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Apex 16 (normalized using XFOIL date021206) (apex16-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Apex 16 (normalized using XFOIL date021206) (apex16-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.64 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-apex16-il-1000000.txt
Download as CSV file: xf-apex16-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Apex 16 (normalized using XFOIL date021206)     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.3287   0.08450   0.08282  -0.0774   0.9879   0.0131
  -9.750  -0.3241   0.07665   0.07496  -0.0864   0.9863   0.0132
  -9.500  -0.3221   0.06988   0.06813  -0.0954   0.9847   0.0132
  -9.250  -0.3277   0.06456   0.06273  -0.1017   0.9797   0.0132
  -9.000  -0.3298   0.05991   0.05797  -0.1069   0.9750   0.0132
  -8.750  -0.3219   0.05505   0.05296  -0.1111   0.9726   0.0132
  -8.500  -0.3131   0.05091   0.04866  -0.1134   0.9690   0.0133
  -8.250  -0.3179   0.04383   0.04133  -0.1154   0.9629   0.0135
  -8.000  -0.3008   0.04122   0.03861  -0.1174   0.9602   0.0138
  -7.750  -0.2789   0.03873   0.03600  -0.1195   0.9578   0.0141
  -7.500  -0.2673   0.03688   0.03405  -0.1183   0.9506   0.0143
  -7.250  -0.2477   0.03475   0.03176  -0.1187   0.9458   0.0148
  -7.000  -0.2299   0.03258   0.02943  -0.1182   0.9398   0.0157
  -6.750  -0.2044   0.03084   0.02745  -0.1164   0.9337   0.0173
  -6.500  -0.1837   0.02852   0.02487  -0.1160   0.9284   0.0174
  -6.250  -0.1703   0.02651   0.02265  -0.1138   0.9209   0.0174
  -6.000  -0.1601   0.02179   0.01762  -0.1124   0.9148   0.0183
  -5.750  -0.1411   0.02076   0.01651  -0.1113   0.9086   0.0186
  -5.500  -0.1187   0.01966   0.01529  -0.1107   0.9032   0.0192
  -5.250  -0.0949   0.01855   0.01405  -0.1103   0.8982   0.0201
  -5.000  -0.0682   0.01899   0.01436  -0.1095   0.8926   0.0226
  -4.750  -0.0480   0.01579   0.01080  -0.1083   0.8873   0.0235
  -4.500  -0.0232   0.01244   0.00723  -0.1071   0.8823   0.0183
  -4.250   0.0007   0.01160   0.00631  -0.1064   0.8766   0.0182
  -4.000   0.0259   0.01095   0.00562  -0.1061   0.8717   0.0187
  -3.750   0.0478   0.01030   0.00493  -0.1050   0.8658   0.0188
  -3.500   0.0711   0.00980   0.00439  -0.1043   0.8601   0.0192
  -3.250   0.0952   0.00942   0.00396  -0.1037   0.8549   0.0199
  -3.000   0.1184   0.00908   0.00359  -0.1029   0.8489   0.0205
  -2.750   0.1429   0.00874   0.00318  -0.1024   0.8436   0.0209
  -2.500   0.1672   0.00847   0.00287  -0.1018   0.8380   0.0215
  -2.250   0.1919   0.00823   0.00257  -0.1012   0.8323   0.0220
  -2.000   0.2187   0.00813   0.00243  -0.1011   0.8270   0.0228
  -1.750   0.2418   0.00775   0.00198  -0.1003   0.8209   0.0247
  -1.500   0.2680   0.00760   0.00179  -0.1000   0.8152   0.0267
  -1.250   0.2939   0.00750   0.00166  -0.0997   0.8093   0.0286
  -1.000   0.3198   0.00739   0.00151  -0.0994   0.8028   0.0330
  -0.750   0.3420   0.00684   0.00137  -0.0986   0.7965   0.2022
  -0.500   0.3594   0.00597   0.00123  -0.0970   0.7895   0.4566
  -0.250   0.3848   0.00586   0.00121  -0.0967   0.7832   0.5031
   0.000   0.4095   0.00574   0.00122  -0.0961   0.7763   0.5419
   0.250   0.4348   0.00568   0.00123  -0.0957   0.7696   0.5833
   0.500   0.4600   0.00561   0.00126  -0.0952   0.7628   0.6131
   0.750   0.4857   0.00561   0.00128  -0.0948   0.7556   0.6315
   1.000   0.5114   0.00560   0.00130  -0.0945   0.7482   0.6475
   1.250   0.5371   0.00562   0.00132  -0.0941   0.7405   0.6594
   1.500   0.5629   0.00563   0.00135  -0.0937   0.7321   0.6712
   1.750   0.5881   0.00566   0.00138  -0.0933   0.7234   0.6831
   2.000   0.6131   0.00568   0.00142  -0.0927   0.7134   0.6945
   2.250   0.6378   0.00572   0.00147  -0.0922   0.7024   0.7058
   2.500   0.6606   0.00578   0.00151  -0.0911   0.6855   0.7174
   2.750   0.6823   0.00588   0.00156  -0.0899   0.6663   0.7296
   3.000   0.7048   0.00595   0.00163  -0.0888   0.6488   0.7420
   3.250   0.7275   0.00604   0.00172  -0.0878   0.6340   0.7547
