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Dayton-Wright 6 (daytonwright6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Dayton-Wright 6 (daytonwright6-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.24 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-daytonwright6-il-1000000-n5.txt
Download as CSV file: xf-daytonwright6-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Dayton-Wright 6                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7608   0.03508   0.03244  -0.1174   0.9862   0.0202
 -14.500  -0.7604   0.03223   0.02940  -0.1179   0.9804   0.0203
 -14.250  -0.7521   0.03035   0.02739  -0.1173   0.9740   0.0204
 -14.000  -0.7450   0.02851   0.02540  -0.1160   0.9656   0.0205
 -13.500  -0.7111   0.02557   0.02218  -0.1154   0.9511   0.0208
 -13.250  -0.6842   0.02419   0.02066  -0.1167   0.9449   0.0210
 -13.000  -0.6524   0.02292   0.01924  -0.1187   0.9357   0.0212
 -12.750  -0.6117   0.02165   0.01781  -0.1226   0.9276   0.0214
 -12.500  -0.5726   0.02050   0.01646  -0.1259   0.9153   0.0217
 -12.250  -0.5411   0.01947   0.01524  -0.1275   0.8976   0.0219
 -12.000  -0.5178   0.01869   0.01426  -0.1271   0.8785   0.0220
 -11.750  -0.4985   0.01807   0.01348  -0.1257   0.8625   0.0222
 -11.500  -0.4797   0.01758   0.01283  -0.1241   0.8491   0.0223
 -11.250  -0.4615   0.01702   0.01214  -0.1223   0.8381   0.0224
 -11.000  -0.4424   0.01650   0.01149  -0.1207   0.8294   0.0225
 -10.750  -0.4222   0.01608   0.01097  -0.1192   0.8215   0.0226
 -10.500  -0.4016   0.01562   0.01041  -0.1177   0.8157   0.0227
 -10.250  -0.3804   0.01519   0.00990  -0.1164   0.8096   0.0228
 -10.000  -0.3586   0.01483   0.00944  -0.1151   0.8038   0.0229
  -9.750  -0.3378   0.01429   0.00881  -0.1137   0.7990   0.0231
  -9.500  -0.3183   0.01361   0.00806  -0.1121   0.7934   0.0234
  -9.250  -0.2965   0.01321   0.00759  -0.1108   0.7876   0.0237
  -9.000  -0.2742   0.01282   0.00713  -0.1096   0.7819   0.0238
  -8.750  -0.2513   0.01248   0.00675  -0.1085   0.7753   0.0240
  -8.500  -0.2286   0.01219   0.00639  -0.1073   0.7686   0.0242
  -8.250  -0.2050   0.01189   0.00605  -0.1062   0.7614   0.0243
  -8.000  -0.1824   0.01164   0.00572  -0.1050   0.7523   0.0245
  -7.750  -0.1590   0.01139   0.00542  -0.1039   0.7414   0.0247
  -7.500  -0.1367   0.01117   0.00512  -0.1026   0.7263   0.0249
  -7.250  -0.1160   0.01100   0.00484  -0.1009   0.7015   0.0251
  -7.000  -0.0980   0.01095   0.00460  -0.0986   0.6601   0.0253
  -6.750  -0.0792   0.01093   0.00439  -0.0965   0.6230   0.0255
  -6.500  -0.0580   0.01084   0.00417  -0.0950   0.5986   0.0257
  -6.250  -0.0355   0.01073   0.00397  -0.0937   0.5814   0.0260
  -6.000  -0.0126   0.01062   0.00378  -0.0925   0.5672   0.0262
  -5.750   0.0107   0.01052   0.00360  -0.0914   0.5551   0.0265
  -5.500   0.0343   0.01041   0.00343  -0.0904   0.5439   0.0267
