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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 500,000
Max Cl/Cd: 70.54 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-500000.txt
Download as CSV file: xf-rhodesg36-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.0379   0.09291   0.09027  -0.1076   0.9717   0.0469
 -13.250  -0.0183   0.09050   0.08785  -0.1088   0.9682   0.0471
 -13.000  -0.0033   0.08854   0.08589  -0.1092   0.9625   0.0474
 -12.750   0.0104   0.08664   0.08398  -0.1095   0.9570   0.0477
 -12.500   0.0151   0.08484   0.08219  -0.1086   0.9490   0.0481
 -12.250   0.0172   0.08289   0.08023  -0.1077   0.9405   0.0485
 -12.000   0.0178   0.08063   0.07798  -0.1071   0.9324   0.0490
 -11.750  -0.0504   0.06881   0.06618  -0.1152   0.9142   0.0523
 -11.500  -0.0425   0.06728   0.06466  -0.1136   0.9035   0.0525
 -11.250  -0.2297   0.04114   0.03788  -0.1234   0.8604   0.0472
 -11.000  -0.2204   0.03972   0.03639  -0.1218   0.8484   0.0474
 -10.750  -0.2087   0.03855   0.03512  -0.1204   0.8366   0.0477
 -10.500  -0.2352   0.03195   0.02795  -0.1178   0.8245   0.0447
 -10.250  -0.2434   0.02747   0.02286  -0.1151   0.8140   0.0444
 -10.000  -0.2331   0.02514   0.02017  -0.1133   0.8054   0.0446
  -9.750  -0.2181   0.02339   0.01809  -0.1118   0.7968   0.0450
  -9.500  -0.2002   0.02198   0.01638  -0.1104   0.7886   0.0456
  -9.250  -0.1806   0.02082   0.01491  -0.1091   0.7796   0.0464
  -9.000  -0.1593   0.02003   0.01380  -0.1078   0.7717   0.0469
  -8.750  -0.1365   0.01867   0.01237  -0.1072   0.7635   0.0474
  -8.500  -0.1117   0.01806   0.01169  -0.1065   0.7559   0.0480
  -8.250  -0.0862   0.01756   0.01116  -0.1060   0.7483   0.0486
  -8.000  -0.0608   0.01705   0.01057  -0.1054   0.7397   0.0492
  -7.750  -0.0354   0.01653   0.00993  -0.1047   0.7314   0.0500
  -7.500  -0.0098   0.01601   0.00929  -0.1041   0.7223   0.0509
  -7.250   0.0159   0.01560   0.00872  -0.1034   0.7142   0.0517
  -7.000   0.0417   0.01499   0.00803  -0.1029   0.7055   0.0527
  -6.500   0.0938   0.01426   0.00725  -0.1019   0.6873   0.0548
  -6.250   0.1198   0.01396   0.00686  -0.1013   0.6787   0.0558
  -6.000   0.1461   0.01367   0.00651  -0.1008   0.6698   0.0570
  -5.750   0.1722   0.01352   0.00623  -0.1002   0.6602   0.0580
  -5.500   0.1973   0.01297   0.00569  -0.0996   0.6511   0.0593
  -5.250   0.2227   0.01276   0.00544  -0.0989   0.6413   0.0607
  -5.000   0.2486   0.01257   0.00524  -0.0984   0.6317   0.0624
  -4.500   0.2990   0.01217   0.00473  -0.0970   0.6111   0.0653
  -4.250   0.3228   0.01194   0.00448  -0.0961   0.5996   0.0671
  -4.000   0.3471   0.01180   0.00431  -0.0953   0.5851   0.0690
  -3.750   0.3709   0.01174   0.00418  -0.0943   0.5666   0.0710
  -3.500   0.3920   0.01160   0.00396  -0.0929   0.5371   0.0731
  -3.250   0.4050   0.01182   0.00387  -0.0901   0.4691   0.0751
  -3.000   0.4192   0.01214   0.00393  -0.0876   0.4263   0.0772
  -2.750   0.4383   0.01231   0.00397  -0.0859   0.4065   0.0795
  -2.500   0.4580   0.01233   0.00394  -0.0843   0.3939   0.0832
  -2.250   0.4789   0.01239   0.00394  -0.0830   0.3841   0.0874
  -2.000   0.4997   0.01242   0.00396  -0.0816   0.3765   0.0948
  -1.750   0.5213   0.01238   0.00409  -0.0804   0.3704   0.1371
  -1.500   0.5426   0.01251   0.00420  -0.0792   0.3647   0.1598
  -1.250   0.5619   0.01263   0.00431  -0.0775   0.3594   0.1734
  -1.000   0.5835   0.01264   0.00436  -0.0763   0.3559   0.1858
  -0.750   0.6039   0.01268   0.00443  -0.0749   0.3522   0.1992
  -0.500   0.6234   0.01275   0.00453  -0.0734   0.3485   0.2155
  -0.250   0.6420   0.01280   0.00467  -0.0718   0.3451   0.2546
   0.000   0.6577   0.01267   0.00491  -0.0698   0.3412   0.4010
   0.250   0.6674   0.01204   0.00515  -0.0664   0.3394   0.6818
   0.500   0.8175   0.01216   0.00588  -0.0916   0.3332   1.0000
   0.750   0.8300   0.01230   0.00598  -0.0888   0.3308   1.0000
   1.000   0.8424   0.01248   0.00610  -0.0859   0.3284   1.0000
   1.250   0.8563   0.01270   0.00627  -0.0833   0.3260   1.0000