   3.500   0.7499   0.00613   0.00182  -0.0868   0.6190   0.7683
   3.750   0.7715   0.00624   0.00193  -0.0855   0.6025   0.7834
   4.000   0.7903   0.00641   0.00207  -0.0837   0.5791   0.8011
   4.250   0.8101   0.00656   0.00221  -0.0821   0.5566   0.8202
   4.500   0.8287   0.00674   0.00236  -0.0803   0.5325   0.8380
   4.750   0.8454   0.00697   0.00252  -0.0780   0.5000   0.8550
   5.000   0.8584   0.00726   0.00270  -0.0750   0.4613   0.8729
   5.250   0.8711   0.00755   0.00290  -0.0720   0.4235   0.8937
   5.500   0.8917   0.00802   0.00326  -0.0710   0.3689   0.9356
   5.750   0.9361   0.00889   0.00380  -0.0757   0.2932   1.0000
   6.000   0.9466   0.00944   0.00412  -0.0725   0.2463   1.0000
   6.250   0.9565   0.01006   0.00449  -0.0693   0.1983   1.0000
   6.500   0.9686   0.01064   0.00487  -0.0665   0.1588   1.0000
   6.750   0.9810   0.01122   0.00527  -0.0639   0.1249   1.0000
   7.000   0.9947   0.01177   0.00568  -0.0615   0.0962   1.0000
   7.250   1.0023   0.01265   0.00627  -0.0581   0.0496   1.0000
   7.500   1.0144   0.01334   0.00683  -0.0555   0.0292   1.0000
   7.750   1.0302   0.01384   0.00733  -0.0536   0.0248   1.0000
   8.000   1.0481   0.01424   0.00776  -0.0520   0.0233   1.0000
   8.250   1.0660   0.01465   0.00821  -0.0505   0.0221   1.0000
   8.500   1.0827   0.01513   0.00869  -0.0489   0.0205   1.0000
   8.750   1.0968   0.01577   0.00938  -0.0468   0.0188   1.0000
   9.000   1.1119   0.01636   0.01002  -0.0450   0.0178   1.0000
   9.250   1.1292   0.01681   0.01051  -0.0436   0.0172   1.0000
   9.500   1.1452   0.01736   0.01110  -0.0420   0.0163   1.0000
   9.750   1.1609   0.01792   0.01169  -0.0404   0.0155   1.0000
  10.000   1.1746   0.01861   0.01243  -0.0386   0.0147   1.0000
  10.250   1.1787   0.01992   0.01383  -0.0354   0.0135   1.0000
  10.500   1.1962   0.02041   0.01435  -0.0343   0.0132   1.0000
  10.750   1.2130   0.02095   0.01493  -0.0331   0.0124   1.0000
  11.000   1.2274   0.02165   0.01568  -0.0316   0.0118   1.0000
  11.250   1.2423   0.02233   0.01638  -0.0303   0.0112   1.0000
  11.500   1.2528   0.02332   0.01741  -0.0285   0.0106   1.0000
  11.750   1.2525   0.02508   0.01928  -0.0254   0.0099   1.0000
  12.000   1.2672   0.02583   0.02008  -0.0243   0.0097   1.0000
  12.250   1.2770   0.02694   0.02126  -0.0226   0.0095   1.0000
  12.500   1.2882   0.02798   0.02237  -0.0212   0.0090   1.0000
  12.750   1.3009   0.02891   0.02336  -0.0201   0.0086   1.0000
  13.000   1.3125   0.02993   0.02442  -0.0189   0.0082   1.0000
  13.250   1.3204   0.03128   0.02584  -0.0175   0.0080   1.0000
  13.500   1.3264   0.03283   0.02746  -0.0160   0.0078   1.0000
  13.750   1.3248   0.03504   0.02976  -0.0140   0.0074   1.0000
  14.000   1.3213   0.03753   0.03237  -0.0121   0.0073   1.0000
  14.250   1.3263   0.03934   0.03428  -0.0109   0.0071   1.0000
  14.500   1.3274   0.04157   0.03662  -0.0097   0.0071   1.0000
  14.750   1.3319   0.04353   0.03868  -0.0088   0.0069   1.0000
  15.000   1.3390   0.04530   0.04053  -0.0083   0.0068   1.0000
  15.250   1.3425   0.04749   0.04282  -0.0077   0.0065   1.0000
  15.500   1.3413   0.05024   0.04569  -0.0070   0.0064   1.0000
  15.750   1.3479   0.05223   0.04776  -0.0069   0.0062   1.0000
  16.000   1.3471   0.05509   0.05072  -0.0067   0.0061   1.0000
  16.250   1.3465   0.05806   0.05379  -0.0067   0.0059   1.0000
  16.500   1.3445   0.06127   0.05711  -0.0068   0.0058   1.0000
  16.750   1.3385   0.06505   0.06101  -0.0071   0.0058   1.0000
  17.000   1.3382   0.06828   0.06432  -0.0078   0.0057   1.0000
  17.250   1.3331   0.07221   0.06836  -0.0086   0.0056   1.0000
  17.500   1.3205   0.07726   0.07357  -0.0096   0.0057   1.0000
  17.750   1.3137   0.08174   0.07813  -0.0110   0.0055   1.0000
  18.000   1.3061   0.08644   0.08293  -0.0126   0.0054   1.0000
  18.250   1.2942   0.09190   0.08853  -0.0145   0.0054   1.0000
  18.500   1.2831   0.09746   0.09421  -0.0168   0.0053   1.0000
  18.750   1.2653   0.10424   0.10113  -0.0196   0.0053   1.0000
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