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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 200,000
Max Cl/Cd: 52.83 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-200000-n5.txt
Download as CSV file: xf-rhodesg36-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.0309   0.09277   0.08860  -0.1004   0.9522   0.0428
 -12.750  -0.0272   0.08792   0.08373  -0.1043   0.9475   0.0430
 -12.500  -0.0307   0.08403   0.07984  -0.1056   0.9383   0.0431
 -12.250  -0.0316   0.08087   0.07669  -0.1061   0.9281   0.0430
 -12.000  -0.0383   0.07712   0.07296  -0.1068   0.9163   0.0430
 -11.500  -0.0604   0.06873   0.06460  -0.1087   0.8841   0.0429
 -11.250  -0.1970   0.04577   0.04127  -0.1234   0.8580   0.0426
 -11.000  -0.2626   0.03664   0.03127  -0.1213   0.8440   0.0431
 -10.750  -0.2656   0.03342   0.02757  -0.1192   0.8342   0.0436
 -10.500  -0.2485   0.03232   0.02635  -0.1180   0.8250   0.0440
 -10.250  -0.2312   0.03122   0.02511  -0.1168   0.8159   0.0444
 -10.000  -0.2147   0.02994   0.02363  -0.1155   0.8068   0.0449
  -9.750  -0.1987   0.02853   0.02196  -0.1142   0.7984   0.0454
  -9.500  -0.1820   0.02714   0.02029  -0.1128   0.7894   0.0460
  -9.250  -0.1639   0.02579   0.01863  -0.1116   0.7816   0.0466
  -9.000  -0.1454   0.02454   0.01709  -0.1102   0.7721   0.0474
  -8.750  -0.1250   0.02336   0.01552  -0.1090   0.7644   0.0481
  -8.500  -0.1030   0.02259   0.01464  -0.1080   0.7558   0.0488
  -8.250  -0.0790   0.02206   0.01405  -0.1073   0.7483   0.0495
  -8.000  -0.0553   0.02153   0.01344  -0.1065   0.7400   0.0504
  -7.750  -0.0314   0.02095   0.01273  -0.1057   0.7311   0.0514
  -7.500  -0.0073   0.02032   0.01194  -0.1048   0.7233   0.0523
  -7.250   0.0168   0.01971   0.01115  -0.1040   0.7145   0.0533
  -7.000   0.0417   0.01914   0.01044  -0.1032   0.7061   0.0541
  -6.750   0.0663   0.01867   0.00996  -0.1025   0.6963   0.0550
  -6.500   0.0915   0.01828   0.00951  -0.1018   0.6877   0.0561
  -6.250   0.1164   0.01791   0.00907  -0.1011   0.6782   0.0575
  -6.000   0.1417   0.01758   0.00859  -0.1004   0.6690   0.0591
  -5.750   0.1663   0.01719   0.00814  -0.0996   0.6581   0.0603
  -5.500   0.1907   0.01684   0.00777  -0.0988   0.6472   0.0615
  -5.250   0.2150   0.01656   0.00742  -0.0979   0.6356   0.0629
  -5.000   0.2395   0.01633   0.00712  -0.0971   0.6253   0.0647
  -4.750   0.2638   0.01612   0.00682  -0.0962   0.6144   0.0665
  -4.500   0.2873   0.01584   0.00656  -0.0953   0.6033   0.0682
  -4.250   0.3107   0.01566   0.00632  -0.0943   0.5909   0.0702
  -4.000   0.3339   0.01550   0.00612  -0.0933   0.5761   0.0722
  -3.750   0.3561   0.01532   0.00590  -0.0921   0.5580   0.0744
  -3.500   0.3769   0.01522   0.00571  -0.0907   0.5322   0.0770
  -3.250   0.3944   0.01526   0.00554  -0.0887   0.4875   0.0796
  -3.000   0.4079   0.01544   0.00545  -0.0860   0.4480   0.0819
  -2.500   0.4414   0.01568   0.00545  -0.0819   0.4106   0.0902
  -2.250   0.4600   0.01573   0.00551  -0.0802   0.4001   0.0987
  -2.000   0.4793   0.01580   0.00567  -0.0787   0.3912   0.1302
  -1.750   0.4988   0.01598   0.00577  -0.0771   0.3841   0.1518
  -1.500   0.5198   0.01604   0.00585  -0.0759   0.3779   0.1684
  -1.250   0.5396   0.01615   0.00593  -0.0744   0.3722   0.1803
  -1.000   0.5581   0.01626   0.00603  -0.0727   0.3673   0.1930
  -0.750   0.5776   0.01634   0.00614  -0.0713   0.3632   0.2111
  -0.500   0.5979   0.01637   0.00626  -0.0700   0.3590   0.2384
  -0.250   0.6169   0.01633   0.00641  -0.0685   0.3549   0.3031
   0.000   0.6269   0.01565   0.00667  -0.0655   0.3513   0.6005
   0.500   0.7633   0.01602   0.00764  -0.0819   0.3418   1.0000
   1.000   0.7974   0.01643   0.00794  -0.0781   0.3365   1.0000
   1.250   0.8151   0.01666   0.00811  -0.0764   0.3341   1.0000
