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Dayton-Wright 6 (daytonwright6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Dayton-Wright 6 (daytonwright6-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.77 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-daytonwright6-il-1000000.txt
Download as CSV file: xf-daytonwright6-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1346   0.08563   0.08399  -0.0744   0.9810   0.0279
 -12.000  -0.1250   0.08276   0.08112  -0.0757   0.9757   0.0281
 -11.750  -0.1153   0.07922   0.07758  -0.0779   0.9722   0.0283
 -11.500  -0.4631   0.03071   0.02807  -0.1158   0.9493   0.0254
 -11.250  -0.4454   0.02699   0.02396  -0.1181   0.9404   0.0258
 -11.000  -0.4178   0.02421   0.02082  -0.1208   0.9306   0.0261
 -10.750  -0.3911   0.02212   0.01843  -0.1223   0.9186   0.0263
 -10.500  -0.3658   0.02054   0.01657  -0.1229   0.9054   0.0265
 -10.250  -0.3428   0.01946   0.01525  -0.1226   0.8918   0.0267
 -10.000  -0.3211   0.01869   0.01427  -0.1216   0.8799   0.0269
  -9.750  -0.3006   0.01817   0.01358  -0.1202   0.8694   0.0271
  -9.500  -0.2783   0.01799   0.01327  -0.1191   0.8609   0.0273
  -9.250  -0.2662   0.01588   0.01088  -0.1167   0.8520   0.0277
  -9.000  -0.2464   0.01494   0.00983  -0.1152   0.8449   0.0280
  -8.750  -0.2251   0.01430   0.00910  -0.1139   0.8378   0.0282
  -8.500  -0.2025   0.01377   0.00848  -0.1128   0.8313   0.0284
  -8.250  -0.1805   0.01325   0.00790  -0.1115   0.8250   0.0287
  -8.000  -0.1575   0.01284   0.00742  -0.1104   0.8180   0.0289
  -7.750  -0.1347   0.01242   0.00692  -0.1093   0.8115   0.0292
  -7.500  -0.1119   0.01203   0.00647  -0.1081   0.8039   0.0295
  -7.250  -0.0890   0.01167   0.00604  -0.1069   0.7956   0.0297
  -7.000  -0.0663   0.01134   0.00565  -0.1056   0.7864   0.0300
  -6.750  -0.0432   0.01103   0.00528  -0.1044   0.7780   0.0304
  -6.500  -0.0201   0.01073   0.00492  -0.1032   0.7690   0.0308
  -6.250   0.0030   0.01047   0.00461  -0.1021   0.7593   0.0311
  -6.000   0.0260   0.01028   0.00435  -0.1008   0.7477   0.0316
  -5.750   0.0487   0.01010   0.00411  -0.0995   0.7332   0.0319
  -5.500   0.0707   0.00994   0.00386  -0.0981   0.7150   0.0321
  -5.250   0.0898   0.00967   0.00347  -0.0960   0.6884   0.0326
  -5.000   0.1081   0.00953   0.00317  -0.0938   0.6581   0.0331
  -4.750   0.1273   0.00944   0.00296  -0.0919   0.6310   0.0338
  -4.500   0.1481   0.00939   0.00280  -0.0902   0.6086   0.0344
  -4.250   0.1698   0.00935   0.00266  -0.0888   0.5904   0.0350
  -4.000   0.1922   0.00930   0.00254  -0.0875   0.5755   0.0358
  -3.750   0.2153   0.00925   0.00242  -0.0863   0.5638   0.0367
  -3.250   0.2622   0.00912   0.00220  -0.0842   0.5446   0.0397
  -3.000   0.2849   0.00908   0.00212  -0.0830   0.5356   0.0424
  -2.750   0.3085   0.00895   0.00204  -0.0820   0.5281   0.0545
  -2.500   0.3307   0.00886   0.00202  -0.0807   0.5206   0.0820
  -2.250   0.3546   0.00879   0.00199  -0.0798   0.5140   0.0993
  -2.000   0.3782   0.00876   0.00198  -0.0788   0.5074   0.1134
  -1.750   0.4014   0.00875   0.00198  -0.0778   0.5011   0.1272
  -1.500   0.4256   0.00870   0.00197  -0.0770   0.4949   0.1444
  -1.250   0.4484   0.00868   0.00198  -0.0759   0.4882   0.1646
  -1.000   0.4719   0.00865   0.00199  -0.0749   0.4822   0.1868
  -0.750   0.4948   0.00858   0.00201  -0.0739   0.4759   0.2179
  -0.500   0.5160   0.00854   0.00204  -0.0725   0.4695   0.2617
  -0.250   0.5377   0.00839   0.00208  -0.0713   0.4641   0.3304
   0.000   0.5569   0.00819   0.00211  -0.0695   0.4577   0.4228
   0.500   0.7203   0.00773   0.00296  -0.0938   0.4359   0.9814
   0.750   0.7645   0.00789   0.00307  -0.0975   0.4274   0.9853
   1.000   0.8076   0.00808   0.00318  -0.1010   0.4184   0.9895
   1.250   0.8510   0.00827   0.00330  -0.1045   0.4087   0.9938
   1.500   0.8989   0.00837   0.00333  -0.1091   0.3987   0.9967
   2.000   0.9686   0.00859   0.00343  -0.1127   0.3805   1.0000
