Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

S3010-103-84 (s3010-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: S3010-103-84 (s3010-il)
Reynolds number: 50,000
Max Cl/Cd: 28.48 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s3010-il-50000.txt
Download as CSV file: xf-s3010-il-50000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S3010-103-84                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3930   0.10840   0.10170  -0.0086   1.0000   0.2349
  -8.500  -0.3769   0.10398   0.09730  -0.0081   1.0000   0.2440
  -8.250  -0.4009   0.10410   0.09759  -0.0110   1.0000   0.2519
  -8.000  -0.3747   0.09885   0.09233  -0.0094   1.0000   0.2654
  -7.750  -0.3622   0.09492   0.08844  -0.0091   1.0000   0.2746
  -7.500  -0.3702   0.09297   0.08663  -0.0100   1.0000   0.2849
  -7.250  -0.3719   0.09088   0.08463  -0.0100   1.0000   0.2979
  -7.000  -0.3503   0.08632   0.08008  -0.0090   1.0000   0.3083
  -6.750  -0.3484   0.08351   0.07737  -0.0086   1.0000   0.3201
  -6.500  -0.3543   0.08139   0.07540  -0.0079   1.0000   0.3329
  -6.250  -0.3613   0.07940   0.07356  -0.0069   1.0000   0.3472
  -6.000  -0.3657   0.07730   0.07159  -0.0058   1.0000   0.3622
  -5.750  -0.3690   0.07514   0.06957  -0.0039   1.0000   0.3776
  -5.500  -0.4019   0.05686   0.05055  -0.0382   1.0000   0.1588
  -5.250  -0.3937   0.05162   0.04511  -0.0389   1.0000   0.1409
  -5.000  -0.3833   0.04610   0.03897  -0.0408   1.0000   0.1275
  -4.750  -0.3702   0.04260   0.03523  -0.0406   1.0000   0.1235
  -4.500  -0.3537   0.03889   0.03098  -0.0408   1.0000   0.1201
  -4.250  -0.3356   0.03618   0.02784  -0.0406   1.0000   0.1208
  -4.000  -0.3160   0.03388   0.02514  -0.0402   1.0000   0.1238
  -3.750  -0.2942   0.03166   0.02243  -0.0398   1.0000   0.1266
  -3.500  -0.2709   0.02972   0.01994  -0.0392   1.0000   0.1300
  -3.250  -0.2501   0.02824   0.01847  -0.0386   1.0000   0.1405
  -3.000  -0.2279   0.02690   0.01700  -0.0380   1.0000   0.1549
  -2.750  -0.2059   0.02563   0.01577  -0.0372   1.0000   0.1809
  -2.500  -0.1850   0.02449   0.01482  -0.0364   1.0000   0.2333
  -2.250  -0.1637   0.02316   0.01408  -0.0356   1.0000   0.3360
  -2.000  -0.1451   0.02183   0.01374  -0.0339   1.0000   0.5007
  -1.750  -0.1387   0.02086   0.01387  -0.0285   1.0000   0.6969
  -1.500  -0.1146   0.02005   0.01337  -0.0272   1.0000   1.0000
  -1.250  -0.0826   0.02063   0.01333  -0.0302   0.9961   1.0000
  -1.000  -0.0267   0.02164   0.01375  -0.0370   0.9807   1.0000
  -0.750   0.0245   0.02256   0.01423  -0.0426   0.9646   1.0000
  -0.500   0.0737   0.02343   0.01475  -0.0477   0.9485   1.0000
  -0.250   0.1212   0.02426   0.01528  -0.0523   0.9323   1.0000
   0.000   0.1673   0.02502   0.01581  -0.0564   0.9161   1.0000
   0.250   0.2118   0.02572   0.01632  -0.0600   0.8999   1.0000
   0.500   0.2557   0.02637   0.01681  -0.0633   0.8837   1.0000