   1.500   0.8333   0.01692   0.00829  -0.0748   0.3316   1.0000
   1.750   0.8521   0.01720   0.00850  -0.0733   0.3294   1.0000
   2.000   0.8718   0.01751   0.00872  -0.0720   0.3273   1.0000
   2.250   0.8929   0.01784   0.00896  -0.0711   0.3252   1.0000
   2.500   0.9133   0.01809   0.00920  -0.0699   0.3233   1.0000
   2.750   0.9339   0.01835   0.00945  -0.0689   0.3214   1.0000
   3.000   0.9541   0.01863   0.00972  -0.0678   0.3191   1.0000
   3.250   0.9747   0.01892   0.00999  -0.0668   0.3171   1.0000
   3.500   0.9952   0.01923   0.01028  -0.0659   0.3150   1.0000
   3.750   1.0161   0.01955   0.01058  -0.0650   0.3133   1.0000
   4.000   1.0372   0.01989   0.01088  -0.0642   0.3116   1.0000
   4.250   1.0589   0.02024   0.01120  -0.0635   0.3100   1.0000
   4.500   1.0813   0.02062   0.01153  -0.0630   0.3083   1.0000
   4.750   1.1054   0.02102   0.01188  -0.0628   0.3068   1.0000
   5.000   1.1273   0.02138   0.01226  -0.0622   0.3055   1.0000
   5.250   1.1479   0.02174   0.01266  -0.0615   0.3042   1.0000
   5.500   1.1687   0.02212   0.01308  -0.0608   0.3029   1.0000
   5.750   1.1892   0.02251   0.01351  -0.0601   0.3014   1.0000
   6.000   1.2092   0.02291   0.01395  -0.0593   0.2997   1.0000
   6.250   1.2289   0.02333   0.01439  -0.0586   0.2980   1.0000
   6.500   1.2478   0.02374   0.01484  -0.0577   0.2961   1.0000
   6.750   1.2655   0.02416   0.01527  -0.0567   0.2940   1.0000
   7.000   1.2837   0.02460   0.01570  -0.0558   0.2920   1.0000
   7.250   1.3039   0.02505   0.01613  -0.0553   0.2900   1.0000
   7.500   1.3255   0.02553   0.01658  -0.0549   0.2878   1.0000
   7.750   1.3395   0.02606   0.01721  -0.0536   0.2861   1.0000
   8.000   1.3540   0.02661   0.01785  -0.0524   0.2841   1.0000
   8.250   1.3698   0.02717   0.01849  -0.0513   0.2823   1.0000
   8.500   1.3844   0.02775   0.01915  -0.0502   0.2801   1.0000
   8.750   1.4005   0.02833   0.01979  -0.0494   0.2784   1.0000
   9.000   1.4159   0.02893   0.02044  -0.0485   0.2766   1.0000
   9.250   1.4313   0.02954   0.02109  -0.0476   0.2748   1.0000
   9.500   1.4470   0.03013   0.02168  -0.0468   0.2728   1.0000
   9.750   1.4640   0.03072   0.02226  -0.0462   0.2705   1.0000
  10.000   1.4710   0.03167   0.02336  -0.0446   0.2681   1.0000
  10.250   1.4815   0.03257   0.02439  -0.0435   0.2660   1.0000
  10.500   1.4926   0.03346   0.02539  -0.0425   0.2640   1.0000
  10.750   1.5034   0.03439   0.02640  -0.0415   0.2619   1.0000
  11.000   1.5145   0.03532   0.02741  -0.0406   0.2600   1.0000
  11.250   1.5255   0.03626   0.02842  -0.0398   0.2581   1.0000
  11.500   1.5379   0.03713   0.02933  -0.0391   0.2562   1.0000
  11.750   1.5523   0.03793   0.03014  -0.0386   0.2545   1.0000
  12.000   1.5550   0.03951   0.03190  -0.0375   0.2520   1.0000
  12.500   1.5636   0.04265   0.03533  -0.0357   0.2468   1.0000
  12.750   1.5690   0.04420   0.03699  -0.0350   0.2443   1.0000
  13.000   1.5747   0.04573   0.03857  -0.0344   0.2416   1.0000
  13.250   1.5832   0.04704   0.03990  -0.0340   0.2391   1.0000
  13.500   1.5799   0.04958   0.04265  -0.0333   0.2357   1.0000
  13.750   1.5775   0.05216   0.04540  -0.0328   0.2323   1.0000
  14.000   1.5768   0.05463   0.04799  -0.0326   0.2289   1.0000
  14.250   1.5782   0.05691   0.05034  -0.0324   0.2259   1.0000
  14.500   1.5752   0.05978   0.05332  -0.0323   0.2224   1.0000
  14.750   1.5618   0.06401   0.05776  -0.0324   0.2180   1.0000
  15.000   1.5503   0.06813   0.06202  -0.0327   0.2135   1.0000
  15.250   1.5423   0.07192   0.06589  -0.0331   0.2095   1.0000
  15.500   1.5005   0.08049   0.07474  -0.0343   0.2047   1.0000
  15.750   1.4277   0.09424   0.08872  -0.0373   0.1987   1.0000
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