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Dayton-Wright T-1 (daytonwrightt1-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Dayton-Wright T-1 (daytonwrightt1-il)
Reynolds number: 500,000
Max Cl/Cd: 84.45 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-daytonwrightt1-il-500000-n5.txt
Download as CSV file: xf-daytonwrightt1-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Dayton-Wright T-1                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7493   0.05931   0.05621  -0.0860   1.0000   0.0262
 -15.250  -0.8146   0.03916   0.03555  -0.1115   0.9920   0.0260
 -15.000  -0.8123   0.03535   0.03148  -0.1148   0.9849   0.0262
 -14.750  -0.8030   0.03282   0.02874  -0.1159   0.9788   0.0264
 -14.500  -0.7888   0.03080   0.02653  -0.1165   0.9734   0.0266
 -14.250  -0.7711   0.02912   0.02467  -0.1169   0.9692   0.0269
 -14.000  -0.7554   0.02775   0.02312  -0.1163   0.9628   0.0272
 -13.750  -0.7356   0.02643   0.02163  -0.1162   0.9586   0.0275
 -13.500  -0.7174   0.02528   0.02031  -0.1154   0.9531   0.0276
 -13.250  -0.6983   0.02424   0.01912  -0.1146   0.9474   0.0278
 -13.000  -0.6767   0.02328   0.01800  -0.1140   0.9432   0.0280
 -12.750  -0.6571   0.02235   0.01694  -0.1130   0.9378   0.0281
 -12.500  -0.6384   0.02122   0.01570  -0.1119   0.9320   0.0284
 -12.250  -0.6167   0.02033   0.01471  -0.1111   0.9275   0.0287
 -12.000  -0.5951   0.01960   0.01391  -0.1102   0.9221   0.0290
 -11.750  -0.5727   0.01894   0.01317  -0.1093   0.9162   0.0292
 -11.500  -0.5490   0.01834   0.01248  -0.1086   0.9111   0.0296
 -11.250  -0.5254   0.01780   0.01187  -0.1078   0.9055   0.0299
 -11.000  -0.5015   0.01727   0.01127  -0.1070   0.8999   0.0303
 -10.750  -0.4769   0.01674   0.01065  -0.1063   0.8952   0.0307
 -10.500  -0.4524   0.01624   0.01006  -0.1056   0.8903   0.0310
 -10.250  -0.4278   0.01576   0.00951  -0.1050   0.8849   0.0313
 -10.000  -0.4025   0.01530   0.00897  -0.1043   0.8800   0.0316
  -9.750  -0.3770   0.01487   0.00845  -0.1038   0.8754   0.0320
  -9.500  -0.3516   0.01447   0.00799  -0.1031   0.8699   0.0323
  -9.250  -0.3257   0.01410   0.00754  -0.1026   0.8648   0.0326
  -8.750  -0.2742   0.01330   0.00663  -0.1015   0.8547   0.0334
  -8.500  -0.2482   0.01292   0.00621  -0.1010   0.8493   0.0340
  -8.250  -0.2216   0.01260   0.00583  -0.1006   0.8443   0.0346
  -8.000  -0.1951   0.01231   0.00551  -0.1001   0.8389   0.0353
  -7.750  -0.1684   0.01205   0.00521  -0.0997   0.8330   0.0361
  -7.500  -0.1412   0.01181   0.00491  -0.0994   0.8278   0.0370
  -7.250  -0.1143   0.01159   0.00465  -0.0990   0.8219   0.0378
  -7.000  -0.0872   0.01136   0.00438  -0.0986   0.8157   0.0387
  -6.750  -0.0601   0.01112   0.00410  -0.0983   0.8101   0.0401
  -6.500  -0.0331   0.01090   0.00388  -0.0979   0.8034   0.0418
  -6.250  -0.0058   0.01072   0.00366  -0.0976   0.7968   0.0440