  -5.250   0.0583   0.01031   0.00327  -0.0894   0.5347   0.0269
  -5.000   0.0823   0.01022   0.00312  -0.0884   0.5263   0.0272
  -4.750   0.1068   0.01013   0.00299  -0.0876   0.5193   0.0274
  -4.500   0.1311   0.01004   0.00287  -0.0867   0.5120   0.0277
  -4.250   0.1548   0.00991   0.00269  -0.0857   0.5048   0.0283
  -4.000   0.1792   0.00979   0.00255  -0.0848   0.4988   0.0290
  -3.750   0.2033   0.00972   0.00244  -0.0839   0.4929   0.0296
  -3.500   0.2279   0.00965   0.00235  -0.0831   0.4877   0.0300
  -3.250   0.2526   0.00959   0.00227  -0.0823   0.4819   0.0306
  -3.000   0.2765   0.00956   0.00220  -0.0814   0.4750   0.0313
  -2.750   0.3012   0.00951   0.00214  -0.0806   0.4692   0.0320
  -2.500   0.3258   0.00948   0.00208  -0.0798   0.4634   0.0328
  -2.000   0.3741   0.00941   0.00199  -0.0780   0.4524   0.0376
  -1.750   0.3966   0.00926   0.00195  -0.0769   0.4462   0.0667
  -1.500   0.4199   0.00925   0.00194  -0.0759   0.4394   0.0781
  -1.250   0.4437   0.00923   0.00193  -0.0750   0.4321   0.0891
  -1.000   0.4667   0.00924   0.00194  -0.0740   0.4251   0.0997
  -0.500   0.5133   0.00922   0.00197  -0.0720   0.4116   0.1279
  -0.250   0.5360   0.00921   0.00200  -0.0710   0.4050   0.1479
   0.000   0.5584   0.00922   0.00203  -0.0698   0.3969   0.1677
   0.250   0.5805   0.00925   0.00207  -0.0687   0.3886   0.1855
   0.500   0.6018   0.00926   0.00212  -0.0673   0.3808   0.2124
   0.750   0.6219   0.00925   0.00217  -0.0658   0.3743   0.2480
   1.000   0.6408   0.00916   0.00224  -0.0640   0.3679   0.3147
   1.250   0.6580   0.00907   0.00232  -0.0619   0.3616   0.3980
   1.750   0.8284   0.00859   0.00322  -0.0883   0.3414   0.9795
   2.000   0.8685   0.00882   0.00340  -0.0912   0.3349   0.9871
   2.250   0.9018   0.00902   0.00355  -0.0927   0.3291   0.9904
   2.500   0.9338   0.00918   0.00368  -0.0938   0.3242   0.9932
   2.750   0.9927   0.00938   0.00382  -0.1010   0.3178   0.9979
   3.000   1.0356   0.00953   0.00393  -0.1047   0.3124   1.0000
   3.250   1.0558   0.00964   0.00403  -0.1033   0.3090   1.0000
   3.500   1.0756   0.00976   0.00415  -0.1018   0.3051   1.0000
   3.750   1.0945   0.00992   0.00428  -0.1002   0.3010   1.0000
   4.000   1.1133   0.01007   0.00441  -0.0985   0.2962   1.0000
   4.250   1.1330   0.01019   0.00454  -0.0970   0.2933   1.0000
   4.500   1.1513   0.01035   0.00468  -0.0953   0.2879   1.0000
   4.750   1.1680   0.01054   0.00484  -0.0932   0.2826   1.0000
   5.000   1.1844   0.01067   0.00497  -0.0911   0.2787   1.0000
   5.250   1.1999   0.01080   0.00511  -0.0888   0.2743   1.0000
   5.500   1.2138   0.01102   0.00529  -0.0862   0.2674   1.0000
   5.750   1.2306   0.01117   0.00544  -0.0842   0.2627   1.0000
   6.000   1.2460   0.01138   0.00563  -0.0820   0.2557   1.0000
   6.250   1.2619   0.01160   0.00584  -0.0799   0.2505   1.0000
   6.500   1.2783   0.01182   0.00604  -0.0780   0.2428   1.0000