   2.250   0.9869   0.00874   0.00353  -0.1109   0.3727   1.0000
   2.500   1.0071   0.00885   0.00361  -0.1095   0.3659   1.0000
   2.750   1.0260   0.00900   0.00372  -0.1078   0.3593   1.0000
   3.000   1.0456   0.00913   0.00383  -0.1063   0.3535   1.0000
   3.250   1.0652   0.00926   0.00394  -0.1048   0.3476   1.0000
   3.500   1.0833   0.00945   0.00408  -0.1030   0.3413   1.0000
   3.750   1.1034   0.00956   0.00420  -0.1016   0.3371   1.0000
   4.000   1.1227   0.00971   0.00432  -0.1000   0.3322   1.0000
   4.250   1.1402   0.00991   0.00448  -0.0981   0.3263   1.0000
   4.500   1.1596   0.01004   0.00462  -0.0966   0.3218   1.0000
   4.750   1.1785   0.01018   0.00476  -0.0950   0.3174   1.0000
   5.000   1.1936   0.01039   0.00493  -0.0926   0.3113   1.0000
   5.250   1.2094   0.01052   0.00507  -0.0903   0.3069   1.0000
   5.500   1.2257   0.01064   0.00521  -0.0882   0.3029   1.0000
   5.750   1.2414   0.01081   0.00537  -0.0860   0.2988   1.0000
   6.000   1.2559   0.01104   0.00557  -0.0835   0.2932   1.0000
   6.250   1.2744   0.01116   0.00572  -0.0820   0.2890   1.0000
   6.500   1.2912   0.01135   0.00590  -0.0801   0.2838   1.0000
   6.750   1.3064   0.01161   0.00613  -0.0779   0.2786   1.0000
   7.000   1.3252   0.01176   0.00631  -0.0765   0.2740   1.0000
   7.250   1.3417   0.01200   0.00654  -0.0747   0.2673   1.0000
   7.500   1.3583   0.01226   0.00680  -0.0729   0.2618   1.0000
   7.750   1.3758   0.01250   0.00703  -0.0713   0.2545   1.0000
   8.000   1.3910   0.01283   0.00733  -0.0694   0.2461   1.0000
   8.250   1.4054   0.01322   0.00768  -0.0674   0.2345   1.0000
   8.500   1.4176   0.01370   0.00809  -0.0651   0.2192   1.0000
   8.750   1.4279   0.01429   0.00859  -0.0626   0.2005   1.0000
   9.000   1.4288   0.01533   0.00942  -0.0586   0.1695   1.0000
   9.250   1.4230   0.01674   0.01060  -0.0539   0.1347   1.0000
   9.500   1.4080   0.01873   0.01231  -0.0482   0.0918   1.0000
   9.750   1.3888   0.02117   0.01449  -0.0426   0.0511   1.0000
  10.000   1.3740   0.02360   0.01679  -0.0381   0.0215   1.0000
  10.250   1.3787   0.02493   0.01815  -0.0361   0.0181   1.0000
  10.500   1.3866   0.02611   0.01937  -0.0346   0.0170   1.0000
  10.750   1.3926   0.02747   0.02078  -0.0330   0.0161   1.0000
  11.000   1.3968   0.02902   0.02239  -0.0314   0.0152   1.0000
  11.250   1.4025   0.03051   0.02394  -0.0301   0.0150   1.0000
  11.500   1.4083   0.03205   0.02555  -0.0289   0.0145   1.0000
  11.750   1.4130   0.03376   0.02733  -0.0278   0.0142   1.0000
  12.000   1.4161   0.03567   0.02930  -0.0268   0.0137   1.0000
  12.250   1.4187   0.03771   0.03141  -0.0259   0.0133   1.0000
  12.500   1.4172   0.04025   0.03403  -0.0250   0.0130   1.0000
  12.750   1.4137   0.04314   0.03701  -0.0244   0.0126   1.0000
  13.000   1.4060   0.04663   0.04061  -0.0238   0.0123   1.0000
  13.250   1.4038   0.04964   0.04371  -0.0236   0.0122   1.0000
  13.500   1.4040   0.05246   0.04660  -0.0236   0.0120   1.0000
  13.750   1.4024   0.05552   0.04974  -0.0237   0.0118   1.0000
  14.000   1.3969   0.05911   0.05342  -0.0238   0.0116   1.0000
  14.250   1.3899   0.06294   0.05735  -0.0240   0.0116   1.0000
  14.500   1.3829   0.06684   0.06134  -0.0244   0.0114   1.0000
  14.750   1.3757   0.07079   0.06538  -0.0248   0.0113   1.0000
  15.000   1.3681   0.07488   0.06956  -0.0253   0.0110   1.0000
  15.250   1.3596   0.07916   0.07393  -0.0260   0.0110   1.0000
  15.500   1.3500   0.08365   0.07851  -0.0267   0.0109   1.0000
  15.750   1.3405   0.08817   0.08312  -0.0276   0.0108   1.0000
  16.000   1.3309   0.09279   0.08783  -0.0285   0.0107   1.0000
  16.250   1.3232   0.09720   0.09231  -0.0295   0.0105   1.0000
  16.500   1.3112   0.10229   0.09750  -0.0307   0.0105   1.0000
  16.750   1.3003   0.10726   0.10254  -0.0319   0.0102   1.0000
  17.000   1.2909   0.11209   0.10745  -0.0333   0.0102   1.0000
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