   1.500   0.8725   0.01300   0.00649  -0.0813   0.3232   1.0000
   1.750   0.8907   0.01319   0.00666  -0.0796   0.3216   1.0000
   2.000   0.9095   0.01335   0.00682  -0.0780   0.3202   1.0000
   2.250   0.9286   0.01354   0.00700  -0.0766   0.3186   1.0000
   2.500   0.9480   0.01374   0.00718  -0.0752   0.3168   1.0000
   2.750   0.9676   0.01395   0.00738  -0.0739   0.3150   1.0000
   3.000   0.9876   0.01418   0.00759  -0.0727   0.3133   1.0000
   3.250   1.0077   0.01442   0.00781  -0.0715   0.3116   1.0000
   3.500   1.0281   0.01469   0.00805  -0.0704   0.3100   1.0000
   3.750   1.0489   0.01499   0.00831  -0.0695   0.3081   1.0000
   4.000   1.0719   0.01536   0.00863  -0.0690   0.3057   1.0000
   4.250   1.0946   0.01567   0.00892  -0.0684   0.3041   1.0000
   4.500   1.1147   0.01589   0.00917  -0.0674   0.3030   1.0000
   4.750   1.1353   0.01614   0.00944  -0.0665   0.3017   1.0000
   5.000   1.1543   0.01637   0.00969  -0.0654   0.2996   1.0000
   5.250   1.1736   0.01664   0.00997  -0.0643   0.2975   1.0000
   5.500   1.1929   0.01691   0.01024  -0.0633   0.2954   1.0000
   5.750   1.2132   0.01721   0.01054  -0.0625   0.2938   1.0000
   6.000   1.2332   0.01753   0.01085  -0.0617   0.2919   1.0000
   6.250   1.2547   0.01789   0.01118  -0.0612   0.2902   1.0000
   6.500   1.2794   0.01834   0.01158  -0.0612   0.2872   1.0000
   6.750   1.2969   0.01863   0.01193  -0.0601   0.2861   1.0000
   7.000   1.3156   0.01896   0.01231  -0.0591   0.2849   1.0000
   7.250   1.3344   0.01929   0.01269  -0.0583   0.2834   1.0000
   7.500   1.3534   0.01965   0.01308  -0.0575   0.2819   1.0000
   7.750   1.3722   0.02003   0.01349  -0.0568   0.2803   1.0000
   8.000   1.3907   0.02041   0.01390  -0.0560   0.2786   1.0000
   8.250   1.4094   0.02081   0.01432  -0.0553   0.2771   1.0000
   8.500   1.4280   0.02123   0.01476  -0.0546   0.2757   1.0000
   8.750   1.4463   0.02169   0.01521  -0.0539   0.2737   1.0000
   9.000   1.4681   0.02214   0.01565  -0.0538   0.2715   1.0000
   9.250   1.4866   0.02262   0.01617  -0.0532   0.2700   1.0000
   9.500   1.5011   0.02314   0.01678  -0.0521   0.2686   1.0000
   9.750   1.5161   0.02369   0.01740  -0.0512   0.2669   1.0000
  10.000   1.5313   0.02425   0.01803  -0.0504   0.2650   1.0000
  10.250   1.5471   0.02482   0.01865  -0.0497   0.2632   1.0000
  10.500   1.5625   0.02543   0.01930  -0.0490   0.2615   1.0000
  10.750   1.5771   0.02607   0.01998  -0.0482   0.2595   1.0000
  11.000   1.5914   0.02678   0.02069  -0.0475   0.2572   1.0000
  11.250   1.6078   0.02743   0.02135  -0.0470   0.2545   1.0000
  11.500   1.6197   0.02828   0.02231  -0.0462   0.2529   1.0000
  11.750   1.6325   0.02912   0.02325  -0.0456   0.2508   1.0000
  12.000   1.6456   0.02998   0.02418  -0.0450   0.2487   1.0000
  12.250   1.6577   0.03091   0.02519  -0.0444   0.2461   1.0000
  12.500   1.6687   0.03196   0.02626  -0.0438   0.2433   1.0000
  12.750   1.6790   0.03306   0.02735  -0.0432   0.2401   1.0000
  13.000   1.6893   0.03425   0.02867  -0.0427   0.2371   1.0000
  13.250   1.7007   0.03539   0.02991  -0.0423   0.2338   1.0000
  13.500   1.7101   0.03671   0.03130  -0.0420   0.2302   1.0000
  13.750   1.7168   0.03828   0.03288  -0.0415   0.2264   1.0000
  14.000   1.7261   0.03971   0.03441  -0.0412   0.2218   1.0000
  14.250   1.7327   0.04141   0.03618  -0.0409   0.2159   1.0000
  14.500   1.7352   0.04350   0.03830  -0.0405   0.2095   1.0000
  14.750   1.7352   0.04594   0.04077  -0.0402   0.1993   1.0000
  15.000   1.7308   0.04884   0.04368  -0.0397   0.1869   1.0000
  15.250   1.7138   0.05309   0.04788  -0.0391   0.1708   1.0000
  15.500   1.6890   0.05829   0.05305  -0.0384   0.1535   1.0000
  15.750   1.6558   0.06468   0.05943  -0.0380   0.1390   1.0000
  16.000   1.6223   0.07141   0.06619  -0.0380   0.1290   1.0000
  16.250   1.5886   0.07858   0.07343  -0.0385   0.1219   1.0000
  16.500   1.5555   0.08595   0.08090  -0.0394   0.1165   1.0000
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