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AUGUST 160 (august160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AUGUST 160 (august160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.23 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-august160-il-1000000.txt
Download as CSV file: xf-august160-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AUGUST 160                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.1192   0.11917   0.11575  -0.0374   0.4897   0.0123
 -12.500  -0.1141   0.11616   0.11272  -0.0387   0.4851   0.0122
 -12.250  -0.1888   0.11992   0.11627  -0.0416   0.5021   0.0117
 -12.000  -0.1813   0.11698   0.11331  -0.0430   0.4956   0.0122
 -11.750  -0.1760   0.11338   0.10968  -0.0447   0.4892   0.0128
 -11.500  -0.1780   0.10780   0.10410  -0.0479   0.4870   0.0135
 -11.250  -0.1739   0.10398   0.10029  -0.0497   0.4826   0.0135
 -11.000  -0.1734   0.09915   0.09545  -0.0521   0.4785   0.0136
 -10.750  -0.1693   0.09548   0.09178  -0.0538   0.4734   0.0136
 -10.250  -0.0948   0.08255   0.07900  -0.0507   0.4473   0.0142
 -10.000  -0.0927   0.07901   0.07547  -0.0517   0.4440   0.0143
  -9.750  -0.0906   0.07556   0.07201  -0.0528   0.4398   0.0144
  -9.500  -0.0900   0.07189   0.06833  -0.0539   0.4356   0.0145
  -9.250  -0.0909   0.06806   0.06449  -0.0551   0.4319   0.0148
  -9.000  -0.0931   0.06399   0.06044  -0.0565   0.4294   0.0150
  -8.750  -0.0991   0.05935   0.05581  -0.0583   0.4277   0.0151
  -8.500  -0.1086   0.05432   0.05081  -0.0605   0.4255   0.0155
  -8.250  -0.1219   0.04912   0.04564  -0.0634   0.4241   0.0154
  -8.000  -0.1580   0.04238   0.03891  -0.0685   0.4248   0.0152
  -7.750  -0.1862   0.03784   0.03431  -0.0670   0.4239   0.0153
  -7.500  -0.2022   0.03277   0.02913  -0.0659   0.4222   0.0152
  -7.250  -0.2657   0.01873   0.01433  -0.0601   0.4268   0.0170
  -7.000  -0.2530   0.01719   0.01270  -0.0586   0.4219   0.0171
  -6.750  -0.2385   0.01594   0.01134  -0.0572   0.4164   0.0173
  -6.500  -0.2219   0.01497   0.01029  -0.0559   0.4112   0.0176
  -6.250  -0.2224   0.01150   0.00615  -0.0518   0.4090   0.0201
  -6.000  -0.2021   0.01046   0.00510  -0.0509   0.4044   0.0204
  -5.750  -0.1815   0.00972   0.00429  -0.0500   0.3992   0.0207
  -5.500  -0.1608   0.00904   0.00351  -0.0490   0.3937   0.0213
  -5.250  -0.1505   0.01731   0.01061  -0.0470   0.3935   0.0160
  -5.000  -0.1269   0.01610   0.00926  -0.0459   0.3902   0.0155
  -4.750  -0.1027   0.01502   0.00801  -0.0448   0.3860   0.0151
  -4.500  -0.0774   0.01463   0.00753  -0.0441   0.3815   0.0155
  -4.250  -0.0528   0.01401   0.00679  -0.0432   0.3763   0.0154
  -4.000  -0.0274   0.01338   0.00610  -0.0424   0.3737   0.0153
  -3.750  -0.0022   0.01290   0.00557  -0.0416   0.3705   0.0152
  -3.500   0.0229   0.01249   0.00511  -0.0408   0.3670   0.0153
  -3.250   0.0479   0.01217   0.00473  -0.0400   0.3630   0.0156
  -3.000   0.0727   0.01192   0.00442  -0.0391   0.3587   0.0159
  -2.750   0.0988   0.01168   0.00415  -0.0385   0.3568   0.0163
  -2.500   0.1247   0.01145   0.00390  -0.0378   0.3546   0.0164
  -2.250   0.1501   0.01117   0.00360  -0.0371   0.3521   0.0169
  -2.000   0.1755   0.01094   0.00334  -0.0364   0.3494   0.0173
  -1.750   0.2014   0.01080   0.00318  -0.0358   0.3467   0.0178
  -1.500   0.2274   0.01071   0.00305  -0.0352   0.3435   0.0183
  -1.250   0.2535   0.01065   0.00296  -0.0346   0.3407   0.0188
  -1.000   0.2804   0.01054   0.00285  -0.0342   0.3394   0.0195
  -0.750   0.3070   0.01044   0.00274  -0.0337   0.3377   0.0208
  -0.500   0.3338   0.01036   0.00266  -0.0333   0.3358   0.0227
  -0.250   0.3595   0.01021   0.00259  -0.0327   0.3338   0.0461
   0.000   0.3827   0.00987   0.00255  -0.0317   0.3317   0.1480
   0.250   0.4057   0.00958   0.00254  -0.0308   0.3297   0.2469
   0.500   0.4258   0.00917   0.00256  -0.0293   0.3273   0.3984
   0.750   0.4423   0.00873   0.00262  -0.0271   0.3245   0.5761
   1.000   0.4487   0.00797   0.00265  -0.0224   0.3239   0.8081
   1.250   0.4740   0.00788   0.00283  -0.0214   0.3228   0.9117
   1.500   0.5027   0.00798   0.00295  -0.0212   0.3215   0.9410
   1.750   0.5358   0.00812   0.00309  -0.0219   0.3200   0.9585
   2.000   0.5681   0.00825   0.00319  -0.0226   0.3185   0.9670
