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HQ 1.0/12 AIRFOIL (hq1012-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.0/12 AIRFOIL (hq1012-il)
Reynolds number: 200,000
Max Cl/Cd: 54.88 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1012-il-200000-n5.txt
Download as CSV file: xf-hq1012-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.0/12 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7659   0.08668   0.08285  -0.0273   1.0000   0.0124
 -13.500  -0.8085   0.07286   0.06879  -0.0368   1.0000   0.0121
 -13.250  -0.8386   0.06352   0.05919  -0.0432   1.0000   0.0117
 -13.000  -0.8580   0.05714   0.05261  -0.0472   1.0000   0.0118
 -12.750  -0.8729   0.05210   0.04737  -0.0497   1.0000   0.0118
 -12.500  -0.8849   0.04787   0.04294  -0.0513   1.0000   0.0120
 -12.250  -0.8942   0.04428   0.03914  -0.0520   1.0000   0.0121
 -12.000  -0.9010   0.04121   0.03588  -0.0520   1.0000   0.0122
 -11.750  -0.9051   0.03862   0.03309  -0.0514   1.0000   0.0125
 -11.500  -0.9074   0.03633   0.03061  -0.0502   1.0000   0.0128
 -11.250  -0.9078   0.03438   0.02844  -0.0485   1.0000   0.0133
 -11.000  -0.9057   0.03272   0.02656  -0.0463   1.0000   0.0138
 -10.750  -0.9012   0.03110   0.02477  -0.0442   1.0000   0.0143
 -10.500  -0.8928   0.02974   0.02334  -0.0426   1.0000   0.0150
 -10.250  -0.8807   0.02866   0.02217  -0.0411   1.0000   0.0157
 -10.000  -0.8677   0.02747   0.02085  -0.0397   1.0000   0.0164
  -9.750  -0.8541   0.02622   0.01946  -0.0381   1.0000   0.0173
  -9.500  -0.8396   0.02503   0.01808  -0.0366   1.0000   0.0183
  -9.250  -0.8254   0.02385   0.01679  -0.0350   1.0000   0.0193
  -9.000  -0.8100   0.02297   0.01588  -0.0335   1.0000   0.0207
  -8.750  -0.7932   0.02227   0.01512  -0.0321   1.0000   0.0226
  -8.500  -0.7767   0.02153   0.01425  -0.0304   1.0000   0.0249
  -8.250  -0.7631   0.02060   0.01330  -0.0285   1.0000   0.0269
  -8.000  -0.7482   0.01996   0.01263  -0.0266   1.0000   0.0293
  -7.750  -0.7211   0.01927   0.01180  -0.0271   0.9946   0.0330
  -7.500  -0.6891   0.01850   0.01102  -0.0288   0.9865   0.0379
  -7.250  -0.6555   0.01796   0.01036  -0.0304   0.9792   0.0430
  -7.000  -0.6230   0.01723   0.00964  -0.0320   0.9715   0.0488
  -6.750  -0.5910   0.01678   0.00908  -0.0332   0.9625   0.0547
  -6.500  -0.5595   0.01609   0.00839  -0.0346   0.9540   0.0615
  -6.250  -0.5281   0.01561   0.00782  -0.0356   0.9445   0.0682
  -6.000  -0.4986   0.01505   0.00726  -0.0364   0.9345   0.0770
  -5.750  -0.4685   0.01453   0.00673  -0.0371   0.9253   0.0868
  -5.500  -0.4397   0.01407   0.00623  -0.0375   0.9157   0.0991
  -5.250  -0.4124   0.01362   0.00580  -0.0377   0.9061   0.1165
  -5.000  -0.3857   0.01314   0.00541  -0.0377   0.8972   0.1438
  -4.750  -0.3607   0.01268   0.00508  -0.0374   0.8874   0.1823