  -6.000   0.0213   0.01052   0.00346  -0.0973   0.7901   0.0477
  -5.750   0.0483   0.01033   0.00328  -0.0969   0.7826   0.0540
  -5.500   0.0754   0.01016   0.00312  -0.0966   0.7753   0.0642
  -5.250   0.1024   0.01000   0.00299  -0.0963   0.7666   0.0749
  -5.000   0.1292   0.00988   0.00285  -0.0959   0.7559   0.0843
  -4.750   0.1557   0.00979   0.00272  -0.0954   0.7421   0.0927
  -4.500   0.1819   0.00970   0.00260  -0.0949   0.7271   0.1018
  -4.250   0.2084   0.00962   0.00251  -0.0945   0.7132   0.1109
  -4.000   0.2346   0.00957   0.00243  -0.0940   0.6982   0.1210
  -3.750   0.2602   0.00953   0.00235  -0.0934   0.6805   0.1343
  -3.500   0.2856   0.00951   0.00230  -0.0928   0.6625   0.1506
  -3.250   0.3112   0.00948   0.00226  -0.0923   0.6467   0.1676
  -3.000   0.3371   0.00944   0.00224  -0.0918   0.6334   0.1873
  -2.750   0.3629   0.00941   0.00224  -0.0914   0.6214   0.2099
  -2.500   0.3887   0.00942   0.00225  -0.0909   0.6087   0.2308
  -2.250   0.4143   0.00945   0.00226  -0.0904   0.5952   0.2486
  -2.000   0.4402   0.00948   0.00228  -0.0900   0.5812   0.2639
  -1.750   0.4660   0.00953   0.00232  -0.0895   0.5679   0.2792
  -1.500   0.4917   0.00958   0.00236  -0.0891   0.5554   0.2949
  -1.250   0.5172   0.00964   0.00240  -0.0886   0.5424   0.3091
  -1.000   0.5428   0.00971   0.00245  -0.0882   0.5289   0.3238
  -0.750   0.5681   0.00977   0.00252  -0.0877   0.5151   0.3431
  -0.500   0.5932   0.00984   0.00259  -0.0872   0.5009   0.3626
  -0.250   0.6181   0.00993   0.00266  -0.0867   0.4863   0.3804
   0.000   0.6427   0.01003   0.00275  -0.0861   0.4706   0.3994
   0.250   0.6668   0.01013   0.00284  -0.0855   0.4538   0.4241
   0.500   0.6901   0.01018   0.00294  -0.0848   0.4359   0.4669
   0.750   0.7007   0.00930   0.00314  -0.0812   0.4209   0.8611
   1.000   0.7406   0.00952   0.00343  -0.0837   0.4009   0.9458
   1.250   0.7804   0.00983   0.00364  -0.0866   0.3826   0.9742
   1.500   0.8150   0.01012   0.00383  -0.0883   0.3667   0.9865
   1.750   0.8500   0.01040   0.00402  -0.0902   0.3523   0.9944
   2.000   0.8863   0.01068   0.00421  -0.0924   0.3394   0.9993
   2.500   0.9285   0.01110   0.00453  -0.0901   0.3206   1.0000
   2.750   0.9474   0.01133   0.00470  -0.0885   0.3125   1.0000
   3.000   0.9674   0.01151   0.00486  -0.0872   0.3057   1.0000
   3.250   0.9867   0.01173   0.00504  -0.0856   0.2988   1.0000
   3.500   1.0061   0.01194   0.00523  -0.0842   0.2931   1.0000
   3.750   1.0261   0.01215   0.00542  -0.0829   0.2866   1.0000
   4.250   1.0650   0.01264   0.00585  -0.0801   0.2724   1.0000
   4.500   1.0837   0.01290   0.00608  -0.0786   0.2662   1.0000
   4.750   1.1020   0.01316   0.00633  -0.0770   0.2620   1.0000
   5.000   1.1221   0.01337   0.00656  -0.0758   0.2580   1.0000
   5.250   1.1417   0.01362   0.00682  -0.0746   0.2534   1.0000