   0.750   0.2989   0.02696   0.01726  -0.0663   0.8677   1.0000
   1.000   0.3420   0.02748   0.01768  -0.0691   0.8517   1.0000
   1.250   0.3796   0.02799   0.01811  -0.0708   0.8356   1.0000
   1.500   0.4122   0.02851   0.01857  -0.0716   0.8191   1.0000
   1.750   0.4436   0.02902   0.01903  -0.0720   0.8025   1.0000
   2.000   0.4744   0.02951   0.01948  -0.0722   0.7862   1.0000
   2.250   0.5041   0.02998   0.01993  -0.0721   0.7700   1.0000
   2.500   0.5330   0.03044   0.02037  -0.0719   0.7538   1.0000
   2.750   0.5612   0.03088   0.02082  -0.0714   0.7376   1.0000
   3.000   0.5888   0.03130   0.02123  -0.0707   0.7215   1.0000
   3.250   0.6161   0.03169   0.02164  -0.0699   0.7053   1.0000
   3.500   0.6430   0.03206   0.02204  -0.0689   0.6892   1.0000
   3.750   0.6698   0.03238   0.02239  -0.0678   0.6729   1.0000
   4.000   0.6964   0.03270   0.02273  -0.0667   0.6567   1.0000
   4.250   0.7228   0.03298   0.02305  -0.0654   0.6404   1.0000
   4.500   0.7494   0.03321   0.02334  -0.0641   0.6241   1.0000
   4.750   0.7761   0.03342   0.02358  -0.0627   0.6078   1.0000
   5.000   0.8032   0.03354   0.02374  -0.0612   0.5913   1.0000
   5.250   0.8307   0.03362   0.02389  -0.0597   0.5749   1.0000
   5.500   0.8587   0.03361   0.02390  -0.0582   0.5583   1.0000
   5.750   0.8814   0.03416   0.02451  -0.0567   0.5401   1.0000
   6.000   0.9021   0.03492   0.02536  -0.0553   0.5211   1.0000
   6.250   0.9267   0.03528   0.02581  -0.0538   0.5029   1.0000
   6.500   0.9534   0.03543   0.02599  -0.0523   0.4850   1.0000
   6.750   0.9814   0.03545   0.02601  -0.0508   0.4671   1.0000
   7.000   1.0045   0.03607   0.02670  -0.0494   0.4486   1.0000
   7.250   1.0231   0.03713   0.02790  -0.0480   0.4291   1.0000
   7.500   1.0463   0.03775   0.02857  -0.0466   0.4104   1.0000
   7.750   1.0728   0.03803   0.02886  -0.0452   0.3919   1.0000
   8.000   1.0980   0.03856   0.02937  -0.0438   0.3738   1.0000
   8.250   1.1128   0.04011   0.03110  -0.0424   0.3554   1.0000
   8.500   1.1305   0.04143   0.03255  -0.0410   0.3378   1.0000
   8.750   1.1499   0.04257   0.03379  -0.0396   0.3205   1.0000
   9.000   1.1699   0.04374   0.03502  -0.0383   0.3038   1.0000
   9.250   1.1895   0.04498   0.03631  -0.0369   0.2877   1.0000
   9.500   1.2053   0.04667   0.03811  -0.0355   0.2728   1.0000
   9.750   1.2135   0.04912   0.04078  -0.0340   0.2598   1.0000
  10.000   1.2193   0.05176   0.04365  -0.0324   0.2479   1.0000
  10.250   1.2307   0.05407   0.04607  -0.0311   0.2366   1.0000
  10.500   1.2485   0.05576   0.04780  -0.0299   0.2242   1.0000
  10.750   1.2170   0.06154   0.05400  -0.0279   0.2211   1.0000
  11.000   1.1716   0.06844   0.06112  -0.0267   0.2215   1.0000
  11.250   1.1141   0.07812   0.07082  -0.0287   0.2245   1.0000
<< Back to S3010-103-84 (s3010-il)

Polar data table (+)

Polar graphs


<< Back to S3010-103-84 (s3010-il)