0.02822   0.02410  -0.0876   0.8050   0.0107
 -11.500  -0.7190   0.02565   0.02119  -0.0874   0.7959   0.0109
 -11.250  -0.7078   0.02337   0.01867  -0.0872   0.7880   0.0113
 -11.000  -0.6865   0.02261   0.01780  -0.0873   0.7802   0.0115
 -10.750  -0.6634   0.02202   0.01715  -0.0875   0.7733   0.0117
 -10.500  -0.6396   0.02147   0.01651  -0.0877   0.7664   0.0120
 -10.250  -0.6157   0.02085   0.01579  -0.0878   0.7601   0.0123
 -10.000  -0.5915   0.02012   0.01495  -0.0880   0.7538   0.0126
  -9.750  -0.5671   0.01942   0.01411  -0.0881   0.7475   0.0130
  -9.500  -0.5418   0.01875   0.01332  -0.0883   0.7419   0.0134
  -9.250  -0.5153   0.01835   0.01281  -0.0886   0.7361   0.0137
  -9.000  -0.4921   0.01708   0.01138  -0.0886   0.7308   0.0143
  -8.750  -0.4658   0.01656   0.01082  -0.0890   0.7260   0.0147
  -8.500  -0.4384   0.01620   0.01043  -0.0894   0.7209   0.0152
  -8.250  -0.4111   0.01580   0.00996  -0.0897   0.7158   0.0157
  -8.000  -0.3838   0.01536   0.00945  -0.0901   0.7111   0.0163
  -7.750  -0.3559   0.01493   0.00896  -0.0905   0.7065   0.0168
  -7.500  -0.3277   0.01464   0.00859  -0.0909   0.7019   0.0173
  -7.250  -0.3018   0.01373   0.00757  -0.0911   0.6976   0.0181
  -7.000  -0.2737   0.01327   0.00711  -0.0916   0.6938   0.0188
  -6.750  -0.2448   0.01300   0.00683  -0.0922   0.6896   0.0196
  -6.500  -0.2160   0.01275   0.00653  -0.0927   0.6853   0.0205
  -6.250  -0.1871   0.01250   0.00622  -0.0932   0.6810   0.0212
  -6.000  -0.1576   0.01227   0.00596  -0.0938   0.6776   0.0217
  -5.750  -0.1286   0.01149   0.00513  -0.0946   0.6740   0.0230
  -5.500  -0.0989   0.01119   0.00482  -0.0954   0.6703   0.0240
  -5.250  -0.0691   0.01100   0.00459  -0.0961   0.6665   0.0251
  -5.000  -0.0390   0.01080   0.00435  -0.0968   0.6630   0.0263
  -4.750  -0.0085   0.01059   0.00413  -0.0976   0.6596   0.0270
  -4.500   0.0226   0.01018   0.00367  -0.0986   0.6563   0.0287
  -4.250   0.0532   0.00999   0.00346  -0.0995   0.6530   0.0306
  -4.000   0.0837   0.00986   0.00329  -0.1003   0.6493   0.0324
  -3.750   0.1148   0.00968   0.00310  -0.1012   0.6464   0.0342
  -3.500   0.1462   0.00946   0.00290  -0.1022   0.6432   0.0390
  -3.250   0.1775   0.00927   0.00274  -0.1032   0.6400   0.0485
  -3.000   0.2095   0.00902   0.00259  -0.1044   0.6369   0.0781
  -2.750   0.2456   0.00832   0.00237  -0.1072   0.6334   0.2282
  -2.500   0.2855   0.00749   0.00218  -0.1109   0.6307   0.4181
  -2.250   0.3278   0.00674   0.00204  -0.1151   0.6276   0.6041
  -2.000   0.3616   0.00659   0.00211  -0.1165   0.6245   0.6846
  -1.750   0.3925   0.00664   0.00217  -0.1172   0.6214   0.7109
  -1.500   0.4228   0.00676   0.00224  -0.1178   0.6179   0.7283
  -1.250   0.4529   0.00685   0.00235  -0.1182   0.6152   0.7425
  -1.000   0.4819   0.00696   0.00248  -0.1184   0.6123   0.7530
  -0.750   0.5126   0.00706   0.00253  -0.1191   0.6092   0.7596
  -0.500   0.5417   0.00713   0.00259  -0.1194   0.6059   0.7636
  -0.250   0.5710   0.00724   0.00265  -0.1198   0.6022   0.7665
   0.000   0.6010   0.00729   0.00270  -0.1203   0.5990   0.7696
   0.250   0.6313   0.00733   0.00273  -0.1209   0.5952   0.7728
   0.500   0.6618   0.00740   0.00276  -0.1217   0.5913   0.7757
   0.750   0.6907   0.00748   0.00281  -0.1220   0.5873   0.7786
   1.000   0.7193   0.00757   0.00292  -0.1222   0.5838   0.7819
   1.250   0.7484   0.00765   0.00302  -0.1225   0.5802   0.7856
   1.500   0.7782   0.00773   0.00308  -0.1230   0.5765   0.7888
   1.750   0.8082   0.00782   0.00313  -0.1237   0.5727   0.7910
   2.000   0.8381   0.00788   0.00318  -0.1243   0.5690   0.7929
   2.250   0.8676   0.00790   0.00322  -0.1248   0.5654   0.7946
   2.500   0.8967   0.00795   0.00329  -0.1252   0.5614   0.7961
