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HOBIESMO1.DAT (hobiesm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HOBIESMO1.DAT (hobiesm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 118.23 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hobiesm-il-1000000-n5.txt
Download as CSV file: xf-hobiesm-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HOBIESMO1.DAT                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.6864   0.06941   0.06763  -0.0467   1.0000   0.0040
 -11.750  -0.7629   0.05557   0.05374  -0.0565   1.0000   0.0036
 -11.500  -0.8273   0.02872   0.02626  -0.0824   1.0000   0.0032
 -11.250  -0.8052   0.02422   0.02137  -0.0873   0.9978   0.0034
 -11.000  -0.7773   0.02190   0.01882  -0.0901   0.9950   0.0036
 -10.750  -0.7501   0.02024   0.01696  -0.0918   0.9920   0.0038
 -10.500  -0.7222   0.01889   0.01545  -0.0933   0.9883   0.0040
 -10.250  -0.6925   0.01777   0.01418  -0.0947   0.9849   0.0042
 -10.000  -0.6627   0.01679   0.01306  -0.0960   0.9815   0.0045
  -9.750  -0.6342   0.01591   0.01205  -0.0969   0.9760   0.0047
  -9.500  -0.6023   0.01510   0.01110  -0.0984   0.9718   0.0050
  -9.250  -0.5705   0.01443   0.01030  -0.0997   0.9663   0.0052
  -9.000  -0.5390   0.01345   0.00917  -0.1011   0.9586   0.0059
  -8.750  -0.5066   0.01291   0.00857  -0.1025   0.9494   0.0065
  -8.500  -0.4750   0.01245   0.00803  -0.1035   0.9377   0.0071
  -8.250  -0.4461   0.01203   0.00749  -0.1039   0.9231   0.0077
  -8.000  -0.4189   0.01168   0.00701  -0.1039   0.9085   0.0081
  -7.750  -0.3926   0.01131   0.00652  -0.1036   0.8948   0.0086
  -7.500  -0.3666   0.01092   0.00601  -0.1034   0.8823   0.0095
  -7.250  -0.3401   0.01072   0.00575  -0.1031   0.8710   0.0104
  -7.000  -0.3134   0.01052   0.00548  -0.1029   0.8606   0.0113
  -6.750  -0.2866   0.01029   0.00516  -0.1027   0.8511   0.0121
  -6.500  -0.2599   0.01008   0.00487  -0.1025   0.8420   0.0127
  -6.250  -0.2329   0.00989   0.00460  -0.1023   0.8330   0.0130
  -6.000  -0.2061   0.00957   0.00416  -0.1021   0.8247   0.0137
  -5.750  -0.1795   0.00917   0.00364  -0.1019   0.8162   0.0151
  -5.500  -0.1524   0.00890   0.00330  -0.1017   0.8081   0.0160
  -5.250  -0.1253   0.00869   0.00302  -0.1016   0.8001   0.0168
  -5.000  -0.0979   0.00849   0.00276  -0.1014   0.7918   0.0176
  -4.750  -0.0706   0.00831   0.00250  -0.1012   0.7838   0.0181
  -4.500  -0.0432   0.00815   0.00225  -0.1011   0.7752   0.0186
  -4.250  -0.0157   0.00801   0.00204  -0.1009   0.7670   0.0192
  -4.000   0.0117   0.00789   0.00185  -0.1008   0.7586   0.0199
  -3.750   0.0393   0.00773   0.00166  -0.1006   0.7495   0.0242
  -3.500   0.0666   0.00754   0.00147  -0.1005   0.7407   0.0354
  -3.000   0.1211   0.00720   0.00121  -0.1002   0.7215   0.0760
  -2.750   0.1486   0.00712   0.00112  -0.1001   0.7114   0.0870
  -2.500   0.1760   0.00706   0.00104  -0.0999   0.7010   0.0962
  -2.250   0.2034   0.00703   0.00097  -0.0998   0.6896   0.1039
  -2.000   0.2309   0.00697   0.00091  -0.0997   0.6779   0.1151
  -1.750   0.2583   0.00693   0.00086  -0.0995   0.6660   0.1273
  -1.500   0.2856   0.00690   0.00082  -0.0994   0.6534   0.1390
  -1.250   0.3129   0.00686   0.00079  -0.0992   0.6407   0.1590
  -1.000   0.3400   0.00682   0.00077  -0.0991   0.6272   0.1805
  -0.750   0.3673   0.00681   0.00076  -0.0989   0.6139   0.2007
  -0.500   0.3944   0.00680   0.00076  -0.0987   0.6003   0.2196
  -0.250   0.4216   0.00681   0.00077  -0.0986   0.5866   0.2379
   0.000   0.4488   0.00684   0.00079  -0.0984   0.5730   0.2563
   0.250   0.4759   0.00686   0.00081  -0.0982   0.5599   0.2745
   0.500   0.5030   0.00689   0.00085  -0.0981   0.5470   0.2955
   0.750   0.5301   0.00691   0.00090  -0.0979   0.5342   0.3199
   1.000   0.5572   0.00695   0.00095  -0.0978   0.5216   0.3414
   1.250   0.5843   0.00699   0.00101  -0.0976   0.5093   0.3627
   1.500   0.6113   0.00701   0.00108  -0.0974   0.4973   0.3928
   1.750   0.6380   0.00700   0.00116  -0.0973   0.4854   0.4401