   2.250   0.6069   0.00839   0.00329  -0.0248   0.3167   0.9702
   2.500   0.6437   0.00856   0.00341  -0.0266   0.3150   0.9752
   2.750   0.6844   0.00874   0.00354  -0.0293   0.3131   0.9774
   3.000   0.7241   0.00895   0.00369  -0.0318   0.3106   0.9787
   3.250   0.7635   0.00922   0.00391  -0.0343   0.3079   0.9805
   3.500   0.8018   0.00932   0.00400  -0.0364   0.3072   0.9828
   3.750   0.8356   0.00942   0.00409  -0.0377   0.3062   0.9861
   4.000   0.8773   0.00951   0.00416  -0.0406   0.3047   0.9873
   4.250   0.9134   0.00960   0.00423  -0.0424   0.3032   0.9884
   4.500   0.9486   0.00967   0.00429  -0.0441   0.3014   0.9898
   4.750   0.9812   0.00976   0.00436  -0.0452   0.2996   0.9911
   5.000   1.0113   0.00986   0.00444  -0.0458   0.2977   0.9924
   5.250   1.0413   0.01001   0.00457  -0.0465   0.2957   0.9939
   5.500   1.0723   0.01019   0.00472  -0.0474   0.2940   0.9951
   5.750   1.1077   0.01041   0.00493  -0.0492   0.2921   0.9967
   6.000   1.1461   0.01049   0.00502  -0.0516   0.2916   0.9986
   6.250   1.1766   0.01058   0.00514  -0.0524   0.2910   0.9995
   6.500   1.2053   0.01068   0.00525  -0.0528   0.2902   1.0000
   6.750   1.2267   0.01080   0.00540  -0.0517   0.2896   1.0000
   7.000   1.2480   0.01092   0.00554  -0.0506   0.2888   1.0000
   7.250   1.2690   0.01104   0.00568  -0.0495   0.2879   1.0000
   7.500   1.2894   0.01118   0.00584  -0.0482   0.2871   1.0000
   7.750   1.3096   0.01132   0.00600  -0.0469   0.2864   1.0000
   8.000   1.3295   0.01145   0.00616  -0.0456   0.2855   1.0000
   8.250   1.3493   0.01157   0.00630  -0.0443   0.2842   1.0000
   8.500   1.3683   0.01172   0.00646  -0.0428   0.2831   1.0000
   8.750   1.3867   0.01187   0.00662  -0.0412   0.2815   1.0000
   9.000   1.4041   0.01207   0.00682  -0.0394   0.2795   1.0000
   9.250   1.4208   0.01236   0.00711  -0.0376   0.2774   1.0000
   9.500   1.4406   0.01252   0.00731  -0.0364   0.2768   1.0000
   9.750   1.4621   0.01263   0.00746  -0.0354   0.2759   1.0000
  10.000   1.4837   0.01279   0.00767  -0.0345   0.2752   1.0000
  10.250   1.5058   0.01293   0.00785  -0.0338   0.2739   1.0000
  10.500   1.5281   0.01308   0.00803  -0.0331   0.2725   1.0000
  10.750   1.5502   0.01324   0.00824  -0.0324   0.2710   1.0000
  11.000   1.5720   0.01341   0.00843  -0.0317   0.2692   1.0000
  11.250   1.5929   0.01363   0.00867  -0.0308   0.2674   1.0000
  11.500   1.6122   0.01391   0.00896  -0.0298   0.2648   1.0000
  11.750   1.6309   0.01425   0.00931  -0.0287   0.2623   1.0000
  12.000   1.6524   0.01440   0.00953  -0.0280   0.2609   1.0000
  12.250   1.6721   0.01458   0.00978  -0.0270   0.2593   1.0000
  12.500   1.6914   0.01479   0.01004  -0.0259   0.2573   1.0000
  12.750   1.7098   0.01505   0.01034  -0.0248   0.2553   1.0000
  13.000   1.7267   0.01537   0.01069  -0.0236   0.2524   1.0000
  13.250   1.7416   0.01581   0.01115  -0.0222   0.2498   1.0000
  13.500   1.7584   0.01621   0.01161  -0.0212   0.2475   1.0000
  13.750   1.7784   0.01649   0.01197  -0.0206   0.2450   1.0000
  14.000   1.7959   0.01691   0.01243  -0.0199   0.2407   1.0000
  14.250   1.8091   0.01755   0.01310  -0.0188   0.2363   1.0000
  14.500   1.8237   0.01819   0.01379  -0.0180   0.2316   1.0000
  14.750   1.8332   0.01918   0.01479  -0.0170   0.2228   1.0000
  15.000   1.8359   0.02076   0.01637  -0.0159   0.2118   1.0000
  15.250   1.8300   0.02326   0.01886  -0.0150   0.2003   1.0000
  15.500   1.8191   0.02656   0.02218  -0.0147   0.1890   1.0000
  15.750   1.7911   0.03182   0.02746  -0.0149   0.1743   1.0000
  16.000   1.7575   0.03787   0.03356  -0.0153   0.1653   1.0000
  16.250   1.7259   0.04381   0.03958  -0.0158   0.1604   1.0000
  16.500   1.6904   0.05022   0.04609  -0.0164   0.1562   1.0000
  16.750   1.6537   0.05693   0.05289  -0.0172   0.1521   1.0000
  17.000   1.6160   0.06408   0.06013  -0.0183   0.1488   1.0000
  17.250   1.5854   0.07059   0.06672  -0.0195   0.1445   1.0000
  17.500   1.5558   0.07712   0.07333  -0.0208   0.1386   1.0000
  17.750   1.5231   0.08421   0.08048  -0.0224   0.1333   1.0000
  18.000   1.4886   0.09167   0.08797  -0.0242   0.1242   1.0000
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