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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 200,000
Max Cl/Cd: 54.02 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-200000.txt
Download as CSV file: xf-rhodesg36-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750   0.0446   0.09621   0.09263  -0.0927   0.9592   0.0751
 -12.500   0.0529   0.09266   0.08907  -0.0954   0.9535   0.0778
 -12.250   0.0405   0.08721   0.08362  -0.1016   0.9490   0.0801
 -12.000   0.0720   0.08401   0.08041  -0.1024   0.9466   0.0812
 -11.750   0.0828   0.08164   0.07804  -0.1020   0.9374   0.0826
 -11.500   0.0886   0.07881   0.07522  -0.1026   0.9292   0.0847
 -11.250   0.0486   0.07341   0.06984  -0.1083   0.9172   0.0885
 -11.000   0.0708   0.07124   0.06767  -0.1058   0.9100   0.0892
 -10.750   0.0838   0.06926   0.06570  -0.1041   0.9009   0.0903
 -10.500   0.0924   0.06681   0.06325  -0.1035   0.8938   0.0922
 -10.250   0.0495   0.07247   0.06875  -0.1111   0.9109   0.0920
 -10.000   0.0461   0.06986   0.06616  -0.1115   0.8983   0.0947
  -9.750  -0.0119   0.06340   0.05964  -0.1174   0.8793   0.0983
  -9.500   0.0078   0.06229   0.05858  -0.1145   0.8713   0.0993
  -9.250   0.0229   0.06056   0.05683  -0.1132   0.8648   0.1011
  -9.000  -0.0119   0.05487   0.05085  -0.1174   0.8508   0.1085
  -8.750   0.0138   0.05346   0.04949  -0.1158   0.8463   0.1098
  -8.500  -0.0028   0.05030   0.04590  -0.1167   0.8336   0.1192
  -8.250   0.0224   0.04813   0.04383  -0.1158   0.8279   0.1204
  -8.000  -0.0294   0.03124   0.02510  -0.1133   0.8169   0.0801
  -7.750  -0.0059   0.02907   0.02274  -0.1126   0.8114   0.0784
  -7.500   0.0098   0.02721   0.02061  -0.1109   0.8018   0.0781
  -7.250   0.0311   0.02542   0.01845  -0.1098   0.7951   0.0782
  -7.000   0.0522   0.02402   0.01674  -0.1085   0.7879   0.0784
  -6.750   0.0747   0.02282   0.01527  -0.1073   0.7797   0.0786
  -6.500   0.1012   0.02179   0.01390  -0.1066   0.7735   0.0792
  -6.250   0.1230   0.02083   0.01281  -0.1054   0.7646   0.0801
  -6.000   0.1495   0.01981   0.01177  -0.1049   0.7569   0.0820
  -5.750   0.1748   0.01919   0.01109  -0.1042   0.7490   0.0840
  -5.500   0.2002   0.01856   0.01037  -0.1034   0.7406   0.0857
  -5.250   0.2282   0.01794   0.00960  -0.1029   0.7337   0.0873
  -5.000   0.2516   0.01732   0.00897  -0.1019   0.7242   0.0891
  -4.750   0.2786   0.01671   0.00838  -0.1014   0.7166   0.0921
  -4.500   0.3022   0.01633   0.00802  -0.1003   0.7067   0.0951
  -4.250   0.3288   0.01588   0.00747  -0.0996   0.6978   0.0978
  -4.000   0.3512   0.01547   0.00716  -0.0984   0.6865   0.1014
  -3.750   0.3768   0.01517   0.00680  -0.0976   0.6753   0.1062
  -3.500   0.4004   0.01489   0.00654  -0.0965   0.6618   0.1116
  -3.250   0.4237   0.01471   0.00633  -0.0953   0.6465   0.1187
  -3.000   0.4468   0.01458   0.00618  -0.0940   0.6291   0.1293
  -2.750   0.4687   0.01446   0.00604  -0.0926   0.6090   0.1468
  -2.500   0.4885   0.01429   0.00585  -0.0908   0.5847   0.1763
  -2.250   0.5049   0.01414   0.00573  -0.0886   0.5520   0.2091
  -2.000   0.5193   0.01413   0.00565  -0.0860   0.5112   0.2407
  -1.750   0.5321   0.01422   0.00565  -0.0832   0.4778   0.2823
  -1.500   0.5442   0.01415   0.00575  -0.0805   0.4576   0.3838
  -1.250   0.6027   0.01346   0.00644  -0.0860   0.4385   0.9284
  -1.000   0.6995   0.01424   0.00685  -0.1000   0.4215   1.0000
  -0.750   0.7174   0.01457   0.00699  -0.0983   0.4148   1.0000
  -0.500   0.7360   0.01482   0.00714  -0.0967   0.4088   1.0000
  -0.250   0.7556   0.01511   0.00729  -0.0952   0.4035   1.0000
   0.000   0.7784   0.01552   0.00749  -0.0944   0.3985   1.0000
   0.250   0.7990   0.01577   0.00769  -0.0932   0.3945   1.0000
   0.500   0.8197   0.01603   0.00789  -0.0920   0.3905   1.0000
   0.750   0.8413   0.01632   0.00810  -0.0909   0.3866   1.0000
   1.000   0.8642   0.01666   0.00833  -0.0902   0.3831   1.0000