  -4.500  -0.3357   0.01228   0.00477  -0.0371   0.8783   0.2228
  -4.250  -0.3110   0.01185   0.00446  -0.0367   0.8700   0.2659
  -4.000  -0.2876   0.01137   0.00419  -0.0361   0.8609   0.3196
  -3.750  -0.2644   0.01090   0.00398  -0.0354   0.8533   0.3941
  -3.500  -0.2406   0.01057   0.00385  -0.0346   0.8449   0.4584
  -3.250  -0.2157   0.01037   0.00379  -0.0340   0.8376   0.5101
  -3.000  -0.1902   0.01026   0.00376  -0.0333   0.8297   0.5514
  -2.750  -0.1641   0.01020   0.00373  -0.0328   0.8228   0.5844
  -2.500  -0.1379   0.01018   0.00372  -0.0322   0.8151   0.6105
  -2.250  -0.1112   0.01018   0.00369  -0.0318   0.8084   0.6328
  -2.000  -0.0844   0.01017   0.00365  -0.0314   0.8007   0.6483
  -1.750  -0.0572   0.01016   0.00360  -0.0311   0.7940   0.6600
  -1.500  -0.0302   0.01015   0.00357  -0.0307   0.7862   0.6709
  -1.250  -0.0030   0.01015   0.00354  -0.0304   0.7795   0.6824
  -1.000   0.0239   0.01016   0.00352  -0.0301   0.7717   0.6950
  -0.500   0.0779   0.01017   0.00353  -0.0294   0.7574   0.7185
  -0.250   0.1047   0.01018   0.00352  -0.0289   0.7492   0.7292
   0.000   0.1316   0.01017   0.00349  -0.0285   0.7390   0.7389
   0.250   0.1584   0.01016   0.00347  -0.0282   0.7281   0.7462
   0.500   0.1856   0.01016   0.00344  -0.0279   0.7183   0.7539
   0.750   0.2125   0.01016   0.00342  -0.0275   0.7083   0.7612
   1.000   0.2395   0.01016   0.00342  -0.0272   0.6970   0.7690
   1.250   0.2662   0.01016   0.00344  -0.0268   0.6858   0.7768
   1.500   0.2931   0.01017   0.00344  -0.0265   0.6750   0.7846
   1.750   0.3199   0.01019   0.00347  -0.0261   0.6648   0.7928
   2.000   0.3467   0.01020   0.00352  -0.0258   0.6536   0.8008
   2.250   0.3734   0.01022   0.00357  -0.0254   0.6417   0.8096
   2.500   0.3997   0.01024   0.00362  -0.0249   0.6289   0.8178
   2.750   0.4261   0.01028   0.00368  -0.0245   0.6146   0.8270
   3.000   0.4520   0.01031   0.00374  -0.0240   0.5980   0.8364
   3.250   0.4778   0.01035   0.00380  -0.0234   0.5791   0.8461
   3.500   0.5032   0.01042   0.00386  -0.0227   0.5557   0.8569
   3.750   0.5281   0.01053   0.00394  -0.0220   0.5259   0.8687
   4.000   0.5528   0.01071   0.00403  -0.0213   0.4904   0.8818
   4.250   0.5773   0.01095   0.00417  -0.0206   0.4496   0.8970
   4.500   0.6030   0.01132   0.00439  -0.0203   0.4025   0.9141
   4.750   0.6321   0.01179   0.00467  -0.0209   0.3501   0.9349
   5.000   0.6640   0.01231   0.00500  -0.0222   0.3050   0.9602
   5.250   0.6981   0.01278   0.00536  -0.0240   0.2764   0.9908
   5.500   0.7229   0.01320   0.00572  -0.0239   0.2576   1.0000
   6.000   0.7672   0.01399   0.00642  -0.0223   0.2223   1.0000
   6.250   0.7897   0.01439   0.00678  -0.0216   0.2034   1.0000
   6.500   0.8117   0.01483   0.00718  -0.0209   0.1833   1.0000
   6.750   0.8338   0.01528   0.00758  -0.0201   0.1628   1.0000
