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SM701 (sm701-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 100,000
Max Cl/Cd: 46.8 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sm701-il-100000-n5.txt
Download as CSV file: xf-sm701-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SM701                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4224   0.09787   0.09300  -0.0523   1.0000   0.0335
 -10.500  -0.4678   0.07831   0.07332  -0.0682   0.9946   0.0319
 -10.250  -0.5340   0.06322   0.05766  -0.0825   0.9834   0.0308
 -10.000  -0.5592   0.05778   0.05183  -0.0863   0.9720   0.0306
  -9.750  -0.5669   0.05406   0.04780  -0.0874   0.9611   0.0305
  -9.500  -0.5638   0.05079   0.04426  -0.0882   0.9523   0.0307
  -9.250  -0.5540   0.04773   0.04091  -0.0893   0.9453   0.0310
  -9.000  -0.5436   0.04577   0.03880  -0.0889   0.9376   0.0315
  -8.750  -0.5271   0.04379   0.03663  -0.0895   0.9317   0.0324
  -8.500  -0.5133   0.04152   0.03406  -0.0894   0.9252   0.0332
  -8.250  -0.4977   0.03934   0.03153  -0.0891   0.9185   0.0340
  -8.000  -0.4730   0.03693   0.02873  -0.0902   0.9151   0.0346
  -7.750  -0.4588   0.03528   0.02680  -0.0886   0.9077   0.0350
  -7.500  -0.4342   0.03354   0.02477  -0.0888   0.9035   0.0356
  -7.250  -0.4047   0.03195   0.02298  -0.0896   0.9008   0.0363
  -7.000  -0.3848   0.03087   0.02187  -0.0888   0.8949   0.0371
  -6.750  -0.3612   0.02991   0.02087  -0.0886   0.8899   0.0384
  -6.500  -0.3319   0.02894   0.01979  -0.0893   0.8868   0.0405
  -6.250  -0.3005   0.02791   0.01862  -0.0902   0.8847   0.0424
  -6.000  -0.2861   0.02723   0.01794  -0.0882   0.8775   0.0434
  -5.750  -0.2605   0.02638   0.01711  -0.0883   0.8734   0.0451
  -5.500  -0.2307   0.02552   0.01622  -0.0890   0.8707   0.0474
  -5.250  -0.1986   0.02473   0.01531  -0.0901   0.8688   0.0508
  -5.000  -0.1872   0.02435   0.01499  -0.0878   0.8607   0.0544
  -4.750  -0.1590   0.02369   0.01429  -0.0883   0.8572   0.0611
  -4.500  -0.1274   0.02286   0.01350  -0.0895   0.8547   0.0732
  -4.250  -0.0939   0.02193   0.01274  -0.0913   0.8528   0.1057
  -4.000  -0.0817   0.02148   0.01253  -0.0894   0.8448   0.1524
  -3.750  -0.0526   0.02009   0.01184  -0.0913   0.8414   0.2921
  -3.500  -0.0236   0.01957   0.01238  -0.0916   0.8388   0.5308
  -3.250   0.0123   0.01983   0.01257  -0.0925   0.8368   0.5858
  -3.000   0.0257   0.02025   0.01295  -0.0896   0.8286   0.6044
  -2.750   0.0551   0.02047   0.01307  -0.0893   0.8248   0.6228
  -2.500   0.0869   0.02073   0.01328  -0.0891   0.8221   0.6426
  -2.000   0.1281   0.02145   0.01395  -0.0850   0.8105   0.6754
  -1.750   0.1618   0.02135   0.01374  -0.0858   0.8071   0.6821
  -1.500   0.2031   0.02103   0.01323  -0.0885   0.8045   0.6885
  -1.250   0.2195   0.02117   0.01335  -0.0865   0.7963   0.6919
  -1.000   0.2517   0.02100   0.01310  -0.0871   0.7916   0.6957
  -0.750   0.2921   0.02068   0.01266  -0.0893   0.7883   0.7000
  -0.500   0.3145   0.02069   0.01259  -0.0888   0.7800   0.7049
  -0.250   0.3479   0.02047   0.01231  -0.0896   0.7745   0.7083
   0.000   0.3891   0.02011   0.01187  -0.0917   0.7707   0.7115
   0.250   0.4055   0.02023   0.01198  -0.0898   0.7606   0.7155
   0.500   0.4452   0.01991   0.01157  -0.0919   0.7557   0.7200
   0.750   0.4674   0.01994   0.01158  -0.0910   0.7467   0.7242
   1.000   0.5006   0.01972   0.01133  -0.0917   0.7402   0.7275
   1.250   0.5255   0.01969   0.01129  -0.0912   0.7316   0.7314
   1.500   0.5581   0.01950   0.01106  -0.0919   0.7238   0.7360
   1.750   0.5830   0.01947   0.01102  -0.0915   0.7143   0.7407
   2.000   0.6144   0.01928   0.01081  -0.0918   0.7061   0.7445
   2.250   0.6345   0.01931   0.01087  -0.0904   0.6949   0.7491
   2.500   0.6656   0.01916   0.01068  -0.0909   0.6853   0.7539
   2.750   0.6909   0.01908   0.01061  -0.0903   0.6737   0.7585
   3.000   0.7106   0.01910   0.01068  -0.0887   0.6607   0.7632
   3.250   0.7341   0.01908   0.01066  -0.0879   0.6471   0.7690