   2.750   0.9256   0.00803   0.00336  -0.1256   0.5574   0.7977
   3.000   0.9547   0.00812   0.00344  -0.1261   0.5534   0.7994
   3.250   0.9844   0.00816   0.00352  -0.1266   0.5491   0.8010
   3.500   1.0137   0.00824   0.00359  -0.1272   0.5444   0.8028
   3.750   1.0427   0.00836   0.00367  -0.1277   0.5393   0.8046
   4.000   1.0727   0.00840   0.00375  -0.1283   0.5346   0.8062
   4.250   1.1021   0.00848   0.00383  -0.1289   0.5288   0.8077
   4.500   1.1308   0.00858   0.00391  -0.1294   0.5230   0.8092
   4.750   1.1596   0.00863   0.00400  -0.1298   0.5168   0.8106
   5.000   1.1874   0.00875   0.00411  -0.1301   0.5096   0.8119
   5.250   1.2158   0.00884   0.00423  -0.1304   0.5023   0.8132
   5.500   1.2432   0.00900   0.00437  -0.1306   0.4938   0.8147
   5.750   1.2713   0.00911   0.00451  -0.1309   0.4845   0.8163
   6.000   1.2986   0.00929   0.00467  -0.1312   0.4740   0.8178
   6.250   1.3255   0.00949   0.00485  -0.1313   0.4617   0.8193
   6.500   1.3520   0.00973   0.00505  -0.1315   0.4476   0.8208
   6.750   1.3780   0.01001   0.00527  -0.1315   0.4313   0.8224
   7.000   1.4033   0.01033   0.00554  -0.1314   0.4133   0.8238
   7.250   1.4273   0.01068   0.00583  -0.1312   0.3940   0.8253
   7.500   1.4498   0.01110   0.00618  -0.1306   0.3743   0.8266
   7.750   1.4714   0.01156   0.00656  -0.1299   0.3547   0.8279
   8.000   1.4916   0.01208   0.00701  -0.1290   0.3319   0.8293
   8.250   1.5090   0.01274   0.00753  -0.1276   0.3062   0.8308
   8.500   1.5241   0.01348   0.00813  -0.1259   0.2800   0.8326
   8.750   1.5417   0.01404   0.00863  -0.1245   0.2629   0.8344
   9.000   1.5583   0.01460   0.00915  -0.1231   0.2485   0.8361
   9.250   1.5696   0.01521   0.00971  -0.1206   0.2345   0.8378
   9.500   1.5793   0.01593   0.01038  -0.1180   0.2202   0.8393
   9.750   1.5908   0.01673   0.01114  -0.1160   0.2062   0.8410
  10.000   1.6007   0.01763   0.01202  -0.1139   0.1924   0.8428
  10.250   1.6087   0.01873   0.01307  -0.1117   0.1781   0.8446
  10.500   1.6155   0.02000   0.01430  -0.1096   0.1635   0.8463
  11.000   1.6266   0.02300   0.01721  -0.1057   0.1352   0.8498
  11.250   1.6310   0.02471   0.01888  -0.1040   0.1220   0.8515
  11.500   1.6343   0.02657   0.02069  -0.1023   0.1089   0.8531
  11.750   1.6365   0.02858   0.02265  -0.1006   0.0964   0.8546
  12.000   1.6377   0.03071   0.02475  -0.0989   0.0845   0.8562
  12.250   1.6367   0.03302   0.02702  -0.0972   0.0725   0.8579
  12.500   1.6353   0.03542   0.02940  -0.0955   0.0618   0.8593
  12.750   1.6331   0.03794   0.03190  -0.0939   0.0518   0.8607
  13.000   1.6303   0.04057   0.03451  -0.0923   0.0431   0.8622
  13.250   1.6281   0.04326   0.03719  -0.0910   0.0357   0.8636
  13.500   1.6263   0.04598   0.03992  -0.0898   0.0298   0.8651
  13.750   1.6249   0.04873   0.04268  -0.0888   0.0252   0.8665
  14.000   1.6259   0.05130   0.04528  -0.0879   0.0221   0.8680
  14.250   1.6264   0.05400   0.04802  -0.0872   0.0197   0.8693
  14.500   1.6273   0.05668   0.05075  -0.0865   0.0181   0.8706
  14.750   1.6258   0.05965   0.05377  -0.0858   0.0164   0.8720
  15.000   1.6290   0.06214   0.05634  -0.0853   0.0156   0.8733
  15.250   1.6295   0.06497   0.05924  -0.0849   0.0146   0.8746
  15.500   1.6286   0.06801   0.06233  -0.0845   0.0138   0.8759
  15.750   1.6261   0.07125   0.06565  -0.0841   0.0130   0.8772
  16.000   1.6273   0.07413   0.06861  -0.0839   0.0125   0.8786
  16.250   1.6277   0.07713   0.07169  -0.0837   0.0120   0.8799
  16.500   1.6260   0.08045   0.07508  -0.0837   0.0115   0.8813
  16.750   1.6224   0.08406   0.07875  -0.0837   0.0110   0.8826
  17.000   1.6147   0.08821   0.08299  -0.0838   0.0105   0.8837
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