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TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il)
Reynolds number: 100,000
Max Cl/Cd: 43.91 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-tsagi-r-3a-il-100000-n5.txt
Download as CSV file: xf-tsagi-r-3a-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TsAGI R-3a (12%)                                
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.4546   0.08548   0.08084  -0.0081   1.0045   0.0337
  -8.250  -0.4506   0.08183   0.07725  -0.0101   1.0045   0.0334
  -8.000  -0.4503   0.07732   0.07279  -0.0138   1.0045   0.0330
  -7.750  -0.4496   0.07178   0.06725  -0.0188   1.0045   0.0325
  -7.500  -0.4488   0.06562   0.06104  -0.0236   1.0045   0.0319
  -7.250  -0.4470   0.05929   0.05457  -0.0274   1.0045   0.0316
  -7.000  -0.4428   0.05328   0.04834  -0.0300   1.0045   0.0317
  -6.750  -0.4358   0.04776   0.04250  -0.0315   1.0045   0.0320
  -6.500  -0.4262   0.04279   0.03716  -0.0320   1.0045   0.0323
  -6.250  -0.4137   0.03852   0.03244  -0.0318   1.0045   0.0325
  -6.000  -0.3909   0.03447   0.02788  -0.0329   0.9817   0.0326
  -5.750  -0.3580   0.03080   0.02357  -0.0350   0.9318   0.0329
  -5.500  -0.3245   0.02799   0.02012  -0.0363   0.8736   0.0334
  -5.250  -0.2970   0.02619   0.01782  -0.0358   0.8094   0.0340
  -5.000  -0.2736   0.02510   0.01638  -0.0344   0.7503   0.0348
  -4.750  -0.2499   0.02414   0.01506  -0.0332   0.7019   0.0360
  -4.500  -0.2250   0.02319   0.01367  -0.0322   0.6645   0.0381
  -4.250  -0.1997   0.02239   0.01265  -0.0315   0.6363   0.0400
  -4.000  -0.1736   0.02160   0.01167  -0.0308   0.6140   0.0422
  -3.750  -0.1474   0.02077   0.01061  -0.0301   0.5955   0.0444
  -3.500  -0.1217   0.02011   0.00987  -0.0295   0.5780   0.0472
  -3.250  -0.0957   0.01952   0.00914  -0.0289   0.5615   0.0519
  -3.000  -0.0696   0.01902   0.00853  -0.0284   0.5466   0.0587
  -2.750  -0.0432   0.01854   0.00801  -0.0279   0.5331   0.0673
  -2.500  -0.0167   0.01821   0.00764  -0.0275   0.5213   0.0819
  -2.250   0.0096   0.01788   0.00733  -0.0271   0.5109   0.1033
  -2.000   0.0363   0.01743   0.00696  -0.0267   0.5017   0.1317
  -1.750   0.0627   0.01705   0.00663  -0.0262   0.4937   0.1737
  -1.500   0.0888   0.01655   0.00640  -0.0259   0.4857   0.2455
  -1.250   0.1132   0.01575   0.00626  -0.0254   0.4782   0.4189
  -1.000   0.1312   0.01478   0.00636  -0.0225   0.4720   0.7151
  -0.750   0.1761   0.01456   0.00647  -0.0237   0.4628   0.9235
  -0.500   0.2247   0.01469   0.00632  -0.0273   0.4540   0.9757
  -0.250   0.2657   0.01478   0.00620  -0.0298   0.4448   0.9955
   0.000   0.2905   0.01493   0.00611  -0.0292   0.4381   0.9955
   0.250   0.3156   0.01505   0.00611  -0.0287   0.4300   0.9955
   0.500   0.3407   0.01523   0.00609  -0.0280   0.4231   0.9955
   0.750   0.3661   0.01539   0.00614  -0.0275   0.4156   0.9955
   1.000   0.3915   0.01557   0.00618  -0.0270   0.4081   0.9955
   1.250   0.4170   0.01578   0.00624  -0.0264   0.4010   0.9955
   1.500   0.4428   0.01596   0.00635  -0.0260   0.3925   0.9955
   1.750   0.4684   0.01618   0.00641  -0.0255   0.3854   0.9955
