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Dayton-Wright T-1 (daytonwrightt1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Dayton-Wright T-1 (daytonwrightt1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.93 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-daytonwrightt1-il-1000000.txt
Download as CSV file: xf-daytonwrightt1-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.3829   0.16447   0.16260  -0.0306   1.0000   0.0212
 -17.250  -0.3755   0.16160   0.15973  -0.0319   1.0000   0.0219
 -15.750  -0.8818   0.03810   0.03526  -0.1106   0.9974   0.0249
 -15.500  -0.8727   0.03493   0.03192  -0.1141   0.9942   0.0251
 -15.250  -0.8603   0.03259   0.02942  -0.1156   0.9900   0.0253
 -15.000  -0.8414   0.03066   0.02736  -0.1170   0.9869   0.0256
 -14.750  -0.8195   0.02890   0.02546  -0.1184   0.9848   0.0258
 -14.500  -0.7968   0.02731   0.02373  -0.1195   0.9828   0.0261
 -14.250  -0.7785   0.02597   0.02226  -0.1192   0.9780   0.0264
 -14.000  -0.7579   0.02476   0.02092  -0.1190   0.9735   0.0266
 -13.750  -0.7353   0.02379   0.01982  -0.1189   0.9698   0.0270
 -13.500  -0.7166   0.02297   0.01888  -0.1177   0.9639   0.0272
 -13.250  -0.6966   0.02216   0.01795  -0.1166   0.9584   0.0274
 -13.000  -0.6752   0.02146   0.01713  -0.1157   0.9537   0.0276
 -12.750  -0.6546   0.02088   0.01644  -0.1145   0.9475   0.0277
 -12.500  -0.6412   0.01891   0.01427  -0.1128   0.9412   0.0281
 -12.250  -0.6217   0.01787   0.01315  -0.1115   0.9354   0.0284
 -12.000  -0.6000   0.01714   0.01236  -0.1105   0.9296   0.0287
 -11.750  -0.5769   0.01654   0.01168  -0.1096   0.9247   0.0290
 -11.500  -0.5531   0.01600   0.01110  -0.1088   0.9198   0.0294
 -11.250  -0.5287   0.01554   0.01058  -0.1080   0.9146   0.0297
 -11.000  -0.5040   0.01508   0.01005  -0.1073   0.9099   0.0301
 -10.750  -0.4791   0.01460   0.00950  -0.1067   0.9053   0.0305
 -10.500  -0.4542   0.01412   0.00896  -0.1060   0.9003   0.0308
 -10.250  -0.4289   0.01368   0.00844  -0.1053   0.8954   0.0311
 -10.000  -0.4031   0.01327   0.00796  -0.1047   0.8908   0.0315
  -9.750  -0.3773   0.01289   0.00753  -0.1042   0.8861   0.0318
  -9.500  -0.3510   0.01256   0.00714  -0.1036   0.8812   0.0321
  -9.250  -0.3244   0.01227   0.00678  -0.1032   0.8765   0.0323
  -9.000  -0.3001   0.01159   0.00603  -0.1024   0.8717   0.0329
  -8.750  -0.2745   0.01115   0.00556  -0.1019   0.8667   0.0335
  -8.500  -0.2479   0.01083   0.00520  -0.1014   0.8616   0.0342
  -8.250  -0.2207   0.01059   0.00490  -0.1010   0.8568   0.0349
  -8.000  -0.1937   0.01032   0.00463  -0.1007   0.8518   0.0355
  -7.750  -0.1665   0.01008   0.00434  -0.1003   0.8466   0.0362
  -7.500  -0.1391   0.00988   0.00408  -0.1000   0.8414   0.0368
  -7.250  -0.1116   0.00968   0.00385  -0.0997   0.8362   0.0373
  -7.000  -0.0847   0.00937   0.00351  -0.0992   0.8305   0.0386
  -6.750  -0.0574   0.00915   0.00325  -0.0989   0.8249   0.0401
