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Apex 16 (normalized using XFOIL date021206) (apex16-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Apex 16 (normalized using XFOIL date021206) (apex16-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.41 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-apex16-il-1000000-n5.txt
Download as CSV file: xf-apex16-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.3281   0.08492   0.08314  -0.0804   0.9827   0.0076
 -10.250  -0.3291   0.07829   0.07654  -0.0859   0.9801   0.0078
 -10.000  -0.3316   0.07031   0.06855  -0.0946   0.9777   0.0077
  -9.750  -0.3534   0.06103   0.05916  -0.1055   0.9708   0.0078
  -9.500  -0.3630   0.05478   0.05276  -0.1132   0.9646   0.0079
  -9.250  -0.3633   0.04951   0.04729  -0.1168   0.9581   0.0080
  -9.000  -0.3609   0.04481   0.04238  -0.1183   0.9510   0.0081
  -8.750  -0.3502   0.04061   0.03796  -0.1191   0.9448   0.0084
  -8.500  -0.3441   0.03713   0.03427  -0.1180   0.9366   0.0084
  -8.250  -0.3472   0.03179   0.02857  -0.1158   0.9275   0.0087
  -8.000  -0.3368   0.02867   0.02520  -0.1142   0.9205   0.0088
  -7.750  -0.3231   0.02600   0.02230  -0.1128   0.9142   0.0089
  -7.500  -0.3058   0.02415   0.02028  -0.1117   0.9073   0.0091
  -7.250  -0.2851   0.02298   0.01897  -0.1111   0.9014   0.0093
  -7.000  -0.2700   0.01979   0.01547  -0.1093   0.8934   0.0095
  -6.750  -0.2501   0.01777   0.01320  -0.1082   0.8864   0.0098
  -6.500  -0.2288   0.01627   0.01152  -0.1073   0.8789   0.0101
  -6.250  -0.2059   0.01502   0.01009  -0.1066   0.8726   0.0105
  -6.000  -0.1824   0.01421   0.00916  -0.1060   0.8664   0.0110
  -5.750  -0.1589   0.01330   0.00811  -0.1055   0.8603   0.0111
  -5.500  -0.1350   0.01268   0.00742  -0.1049   0.8545   0.0114
  -5.250  -0.1114   0.01208   0.00673  -0.1043   0.8484   0.0117
  -5.000  -0.0875   0.01158   0.00615  -0.1037   0.8428   0.0118
  -4.750  -0.0640   0.01111   0.00562  -0.1031   0.8364   0.0120
  -4.500  -0.0404   0.01071   0.00514  -0.1024   0.8308   0.0121
  -4.250  -0.0161   0.01041   0.00480  -0.1019   0.8253   0.0123
  -4.000   0.0081   0.01011   0.00445  -0.1014   0.8195   0.0124
  -3.750   0.0276   0.00936   0.00361  -0.1000   0.8138   0.0130
  -3.500   0.0508   0.00899   0.00318  -0.0993   0.8081   0.0135
  -3.250   0.0754   0.00876   0.00290  -0.0988   0.8029   0.0140
  -3.000   0.1007   0.00856   0.00268  -0.0985   0.7979   0.0145
  -2.750   0.1259   0.00839   0.00247  -0.0981   0.7922   0.0151
  -2.500   0.1513   0.00823   0.00226  -0.0978   0.7872   0.0156
  -2.250   0.1771   0.00807   0.00207  -0.0975   0.7818   0.0162
  -2.000   0.2028   0.00795   0.00191  -0.0972   0.7760   0.0168
  -1.750   0.2287   0.00784   0.00176  -0.0969   0.7705   0.0172
  -1.500   0.2548   0.00775   0.00165  -0.0966   0.7641   0.0178
  -1.250   0.2806   0.00770   0.00156  -0.0963   0.7576   0.0182
  -1.000   0.3065   0.00758   0.00140  -0.0960   0.7504   0.0198
  -0.750   0.3320   0.00753   0.00131  -0.0956   0.7429   0.0228
  -0.500   0.3580   0.00747   0.00125  -0.0953   0.7348   0.0270
  -0.250   0.3830   0.00737   0.00122  -0.0949   0.7267   0.0666
   0.000   0.4012   0.00652   0.00106  -0.0935   0.7176   0.3605
   0.250   0.4244   0.00628   0.00105  -0.0928   0.7085   0.4389
   0.500   0.4478   0.00614   0.00106  -0.0920   0.6985   0.4970
   0.750   0.4725   0.00610   0.00108  -0.0915   0.6878   0.5261
   1.000   0.4969   0.00607   0.00111  -0.0909   0.6765   0.5557
   1.250   0.5215   0.00610   0.00114  -0.0903   0.6644   0.5728
   1.500   0.5459   0.00616   0.00118  -0.0897   0.6514   0.5819
   1.750   0.5702   0.00623   0.00123  -0.0891   0.6379   0.5913
   2.000   0.5939   0.00631   0.00129  -0.0883   0.6230   0.6011
   2.250   0.6171   0.00642   0.00136  -0.0875   0.6064   0.6106
   2.750   0.6599   0.00674   0.00155  -0.0850   0.5594   0.6325
   3.000   0.6809   0.00691   0.00166  -0.0837   0.5334   0.6435
   3.250   0.7028   0.00707   0.00177  -0.0826   0.5113   0.6547
   3.500   0.7220   0.00733   0.00192  -0.0810   0.4776   0.6658