   7.000   0.8550   0.01581   0.00803  -0.0193   0.1425   1.0000
   7.250   0.8757   0.01638   0.00853  -0.0184   0.1243   1.0000
   7.500   0.8962   0.01697   0.00908  -0.0174   0.1090   1.0000
   7.750   0.9164   0.01758   0.00969  -0.0164   0.0972   1.0000
   8.000   0.9358   0.01825   0.01032  -0.0154   0.0865   1.0000
   8.250   0.9557   0.01885   0.01094  -0.0144   0.0771   1.0000
   8.500   0.9749   0.01950   0.01162  -0.0133   0.0699   1.0000
   8.750   0.9931   0.02020   0.01233  -0.0121   0.0633   1.0000
   9.000   1.0113   0.02088   0.01308  -0.0109   0.0580   1.0000
   9.250   1.0286   0.02159   0.01386  -0.0096   0.0526   1.0000
   9.500   1.0441   0.02241   0.01472  -0.0081   0.0482   1.0000
   9.750   1.0610   0.02308   0.01547  -0.0068   0.0430   1.0000
  10.000   1.0735   0.02392   0.01630  -0.0050   0.0383   1.0000
  10.250   1.0881   0.02462   0.01709  -0.0034   0.0336   1.0000
  10.500   1.0978   0.02564   0.01809  -0.0014   0.0300   1.0000
  10.750   1.1099   0.02655   0.01914   0.0003   0.0272   1.0000
  11.000   1.1204   0.02759   0.02027   0.0019   0.0242   1.0000
  11.250   1.1276   0.02889   0.02162   0.0037   0.0219   1.0000
  11.500   1.1376   0.03005   0.02290   0.0051   0.0192   1.0000
  11.750   1.1440   0.03151   0.02443   0.0066   0.0176   1.0000
  12.000   1.1484   0.03319   0.02619   0.0079   0.0160   1.0000
  12.250   1.1527   0.03495   0.02810   0.0092   0.0151   1.0000
  12.500   1.1558   0.03690   0.03018   0.0102   0.0139   1.0000
  12.750   1.1573   0.03905   0.03245   0.0110   0.0132   1.0000
  13.000   1.1554   0.04164   0.03513   0.0116   0.0126   1.0000
  13.250   1.1514   0.04457   0.03819   0.0119   0.0122   1.0000
  13.500   1.1490   0.04750   0.04129   0.0120   0.0118   1.0000
  13.750   1.1461   0.05063   0.04458   0.0117   0.0115   1.0000
  14.000   1.1408   0.05421   0.04834   0.0111   0.0111   1.0000
  14.250   1.1340   0.05816   0.05248   0.0101   0.0108   1.0000
  14.500   1.1267   0.06238   0.05686   0.0087   0.0106   1.0000
  14.750   1.1181   0.06703   0.06168   0.0069   0.0104   1.0000
  15.000   1.1082   0.07215   0.06696   0.0046   0.0103   1.0000
  15.250   1.0965   0.07796   0.07292   0.0016   0.0100   1.0000
  15.500   1.0854   0.08386   0.07899  -0.0014   0.0101   1.0000
  15.750   1.0718   0.09059   0.08587  -0.0051   0.0099   1.0000
  16.000   1.0575   0.09770   0.09316  -0.0090   0.0100   1.0000
  16.250   1.0420   0.10534   0.10094  -0.0134   0.0098   1.0000
  16.500   1.0256   0.11339   0.10915  -0.0179   0.0099   1.0000
  16.750   1.0080   0.12193   0.11786  -0.0228   0.0100   1.0000
  17.000   0.9888   0.13119   0.12726  -0.0281   0.0100   1.0000
  17.250   0.9654   0.14190   0.13812  -0.0342   0.0102   1.0000
  17.500   0.9297   0.15680   0.15320  -0.0426   0.0105   1.0000
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