  -6.500  -0.0298   0.00896   0.00306  -0.0987   0.8193   0.0416
  -6.250  -0.0021   0.00881   0.00287  -0.0984   0.8129   0.0431
  -6.000   0.0252   0.00861   0.00266  -0.0980   0.8065   0.0471
  -5.750   0.0523   0.00839   0.00248  -0.0977   0.7980   0.0549
  -5.500   0.0789   0.00819   0.00232  -0.0973   0.7887   0.0718
  -5.250   0.1061   0.00804   0.00221  -0.0970   0.7788   0.0845
  -5.000   0.1335   0.00793   0.00210  -0.0967   0.7702   0.0943
  -4.750   0.1606   0.00784   0.00200  -0.0963   0.7594   0.1033
  -4.250   0.2146   0.00768   0.00184  -0.0957   0.7353   0.1247
  -3.750   0.2685   0.00754   0.00172  -0.0951   0.7125   0.1538
  -3.500   0.2953   0.00748   0.00168  -0.0947   0.7005   0.1713
  -3.000   0.3478   0.00741   0.00163  -0.0939   0.6731   0.2127
  -2.750   0.3742   0.00739   0.00163  -0.0935   0.6593   0.2325
  -2.500   0.4008   0.00738   0.00164  -0.0932   0.6465   0.2544
  -2.250   0.4273   0.00740   0.00166  -0.0929   0.6339   0.2749
  -2.000   0.4536   0.00743   0.00168  -0.0925   0.6213   0.2922
  -1.750   0.4800   0.00747   0.00171  -0.0922   0.6085   0.3069
  -1.500   0.5067   0.00750   0.00173  -0.0919   0.5962   0.3211
  -1.250   0.5331   0.00755   0.00177  -0.0916   0.5839   0.3364
  -1.000   0.5593   0.00761   0.00181  -0.0913   0.5711   0.3516
  -0.750   0.5853   0.00768   0.00186  -0.0909   0.5571   0.3669
  -0.500   0.6114   0.00773   0.00191  -0.0906   0.5427   0.3862
  -0.250   0.6370   0.00776   0.00197  -0.0902   0.5281   0.4144
   0.000   0.6620   0.00775   0.00204  -0.0898   0.5136   0.4586
   0.250   0.6739   0.00683   0.00217  -0.0866   0.5006   0.8533
   0.500   0.6996   0.00685   0.00235  -0.0859   0.4848   0.9361
   0.750   0.7393   0.00709   0.00253  -0.0886   0.4658   0.9703
   1.000   0.7741   0.00735   0.00268  -0.0903   0.4463   0.9830
   1.250   0.8142   0.00763   0.00285  -0.0932   0.4248   0.9895
   1.500   0.8530   0.00792   0.00301  -0.0959   0.4039   0.9944
   1.750   0.8927   0.00819   0.00317  -0.0988   0.3832   0.9974
   2.000   0.9300   0.00846   0.00333  -0.1013   0.3645   0.9998
   2.250   0.9519   0.00867   0.00347  -0.1003   0.3504   1.0000
   2.500   0.9710   0.00889   0.00361  -0.0987   0.3379   1.0000
   2.750   0.9903   0.00910   0.00376  -0.0971   0.3260   1.0000
   3.000   1.0099   0.00929   0.00390  -0.0956   0.3152   1.0000
   3.250   1.0288   0.00951   0.00406  -0.0940   0.3046   1.0000
   3.500   1.0484   0.00971   0.00422  -0.0926   0.2958   1.0000
   3.750   1.0679   0.00991   0.00438  -0.0911   0.2886   1.0000
   4.000   1.0883   0.01008   0.00454  -0.0898   0.2823   1.0000
   4.250   1.1068   0.01033   0.00473  -0.0882   0.2747   1.0000
   4.500   1.1277   0.01048   0.00489  -0.0870   0.2697   1.0000
   4.750   1.1478   0.01068   0.00507  -0.0857   0.2647   1.0000
   5.000   1.1671   0.01093   0.00529  -0.0843   0.2594   1.0000
   5.250   1.1884   0.01110   0.00547  -0.0833   0.2562   1.0000
   5.500   1.2086   0.01128   0.00566  -0.0821   0.2519   1.0000