   1.250   0.8918   0.01714   0.00864  -0.0903   0.3793   1.0000
   1.500   0.9128   0.01742   0.00891  -0.0892   0.3763   1.0000
   1.750   0.9337   0.01770   0.00919  -0.0881   0.3733   1.0000
   2.000   0.9559   0.01801   0.00947  -0.0872   0.3703   1.0000
   2.250   0.9792   0.01835   0.00976  -0.0866   0.3675   1.0000
   2.500   1.0035   0.01871   0.01007  -0.0862   0.3649   1.0000
   2.750   1.0298   0.01915   0.01042  -0.0862   0.3625   1.0000
   3.000   1.0616   0.01980   0.01095  -0.0873   0.3598   1.0000
   3.250   1.0822   0.02013   0.01133  -0.0863   0.3581   1.0000
   3.500   1.1034   0.02049   0.01173  -0.0854   0.3562   1.0000
   3.750   1.1254   0.02088   0.01215  -0.0846   0.3541   1.0000
   4.000   1.1476   0.02128   0.01257  -0.0840   0.3519   1.0000
   4.250   1.1704   0.02169   0.01298  -0.0834   0.3496   1.0000
   4.500   1.1943   0.02211   0.01340  -0.0831   0.3475   1.0000
   4.750   1.2196   0.02258   0.01385  -0.0831   0.3456   1.0000
   5.000   1.2467   0.02312   0.01435  -0.0834   0.3438   1.0000
   5.250   1.2757   0.02384   0.01503  -0.0842   0.3421   1.0000
   5.500   1.3011   0.02460   0.01583  -0.0844   0.3405   1.0000
   5.750   1.3203   0.02508   0.01640  -0.0834   0.3392   1.0000
   6.000   1.3393   0.02559   0.01701  -0.0823   0.3377   1.0000
   6.250   1.3580   0.02612   0.01762  -0.0813   0.3359   1.0000
   6.500   1.3764   0.02665   0.01823  -0.0802   0.3339   1.0000
   6.750   1.3947   0.02716   0.01880  -0.0791   0.3317   1.0000
   7.000   1.4141   0.02756   0.01922  -0.0783   0.3290   1.0000
   7.250   1.4375   0.02799   0.01964  -0.0781   0.3266   1.0000
   7.500   1.4671   0.02861   0.02018  -0.0791   0.3239   1.0000
   7.750   1.4872   0.02946   0.02108  -0.0786   0.3217   1.0000
   8.000   1.4963   0.02994   0.02171  -0.0761   0.3197   1.0000
   8.250   1.5074   0.03052   0.02242  -0.0740   0.3177   1.0000
   8.500   1.5200   0.03114   0.02313  -0.0722   0.3156   1.0000
   8.750   1.5314   0.03172   0.02380  -0.0702   0.3135   1.0000
   9.000   1.5442   0.03225   0.02439  -0.0684   0.3114   1.0000
   9.250   1.5620   0.03271   0.02489  -0.0675   0.3093   1.0000
   9.500   1.5893   0.03313   0.02527  -0.0682   0.3070   1.0000
   9.750   1.6224   0.03406   0.02617  -0.0702   0.3043   1.0000
  10.000   1.6154   0.03475   0.02704  -0.0654   0.3028   1.0000
  10.250   1.6117   0.03562   0.02808  -0.0615   0.3009   1.0000
  10.500   1.6122   0.03656   0.02916  -0.0584   0.2988   1.0000
  10.750   1.6150   0.03749   0.03021  -0.0559   0.2967   1.0000
  11.000   1.6216   0.03823   0.03103  -0.0538   0.2943   1.0000
  11.250   1.6349   0.03873   0.03157  -0.0527   0.2921   1.0000
  11.500   1.6643   0.03873   0.03153  -0.0536   0.2895   1.0000
  11.750   1.6928   0.03923   0.03200  -0.0545   0.2868   1.0000
  12.000   1.6717   0.04090   0.03390  -0.0495   0.2849   1.0000
  12.250   1.6554   0.04279   0.03601  -0.0457   0.2827   1.0000
  12.500   1.6424   0.04473   0.03811  -0.0426   0.2802   1.0000
  12.750   1.6393   0.04626   0.03976  -0.0407   0.2778   1.0000
  13.000   1.6514   0.04680   0.04034  -0.0399   0.2752   1.0000
  13.250   1.6985   0.04525   0.03866  -0.0419   0.2721   1.0000
  13.500   1.7021   0.04663   0.04014  -0.0406   0.2697   1.0000
  13.750   1.6581   0.05099   0.04479  -0.0364   0.2673   1.0000
  14.000   1.6098   0.05651   0.05059  -0.0332   0.2644   1.0000
  14.250   1.5804   0.06111   0.05536  -0.0318   0.2613   1.0000
  14.500   1.6076   0.06039   0.05464  -0.0320   0.2586   1.0000
  14.750   1.6876   0.05494   0.04897  -0.0340   0.2554   1.0000
  15.000   1.6269   0.06252   0.05686  -0.0317   0.2527   1.0000
  15.500   1.4071   0.09495   0.08985  -0.0341   0.2402   1.0000
  15.750   1.5930   0.07260   0.06727  -0.0315   0.2409   1.0000
  16.000   1.1284   0.14845   0.14350  -0.0517   0.1890   1.0000
  16.250   1.1525   0.14735   0.14246  -0.0516   0.1877   1.0000
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