   6.750   1.2933   0.01210   0.00629  -0.0759   0.2359   1.0000
   7.000   1.3088   0.01238   0.00655  -0.0739   0.2262   1.0000
   7.250   1.3235   0.01271   0.00685  -0.0718   0.2170   1.0000
   7.500   1.3359   0.01315   0.00722  -0.0693   0.2032   1.0000
   7.750   1.3460   0.01371   0.00768  -0.0666   0.1856   1.0000
   8.000   1.3480   0.01464   0.00842  -0.0626   0.1562   1.0000
   8.250   1.3525   0.01550   0.00915  -0.0591   0.1344   1.0000
   8.500   1.3481   0.01683   0.01027  -0.0545   0.1017   1.0000
   8.750   1.3212   0.01941   0.01250  -0.0471   0.0418   1.0000
   9.000   1.3168   0.02103   0.01404  -0.0432   0.0174   1.0000
   9.250   1.3270   0.02189   0.01491  -0.0415   0.0153   1.0000
   9.500   1.3374   0.02277   0.01582  -0.0398   0.0140   1.0000
   9.750   1.3486   0.02364   0.01673  -0.0384   0.0133   1.0000
  10.000   1.3591   0.02459   0.01772  -0.0370   0.0126   1.0000
  10.250   1.3687   0.02563   0.01880  -0.0356   0.0122   1.0000
  10.500   1.3768   0.02682   0.02003  -0.0341   0.0116   1.0000
  10.750   1.3840   0.02811   0.02137  -0.0327   0.0108   1.0000
  11.000   1.3924   0.02936   0.02267  -0.0315   0.0106   1.0000
  11.250   1.3999   0.03072   0.02408  -0.0304   0.0104   1.0000
  11.500   1.4070   0.03217   0.02558  -0.0293   0.0101   1.0000
  11.750   1.4130   0.03376   0.02724  -0.0283   0.0098   1.0000
  12.000   1.4176   0.03553   0.02906  -0.0274   0.0095   1.0000
  12.250   1.4215   0.03744   0.03102  -0.0266   0.0092   1.0000
  12.500   1.4247   0.03951   0.03315  -0.0259   0.0090   1.0000
  12.750   1.4254   0.04192   0.03563  -0.0253   0.0087   1.0000
  13.000   1.4248   0.04455   0.03835  -0.0248   0.0085   1.0000
  13.250   1.4243   0.04727   0.04114  -0.0245   0.0083   1.0000
  13.500   1.4255   0.04991   0.04385  -0.0244   0.0082   1.0000
  13.750   1.4256   0.05270   0.04671  -0.0244   0.0080   1.0000
  14.000   1.4243   0.05570   0.04979  -0.0244   0.0079   1.0000
  14.250   1.4209   0.05899   0.05317  -0.0245   0.0078   1.0000
  14.500   1.4178   0.06231   0.05656  -0.0247   0.0077   1.0000
  14.750   1.4112   0.06612   0.06047  -0.0250   0.0076   1.0000
  15.000   1.4079   0.06951   0.06393  -0.0254   0.0075   1.0000
  15.250   1.4013   0.07340   0.06791  -0.0259   0.0073   1.0000
  15.500   1.3949   0.07732   0.07191  -0.0264   0.0072   1.0000
  15.750   1.3875   0.08144   0.07611  -0.0271   0.0071   1.0000
  16.000   1.3794   0.08568   0.08044  -0.0278   0.0070   1.0000
  16.250   1.3735   0.08968   0.08452  -0.0286   0.0069   1.0000
  16.500   1.3647   0.09418   0.08910  -0.0295   0.0068   1.0000
  16.750   1.3566   0.09861   0.09360  -0.0306   0.0067   1.0000
  17.000   1.3490   0.10297   0.09804  -0.0316   0.0067   1.0000
  17.250   1.3393   0.10771   0.10286  -0.0328   0.0065   1.0000
  17.500   1.3303   0.11240   0.10764  -0.0341   0.0065   1.0000
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