   3.500   0.7578   0.01905   0.01064  -0.0871   0.6324   0.7746
   3.750   0.7787   0.01904   0.01065  -0.0856   0.6165   0.7796
   4.000   0.8004   0.01905   0.01065  -0.0844   0.5988   0.7857
   4.250   0.8229   0.01904   0.01061  -0.0834   0.5795   0.7917
   4.500   0.8455   0.01904   0.01056  -0.0822   0.5592   0.7979
   4.750   0.8674   0.01915   0.01059  -0.0811   0.5361   0.8055
   5.000   0.8877   0.01928   0.01063  -0.0796   0.5139   0.8120
   5.250   0.9084   0.01951   0.01075  -0.0783   0.4916   0.8200
   5.500   0.9263   0.01981   0.01098  -0.0766   0.4700   0.8275
   5.750   0.9445   0.02018   0.01125  -0.0751   0.4497   0.8366
   6.000   0.9607   0.02055   0.01156  -0.0731   0.4314   0.8459
   6.250   0.9770   0.02097   0.01193  -0.0713   0.4139   0.8570
   6.500   0.9922   0.02138   0.01231  -0.0693   0.3979   0.8694
   6.750   1.0061   0.02178   0.01270  -0.0670   0.3832   0.8835
   7.000   1.0197   0.02217   0.01309  -0.0648   0.3695   0.9013
   7.250   1.0331   0.02253   0.01348  -0.0625   0.3570   0.9281
   7.500   1.0517   0.02291   0.01384  -0.0616   0.3443   1.0000
   7.750   1.0736   0.02359   0.01444  -0.0615   0.3319   1.0000
   8.000   1.0948   0.02425   0.01510  -0.0613   0.3200   1.0000
   8.250   1.1151   0.02496   0.01577  -0.0609   0.3093   1.0000
   8.500   1.1343   0.02569   0.01645  -0.0603   0.2994   1.0000
   8.750   1.1537   0.02641   0.01720  -0.0598   0.2896   1.0000
   9.250   1.1899   0.02796   0.01876  -0.0584   0.2722   1.0000
   9.500   1.2075   0.02879   0.01954  -0.0576   0.2648   1.0000
   9.750   1.2246   0.02961   0.02044  -0.0568   0.2567   1.0000
  10.000   1.2411   0.03049   0.02128  -0.0559   0.2500   1.0000
  10.250   1.2574   0.03138   0.02228  -0.0551   0.2425   1.0000
  10.500   1.2730   0.03231   0.02320  -0.0542   0.2363   1.0000
  10.750   1.2886   0.03328   0.02425  -0.0534   0.2299   1.0000
  11.000   1.3030   0.03429   0.02533  -0.0524   0.2236   1.0000
  11.250   1.3180   0.03532   0.02635  -0.0516   0.2182   1.0000
  11.500   1.3316   0.03642   0.02760  -0.0506   0.2122   1.0000
  11.750   1.3445   0.03756   0.02878  -0.0497   0.2068   1.0000
  12.000   1.3579   0.03872   0.03000  -0.0488   0.2018   1.0000
  12.250   1.3694   0.04001   0.03144  -0.0479   0.1964   1.0000
  12.500   1.3807   0.04129   0.03277  -0.0469   0.1916   1.0000
  12.750   1.3929   0.04259   0.03412  -0.0461   0.1872   1.0000
  13.000   1.4017   0.04413   0.03584  -0.0452   0.1821   1.0000
  13.250   1.4107   0.04563   0.03743  -0.0443   0.1776   1.0000
  13.500   1.4218   0.04704   0.03884  -0.0436   0.1736   1.0000
  13.750   1.4272   0.04894   0.04098  -0.0427   0.1691   1.0000
  14.000   1.4333   0.05078   0.04295  -0.0419   0.1647   1.0000
  14.250   1.4408   0.05249   0.04469  -0.0412   0.1609   1.0000
  14.500   1.4455   0.05457   0.04692  -0.0406   0.1570   1.0000
  14.750   1.4475   0.05694   0.04950  -0.0400   0.1529   1.0000
  15.000   1.4505   0.05919   0.05187  -0.0396   0.1490   1.0000
  15.250   1.4572   0.06111   0.05379  -0.0392   0.1456   1.0000
  15.500   1.4538   0.06427   0.05721  -0.0390   0.1419   1.0000
  15.750   1.4514   0.06737   0.06051  -0.0389   0.1381   1.0000
  16.000   1.4516   0.07021   0.06345  -0.0390   0.1347   1.0000
  16.250   1.4561   0.07253   0.06577  -0.0391   0.1315   1.0000
  16.500   1.4454   0.07703   0.07058  -0.0398   0.1282   1.0000
  16.750   1.4372   0.08132   0.07508  -0.0407   0.1248   1.0000
  17.000   1.4328   0.08513   0.07901  -0.0416   0.1216   1.0000
  17.250   1.4360   0.08785   0.08174  -0.0422   0.1186   1.0000
  17.500   1.4189   0.09393   0.08810  -0.0443   0.1158   1.0000
  17.750   1.4010   0.10038   0.09480  -0.0469   0.1130   1.0000
  18.000   1.3881   0.10616   0.10074  -0.0495   0.1100   1.0000
  18.250   1.3872   0.10986   0.10449  -0.0511   0.1071   1.0000
  18.500   1.3758   0.11558   0.11033  -0.0539   0.1045   1.0000
  18.750   1.3316   0.12784   0.12292  -0.0607   0.1022   1.0000
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