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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 100,000
Max Cl/Cd: 41.84 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-100000-n5.txt
Download as CSV file: xf-rhodesg36-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 36                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.1479   0.12895   0.12363  -0.0590   0.9798   0.0788
 -13.750  -0.1456   0.12534   0.12002  -0.0642   0.9750   0.0801
 -13.500  -0.1383   0.12128   0.11596  -0.0695   0.9716   0.0805
 -13.250  -0.1072   0.11773   0.11240  -0.0703   0.9699   0.0819
 -13.000  -0.0908   0.11484   0.10951  -0.0722   0.9650   0.0844
 -12.750  -0.0876   0.11110   0.10577  -0.0784   0.9609   0.0880
 -11.750  -0.0519   0.09196   0.08653  -0.0935   0.9401   0.0656
 -11.500  -0.0329   0.08859   0.08315  -0.0964   0.9360   0.0645
 -11.250  -0.0304   0.08517   0.07975  -0.0981   0.9257   0.0643
 -11.000  -0.0307   0.08182   0.07642  -0.0995   0.9144   0.0642
 -10.750  -0.0334   0.07839   0.07300  -0.1007   0.9017   0.0639
 -10.500  -0.0389   0.07473   0.06936  -0.1020   0.8890   0.0634
 -10.000  -0.1368   0.05600   0.05023  -0.1122   0.8591   0.0596
  -9.750  -0.1493   0.05134   0.04530  -0.1119   0.8493   0.0594
  -9.500  -0.1574   0.04641   0.03993  -0.1115   0.8412   0.0595
  -9.250  -0.1641   0.04238   0.03539  -0.1096   0.8316   0.0598
  -9.000  -0.1387   0.04111   0.03412  -0.1096   0.8249   0.0606
  -8.750  -0.1206   0.03922   0.03205  -0.1089   0.8173   0.0615
  -8.500  -0.1069   0.03714   0.02968  -0.1076   0.8084   0.0626
  -8.250  -0.0865   0.03459   0.02668  -0.1073   0.8032   0.0636
  -8.000  -0.0756   0.03292   0.02466  -0.1051   0.7934   0.0642
  -7.750  -0.0540   0.03102   0.02232  -0.1043   0.7870   0.0651
  -7.500  -0.0331   0.02952   0.02035  -0.1032   0.7803   0.0661
  -7.250  -0.0126   0.02861   0.01943  -0.1020   0.7717   0.0672
  -7.000   0.0160   0.02760   0.01832  -0.1020   0.7660   0.0689
  -6.750   0.0349   0.02684   0.01740  -0.1004   0.7566   0.0705
  -6.500   0.0607   0.02586   0.01614  -0.0997   0.7489   0.0720
  -6.250   0.0849   0.02505   0.01511  -0.0987   0.7412   0.0732
  -6.000   0.1078   0.02430   0.01438  -0.0977   0.7319   0.0746
  -5.750   0.1336   0.02361   0.01363  -0.0970   0.7232   0.0769
  -5.500   0.1562   0.02305   0.01296  -0.0958   0.7130   0.0791
  -5.250   0.1818   0.02241   0.01225  -0.0951   0.7045   0.0812
  -5.000   0.2044   0.02188   0.01176  -0.0939   0.6947   0.0830
  -4.750   0.2298   0.02137   0.01121  -0.0932   0.6858   0.0858
  -4.500   0.2531   0.02095   0.01074  -0.0921   0.6757   0.0888
  -4.250   0.2772   0.02052   0.01034  -0.0912   0.6657   0.0920
  -4.000   0.3019   0.02015   0.00991  -0.0902   0.6546   0.0954
  -3.750   0.3242   0.01987   0.00966  -0.0890   0.6422   0.0996
  -3.500   0.3496   0.01959   0.00932  -0.0882   0.6297   0.1057
  -3.250   0.3721   0.01941   0.00917  -0.0869   0.6152   0.1129
  -3.000   0.3934   0.01929   0.00904  -0.0855   0.5992   0.1234
  -2.750   0.4147   0.01919   0.00891  -0.0840   0.5821   0.1409
  -2.500   0.4347   0.01910   0.00877  -0.0824   0.5626   0.1622
  -2.250   0.4536   0.01900   0.00865  -0.0806   0.5394   0.1834
  -2.000   0.4723   0.01891   0.00854  -0.0789   0.5123   0.2082
  -1.750   0.4910   0.01888   0.00844  -0.0771   0.4849   0.2398
  -1.500   0.5095   0.01889   0.00839  -0.0755   0.4633   0.2870