   2.000   0.4944   0.01636   0.00657  -0.0250   0.3762   0.9955
   2.250   0.5202   0.01657   0.00663  -0.0246   0.3692   0.9955
   2.500   0.5464   0.01678   0.00684  -0.0242   0.3602   0.9955
   2.750   0.5723   0.01700   0.00695  -0.0238   0.3537   0.9955
   3.000   0.5985   0.01726   0.00720  -0.0234   0.3460   0.9955
   3.250   0.6246   0.01750   0.00736  -0.0230   0.3396   0.9955
   3.500   0.6506   0.01777   0.00758  -0.0227   0.3334   0.9955
   3.750   0.6767   0.01805   0.00784  -0.0223   0.3266   0.9955
   4.000   0.7026   0.01830   0.00799  -0.0219   0.3214   0.9955
   4.250   0.7286   0.01864   0.00835  -0.0216   0.3153   0.9955
   4.500   0.7544   0.01896   0.00865  -0.0213   0.3102   0.9955
   4.750   0.7801   0.01925   0.00885  -0.0209   0.3059   0.9955
   5.000   0.8058   0.01962   0.00926  -0.0205   0.2999   0.9955
   5.250   0.8312   0.01993   0.00955  -0.0202   0.2943   0.9955
   5.500   0.8565   0.02024   0.00976  -0.0198   0.2898   0.9955
   5.750   0.8816   0.02067   0.01026  -0.0194   0.2841   0.9955
   6.000   0.9066   0.02105   0.01063  -0.0190   0.2793   0.9955
   6.250   0.9316   0.02145   0.01095  -0.0186   0.2755   0.9955
   6.500   0.9561   0.02196   0.01154  -0.0183   0.2708   0.9955
   6.750   0.9805   0.02245   0.01207  -0.0179   0.2662   0.9955
   7.000   1.0049   0.02291   0.01253  -0.0174   0.2621   0.9955
   7.250   1.0293   0.02344   0.01300  -0.0170   0.2584   0.9955
   7.500   1.0525   0.02405   0.01378  -0.0166   0.2538   0.9955
   7.750   1.0759   0.02462   0.01443  -0.0161   0.2495   0.9955
   8.000   1.0996   0.02515   0.01495  -0.0157   0.2456   0.9955
   8.250   1.1228   0.02578   0.01560  -0.0152   0.2418   0.9955
   8.500   1.1443   0.02648   0.01650  -0.0146   0.2371   0.9955
   8.750   1.1664   0.02711   0.01721  -0.0141   0.2328   0.9955
   9.000   1.1893   0.02769   0.01779  -0.0136   0.2293   0.9955
   9.250   1.2105   0.02846   0.01866  -0.0130   0.2257   0.9955
   9.500   1.2296   0.02930   0.01972  -0.0123   0.2212   0.9955
   9.750   1.2500   0.03001   0.02051  -0.0116   0.2171   0.9955
  10.000   1.2717   0.03061   0.02110  -0.0110   0.2136   0.9955
  10.250   1.2891   0.03157   0.02224  -0.0102   0.2097   0.9955
  10.500   1.3048   0.03260   0.02349  -0.0092   0.2055   0.9955
  10.750   1.3225   0.03347   0.02447  -0.0084   0.2020   0.9955
  11.000   1.3419   0.03419   0.02521  -0.0076   0.1990   0.9955
  11.250   1.3560   0.03533   0.02650  -0.0066   0.1959   0.9955
  11.500   1.3640   0.03680   0.02824  -0.0052   0.1920   0.9955
  11.750   1.3748   0.03798   0.02959  -0.0040   0.1886   0.9955
  12.000   1.3883   0.03891   0.03058  -0.0029   0.1859   0.9955
  12.250   1.4050   0.03969   0.03134  -0.0020   0.1836   0.9955
  12.500   1.3944   0.04210   0.03408   0.0003   0.1809   0.9955
  12.750   1.3845   0.04479   0.03701   0.0017   0.1783   0.9955
  13.000   1.3763   0.04767   0.04008   0.0021   0.1759   0.9955
  13.250   1.3734   0.05028   0.04282   0.0020   0.1736   0.9955
  13.500   1.3809   0.05195   0.04453   0.0021   0.1715   0.9955
  13.750   1.3737   0.05540   0.04811   0.0013   0.1695   0.9955
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