   5.500   1.1609   0.01392   0.00710  -0.0733   0.2493   1.0000
   5.750   1.1802   0.01423   0.00741  -0.0721   0.2455   1.0000
   6.000   1.2011   0.01449   0.00770  -0.0712   0.2421   1.0000
   6.250   1.2213   0.01479   0.00802  -0.0703   0.2379   1.0000
   6.500   1.2403   0.01515   0.00838  -0.0692   0.2334   1.0000
   6.750   1.2593   0.01553   0.00876  -0.0681   0.2291   1.0000
   7.000   1.2798   0.01584   0.00910  -0.0673   0.2241   1.0000
   7.250   1.2982   0.01626   0.00951  -0.0662   0.2179   1.0000
   7.500   1.3165   0.01669   0.00995  -0.0652   0.2128   1.0000
   7.750   1.3363   0.01706   0.01036  -0.0644   0.2079   1.0000
   8.000   1.3539   0.01755   0.01085  -0.0633   0.2015   1.0000
   8.250   1.3719   0.01803   0.01134  -0.0624   0.1949   1.0000
   8.500   1.3891   0.01856   0.01187  -0.0613   0.1869   1.0000
   8.750   1.4060   0.01912   0.01244  -0.0603   0.1788   1.0000
   9.000   1.4206   0.01983   0.01311  -0.0590   0.1648   1.0000
   9.250   1.4286   0.02096   0.01408  -0.0570   0.1383   1.0000
   9.500   1.4337   0.02232   0.01530  -0.0548   0.1168   1.0000
   9.750   1.4407   0.02360   0.01652  -0.0529   0.1036   1.0000
  10.250   1.4580   0.02603   0.01893  -0.0497   0.0861   1.0000
  10.500   1.4659   0.02734   0.02023  -0.0482   0.0787   1.0000
  10.750   1.4725   0.02878   0.02166  -0.0467   0.0709   1.0000
  11.000   1.4795   0.03023   0.02311  -0.0454   0.0622   1.0000
  11.250   1.4823   0.03205   0.02489  -0.0438   0.0503   1.0000
  11.500   1.4787   0.03446   0.02723  -0.0420   0.0359   1.0000
  11.750   1.4754   0.03698   0.02973  -0.0404   0.0270   1.0000
  12.000   1.4753   0.03932   0.03210  -0.0392   0.0227   1.0000
  12.250   1.4762   0.04167   0.03451  -0.0383   0.0202   1.0000
  12.500   1.4785   0.04398   0.03689  -0.0376   0.0188   1.0000
  12.750   1.4795   0.04649   0.03947  -0.0370   0.0176   1.0000
  13.000   1.4792   0.04923   0.04230  -0.0366   0.0167   1.0000
  13.250   1.4800   0.05194   0.04510  -0.0364   0.0160   1.0000
  13.500   1.4797   0.05485   0.04810  -0.0362   0.0155   1.0000
  13.750   1.4780   0.05802   0.05136  -0.0362   0.0150   1.0000
  14.000   1.4747   0.06143   0.05487  -0.0364   0.0145   1.0000
  14.250   1.4698   0.06514   0.05868  -0.0366   0.0141   1.0000
  14.500   1.4632   0.06917   0.06282  -0.0371   0.0138   1.0000
  14.750   1.4547   0.07354   0.06730  -0.0377   0.0135   1.0000
  15.000   1.4470   0.07788   0.07174  -0.0384   0.0133   1.0000
  15.250   1.4395   0.08228   0.07626  -0.0392   0.0131   1.0000
  15.500   1.4308   0.08693   0.08103  -0.0402   0.0130   1.0000
  15.750   1.4209   0.09181   0.08603  -0.0414   0.0128   1.0000
  16.000   1.4103   0.09685   0.09119  -0.0427   0.0126   1.0000
  16.250   1.3995   0.10200   0.09645  -0.0441   0.0124   1.0000
  16.500   1.3888   0.10721   0.10177  -0.0456   0.0123   1.0000
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