   5.750   1.2271   0.01154   0.00589  -0.0806   0.2464   1.0000
   6.000   1.2465   0.01178   0.00613  -0.0793   0.2415   1.0000
   6.250   1.2678   0.01198   0.00634  -0.0785   0.2378   1.0000
   6.500   1.2880   0.01224   0.00659  -0.0774   0.2330   1.0000
   6.750   1.3066   0.01258   0.00691  -0.0762   0.2270   1.0000
   7.000   1.3288   0.01278   0.00714  -0.0755   0.2237   1.0000
   7.250   1.3496   0.01305   0.00742  -0.0747   0.2196   1.0000
   7.500   1.3690   0.01339   0.00776  -0.0737   0.2146   1.0000
   7.750   1.3892   0.01370   0.00808  -0.0729   0.2103   1.0000
   8.000   1.4101   0.01398   0.00838  -0.0722   0.2056   1.0000
   8.250   1.4283   0.01441   0.00878  -0.0711   0.1985   1.0000
   8.500   1.4482   0.01475   0.00914  -0.0703   0.1919   1.0000
   8.750   1.4653   0.01526   0.00960  -0.0692   0.1827   1.0000
   9.000   1.4823   0.01577   0.01008  -0.0681   0.1704   1.0000
   9.250   1.4925   0.01667   0.01082  -0.0660   0.1449   1.0000
   9.500   1.4940   0.01811   0.01204  -0.0629   0.1149   1.0000
   9.750   1.5018   0.01921   0.01307  -0.0607   0.1003   1.0000
  10.000   1.5117   0.02022   0.01404  -0.0589   0.0906   1.0000
  10.250   1.5218   0.02125   0.01503  -0.0573   0.0823   1.0000
  10.500   1.5327   0.02224   0.01601  -0.0558   0.0746   1.0000
  10.750   1.5405   0.02346   0.01719  -0.0541   0.0642   1.0000
  11.000   1.5394   0.02534   0.01893  -0.0515   0.0448   1.0000
  11.250   1.5328   0.02769   0.02117  -0.0486   0.0278   1.0000
  11.500   1.5350   0.02951   0.02298  -0.0468   0.0226   1.0000
  11.750   1.5399   0.03116   0.02467  -0.0454   0.0203   1.0000
  12.000   1.5451   0.03284   0.02640  -0.0441   0.0190   1.0000
  12.250   1.5479   0.03480   0.02841  -0.0429   0.0178   1.0000
  12.500   1.5546   0.03647   0.03015  -0.0420   0.0172   1.0000
  12.750   1.5594   0.03837   0.03212  -0.0412   0.0165   1.0000
  13.000   1.5623   0.04052   0.03433  -0.0404   0.0159   1.0000
  13.250   1.5631   0.04297   0.03685  -0.0396   0.0154   1.0000
  13.500   1.5605   0.04587   0.03984  -0.0389   0.0149   1.0000
  13.750   1.5619   0.04842   0.04247  -0.0386   0.0146   1.0000
  14.000   1.5630   0.05108   0.04521  -0.0383   0.0143   1.0000
  14.250   1.5626   0.05399   0.04821  -0.0382   0.0141   1.0000
  14.500   1.5606   0.05715   0.05146  -0.0382   0.0138   1.0000
  14.750   1.5571   0.06057   0.05496  -0.0383   0.0135   1.0000
  15.000   1.5519   0.06427   0.05876  -0.0386   0.0133   1.0000
  15.250   1.5449   0.06829   0.06287  -0.0390   0.0131   1.0000
  15.500   1.5361   0.07264   0.06732  -0.0395   0.0129   1.0000
  15.750   1.5245   0.07744   0.07223  -0.0402   0.0128   1.0000
  16.000   1.5111   0.08260   0.07750  -0.0411   0.0126   1.0000
  16.250   1.4955   0.08819   0.08320  -0.0423   0.0125   1.0000
  16.500   1.4781   0.09414   0.08928  -0.0436   0.0123   1.0000
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