   2.000   0.6644   0.00693   0.00126  -0.0971   0.4733   0.5163
   2.250   0.6901   0.00679   0.00138  -0.0967   0.4613   0.6319
   2.750   0.7469   0.00636   0.00163  -0.0970   0.4239   1.0000
   3.000   0.7731   0.00656   0.00175  -0.0967   0.4032   1.0000
   3.250   0.7992   0.00676   0.00188  -0.0964   0.3839   1.0000
   3.500   0.8242   0.00705   0.00205  -0.0959   0.3533   1.0000
   3.750   0.8479   0.00750   0.00227  -0.0952   0.3054   1.0000
   4.000   0.8697   0.00814   0.00259  -0.0943   0.2401   1.0000
   4.250   0.8915   0.00880   0.00295  -0.0934   0.1791   1.0000
   4.500   0.9058   0.01030   0.00378  -0.0914   0.0392   1.0000
   4.750   0.9302   0.01068   0.00409  -0.0908   0.0227   1.0000
   5.000   0.9552   0.01098   0.00436  -0.0903   0.0178   1.0000
   5.250   0.9804   0.01125   0.00464  -0.0899   0.0145   1.0000
   5.500   1.0051   0.01156   0.00493  -0.0894   0.0115   1.0000
   5.750   1.0296   0.01190   0.00529  -0.0888   0.0095   1.0000
   6.000   1.0542   0.01220   0.00562  -0.0883   0.0084   1.0000
   6.250   1.0783   0.01255   0.00597  -0.0877   0.0075   1.0000
   6.500   1.1017   0.01296   0.00640  -0.0870   0.0066   1.0000
   6.750   1.1242   0.01348   0.00697  -0.0861   0.0059   1.0000
   7.000   1.1477   0.01383   0.00736  -0.0854   0.0056   1.0000
   7.250   1.1710   0.01421   0.00776  -0.0847   0.0051   1.0000
   7.500   1.1933   0.01467   0.00828  -0.0839   0.0048   1.0000
   7.750   1.2153   0.01513   0.00878  -0.0830   0.0044   1.0000
   8.000   1.2368   0.01562   0.00931  -0.0820   0.0042   1.0000
   8.250   1.2571   0.01620   0.00992  -0.0809   0.0039   1.0000
   8.500   1.2745   0.01702   0.01082  -0.0793   0.0036   1.0000
   8.750   1.2901   0.01793   0.01183  -0.0775   0.0034   1.0000
   9.000   1.3089   0.01851   0.01247  -0.0761   0.0034   1.0000
   9.250   1.3262   0.01918   0.01323  -0.0746   0.0033   1.0000
   9.500   1.3413   0.01997   0.01410  -0.0727   0.0032   1.0000
   9.750   1.3546   0.02077   0.01499  -0.0706   0.0030   1.0000
  10.000   1.3652   0.02156   0.01586  -0.0680   0.0029   1.0000
  10.250   1.3735   0.02248   0.01687  -0.0651   0.0028   1.0000
  10.500   1.3828   0.02338   0.01784  -0.0625   0.0027   1.0000
  10.750   1.3902   0.02444   0.01899  -0.0599   0.0026   1.0000
  11.000   1.4001   0.02535   0.01997  -0.0578   0.0025   1.0000
  11.250   1.4105   0.02627   0.02095  -0.0559   0.0024   1.0000
  11.500   1.4181   0.02744   0.02221  -0.0539   0.0024   1.0000
  11.750   1.4252   0.02872   0.02357  -0.0520   0.0023   1.0000
  12.000   1.4304   0.03023   0.02520  -0.0501   0.0022   1.0000
  12.250   1.4389   0.03149   0.02653  -0.0487   0.0022   1.0000
  12.500   1.4425   0.03328   0.02842  -0.0471   0.0021   1.0000
  12.750   1.4449   0.03529   0.03054  -0.0457   0.0021   1.0000
  13.000   1.4443   0.03769   0.03306  -0.0443   0.0020   1.0000
  13.250   1.4419   0.04041   0.03592  -0.0432   0.0020   1.0000
  13.500   1.4378   0.04347   0.03914  -0.0423   0.0020   1.0000
  13.750   1.4339   0.04666   0.04247  -0.0417   0.0019   1.0000
  14.000   1.4206   0.05122   0.04724  -0.0414   0.0019   1.0000
  14.250   1.4084   0.05589   0.05212  -0.0417   0.0019   1.0000
  14.500   1.4026   0.05987   0.05624  -0.0423   0.0019   1.0000
  14.750   1.3936   0.06456   0.06109  -0.0434   0.0019   1.0000
  15.000   1.3849   0.06945   0.06614  -0.0448   0.0019   1.0000
  15.250   1.3717   0.07533   0.07219  -0.0469   0.0019   1.0000
  15.500   1.3633   0.08066   0.07766  -0.0491   0.0018   1.0000
  15.750   1.3484   0.08744   0.08461  -0.0521   0.0018   1.0000
  16.000   1.3323   0.09477   0.09210  -0.0556   0.0018   1.0000
  16.250   1.3158   0.10256   0.10006  -0.0596   0.0018   1.0000
  16.500   1.2990   0.11076   0.10841  -0.0641   0.0018   1.0000
  16.750   1.2780   0.12027   0.11809  -0.0694   0.0018   1.0000
  17.000   1.2558   0.13059   0.12857  -0.0755   0.0018   1.0000
  17.250   1.2344   0.14123   0.13936  -0.0818   0.0019   1.0000
  17.500   1.2029   0.15537   0.15368  -0.0904   0.0019   1.0000
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