   3.750   0.7385   0.00769   0.00212  -0.0788   0.4325   0.6768
   4.000   0.7558   0.00803   0.00232  -0.0769   0.3925   0.6887
   4.250   0.7755   0.00827   0.00249  -0.0754   0.3670   0.6998
   4.500   0.7916   0.00861   0.00271  -0.0732   0.3309   0.7117
   4.750   0.8076   0.00894   0.00294  -0.0710   0.2954   0.7231
   5.000   0.8224   0.00934   0.00319  -0.0686   0.2566   0.7357
   5.250   0.8368   0.00977   0.00349  -0.0662   0.2179   0.7482
   5.500   0.8518   0.01017   0.00379  -0.0639   0.1849   0.7641
   5.750   0.8639   0.01069   0.00416  -0.0610   0.1429   0.7826
   6.000   0.8781   0.01110   0.00451  -0.0586   0.1148   0.8051
   6.250   0.8942   0.01141   0.00482  -0.0565   0.0968   0.8310
   6.500   0.9086   0.01181   0.00516  -0.0541   0.0747   0.8521
   7.000   0.9360   0.01272   0.00601  -0.0493   0.0277   0.9113
   7.250   0.9911   0.01324   0.00660  -0.0562   0.0211   1.0000
   7.500   1.0097   0.01360   0.00696  -0.0548   0.0190   1.0000
   7.750   1.0286   0.01394   0.00732  -0.0534   0.0180   1.0000
   8.000   1.0477   0.01427   0.00768  -0.0521   0.0174   1.0000
   8.250   1.0663   0.01463   0.00806  -0.0508   0.0166   1.0000
   8.500   1.0842   0.01503   0.00850  -0.0494   0.0157   1.0000
   8.750   1.1016   0.01547   0.00894  -0.0479   0.0146   1.0000
   9.000   1.1182   0.01596   0.00946  -0.0463   0.0135   1.0000
   9.250   1.1342   0.01650   0.01003  -0.0447   0.0128   1.0000
   9.500   1.1523   0.01691   0.01048  -0.0434   0.0126   1.0000
   9.750   1.1696   0.01737   0.01098  -0.0421   0.0122   1.0000
  10.000   1.1865   0.01786   0.01150  -0.0407   0.0118   1.0000
  10.250   1.2026   0.01841   0.01211  -0.0393   0.0112   1.0000
  10.500   1.2190   0.01894   0.01267  -0.0379   0.0106   1.0000
  10.750   1.2351   0.01950   0.01325  -0.0366   0.0099   1.0000
  11.000   1.2494   0.02018   0.01395  -0.0350   0.0091   1.0000
  11.250   1.2630   0.02093   0.01474  -0.0334   0.0085   1.0000
  11.500   1.2782   0.02156   0.01542  -0.0321   0.0082   1.0000
  11.750   1.2925   0.02227   0.01618  -0.0307   0.0078   1.0000
  12.000   1.3063   0.02303   0.01699  -0.0293   0.0074   1.0000
  12.250   1.3198   0.02382   0.01782  -0.0280   0.0070   1.0000
  12.500   1.3327   0.02466   0.01871  -0.0266   0.0065   1.0000
  12.750   1.3445   0.02559   0.01967  -0.0252   0.0060   1.0000
  13.000   1.3535   0.02677   0.02091  -0.0235   0.0055   1.0000
  13.250   1.3638   0.02786   0.02206  -0.0221   0.0054   1.0000
  13.500   1.3749   0.02890   0.02317  -0.0208   0.0052   1.0000
  13.750   1.3832   0.03018   0.02453  -0.0193   0.0051   1.0000
  14.000   1.3920   0.03147   0.02589  -0.0180   0.0049   1.0000
  14.250   1.4006   0.03280   0.02730  -0.0168   0.0048   1.0000
  14.500   1.4077   0.03427   0.02884  -0.0156   0.0046   1.0000
  14.750   1.4142   0.03584   0.03048  -0.0144   0.0044   1.0000
  15.000   1.4196   0.03756   0.03229  -0.0133   0.0043   1.0000
  15.250   1.4248   0.03934   0.03416  -0.0123   0.0043   1.0000
  15.500   1.4297   0.04120   0.03610  -0.0114   0.0041   1.0000
  15.750   1.4324   0.04333   0.03830  -0.0105   0.0039   1.0000
  16.000   1.4326   0.04579   0.04085  -0.0097   0.0037   1.0000
  16.250   1.4333   0.04828   0.04345  -0.0091   0.0036   1.0000
  16.500   1.4322   0.05104   0.04631  -0.0087   0.0035   1.0000
  16.750   1.4265   0.05444   0.04984  -0.0084   0.0034   1.0000
  17.000   1.4251   0.05745   0.05296  -0.0084   0.0034   1.0000
  17.250   1.4212   0.06089   0.05651  -0.0085   0.0034   1.0000
  17.500   1.4195   0.06412   0.05984  -0.0089   0.0033   1.0000
  17.750   1.4161   0.06765   0.06348  -0.0094   0.0033   1.0000
  18.000   1.4107   0.07157   0.06752  -0.0102   0.0032   1.0000
  18.250   1.4032   0.07590   0.07197  -0.0112   0.0032   1.0000
  18.500   1.3919   0.08094   0.07714  -0.0126   0.0032   1.0000
  18.750   1.3816   0.08593   0.08226  -0.0142   0.0032   1.0000
  19.000   1.3714   0.09108   0.08753  -0.0161   0.0031   1.0000
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