  -1.250   0.5276   0.01874   0.00846  -0.0740   0.4471   0.3965
  -1.000   0.5426   0.01804   0.00876  -0.0712   0.4352   0.7188
  -0.750   0.6538   0.01856   0.00926  -0.0873   0.4173   1.0000
  -0.500   0.6710   0.01887   0.00937  -0.0855   0.4103   1.0000
  -0.250   0.6895   0.01921   0.00948  -0.0839   0.4046   1.0000
   0.000   0.7087   0.01949   0.00966  -0.0824   0.3992   1.0000
   0.250   0.7284   0.01980   0.00983  -0.0810   0.3940   1.0000
   0.500   0.7491   0.02014   0.01001  -0.0798   0.3894   1.0000
   1.000   0.7929   0.02083   0.01042  -0.0780   0.3810   1.0000
   1.250   0.8139   0.02116   0.01068  -0.0769   0.3768   1.0000
   1.500   0.8357   0.02151   0.01093  -0.0760   0.3729   1.0000
   1.750   0.8589   0.02188   0.01119  -0.0754   0.3695   1.0000
   2.000   0.8847   0.02228   0.01145  -0.0753   0.3666   1.0000
   2.250   0.9098   0.02269   0.01176  -0.0750   0.3638   1.0000
   2.500   0.9314   0.02307   0.01214  -0.0742   0.3611   1.0000
   2.750   0.9537   0.02347   0.01252  -0.0735   0.3583   1.0000
   3.000   0.9764   0.02389   0.01291  -0.0730   0.3557   1.0000
   3.250   0.9997   0.02433   0.01331  -0.0725   0.3531   1.0000
   3.500   1.0233   0.02477   0.01370  -0.0721   0.3506   1.0000
   3.750   1.0482   0.02523   0.01409  -0.0720   0.3482   1.0000
   4.000   1.0756   0.02574   0.01451  -0.0723   0.3459   1.0000
   4.250   1.0987   0.02626   0.01502  -0.0719   0.3438   1.0000
   4.500   1.1176   0.02677   0.01559  -0.0709   0.3416   1.0000
   4.750   1.1375   0.02730   0.01619  -0.0700   0.3396   1.0000
   5.000   1.1573   0.02786   0.01679  -0.0691   0.3376   1.0000
   5.250   1.1773   0.02843   0.01739  -0.0683   0.3357   1.0000
   5.500   1.1977   0.02902   0.01801  -0.0676   0.3339   1.0000
   5.750   1.2186   0.02962   0.01863  -0.0671   0.3321   1.0000
   6.000   1.2401   0.03022   0.01925  -0.0666   0.3304   1.0000
   6.250   1.2629   0.03083   0.01986  -0.0664   0.3287   1.0000
   6.500   1.2882   0.03146   0.02048  -0.0666   0.3271   1.0000
   6.750   1.3169   0.03217   0.02115  -0.0674   0.3254   1.0000
   7.000   1.3239   0.03294   0.02208  -0.0648   0.3238   1.0000
   7.250   1.3324   0.03380   0.02308  -0.0625   0.3223   1.0000
   7.500   1.3413   0.03471   0.02413  -0.0604   0.3207   1.0000
   7.750   1.3502   0.03569   0.02523  -0.0584   0.3191   1.0000
   8.000   1.3588   0.03672   0.02639  -0.0565   0.3176   1.0000
   8.250   1.3673   0.03779   0.02757  -0.0546   0.3160   1.0000
   8.500   1.3760   0.03886   0.02875  -0.0529   0.3143   1.0000
   8.750   1.3874   0.03981   0.02978  -0.0515   0.3123   1.0000
   9.000   1.4055   0.04047   0.03046  -0.0510   0.3101   1.0000
   9.250   1.4332   0.04087   0.03082  -0.0515   0.3078   1.0000
   9.500   1.4505   0.04174   0.03173  -0.0510   0.3057   1.0000
   9.750   1.4295   0.04392   0.03418  -0.0464   0.3037   1.0000
  10.000   1.4061   0.04660   0.03710  -0.0422   0.3014   1.0000
  10.250   1.3814   0.04981   0.04054  -0.0387   0.2990   1.0000
  10.500   1.3539   0.05367   0.04461  -0.0358   0.2966   1.0000
  10.750   1.3381   0.05696   0.04803  -0.0340   0.2939   1.0000
  11.000   1.3676   0.05652   0.04757  -0.0342   0.2913   1.0000
  11.250   1.4267   0.05402   0.04494  -0.0360   0.2890   1.0000
  11.750   0.9853   0.11651   0.10840  -0.0406   0.2565   1.0000
  12.000   0.9585   0.12443   0.11640  -0.0430   0.2486   1.0000
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