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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.49 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-1000000-n5.txt
Download as CSV file: xf-rhodesg36-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8331   0.03608   0.03256  -0.1449   0.9422   0.0268
 -18.000  -0.8619   0.03128   0.02759  -0.1472   0.9382   0.0268
 -17.750  -0.8769   0.02880   0.02497  -0.1463   0.9348   0.0268
 -17.500  -0.8816   0.02717   0.02324  -0.1446   0.9310   0.0269
 -17.250  -0.8848   0.02591   0.02188  -0.1419   0.9268   0.0269
 -17.000  -0.8859   0.02484   0.02071  -0.1388   0.9230   0.0270
 -16.750  -0.8821   0.02391   0.01969  -0.1360   0.9183   0.0270
 -16.500  -0.8801   0.02306   0.01876  -0.1326   0.9138   0.0272
 -16.250  -0.8706   0.02217   0.01781  -0.1303   0.9095   0.0274
 -16.000  -0.8562   0.02139   0.01698  -0.1287   0.9031   0.0276
 -15.750  -0.8404   0.02068   0.01621  -0.1270   0.8963   0.0277
 -15.500  -0.8235   0.02005   0.01552  -0.1253   0.8856   0.0279
 -15.250  -0.8080   0.01943   0.01481  -0.1231   0.8684   0.0280
 -15.000  -0.7919   0.01890   0.01413  -0.1210   0.8471   0.0282
 -14.750  -0.7728   0.01843   0.01353  -0.1194   0.8318   0.0284
 -14.500  -0.7522   0.01798   0.01297  -0.1180   0.8208   0.0285
 -14.250  -0.7302   0.01754   0.01244  -0.1169   0.8133   0.0287
 -14.000  -0.7078   0.01712   0.01194  -0.1159   0.8062   0.0289
 -13.750  -0.6848   0.01671   0.01145  -0.1149   0.8005   0.0291
 -13.500  -0.6612   0.01629   0.01098  -0.1140   0.7949   0.0293
 -13.250  -0.6375   0.01591   0.01052  -0.1131   0.7875   0.0295
 -13.000  -0.6134   0.01555   0.01007  -0.1122   0.7802   0.0297
 -12.750  -0.5889   0.01518   0.00964  -0.1114   0.7728   0.0300
 -12.500  -0.5643   0.01485   0.00922  -0.1106   0.7656   0.0302
 -12.250  -0.5390   0.01451   0.00882  -0.1099   0.7585   0.0304
 -12.000  -0.5137   0.01421   0.00844  -0.1091   0.7488   0.0306
 -11.750  -0.4883   0.01390   0.00806  -0.1084   0.7403   0.0307
 -11.500  -0.4634   0.01355   0.00764  -0.1077   0.7294   0.0311
 -11.250  -0.4377   0.01326   0.00730  -0.1070   0.7190   0.0314
 -11.000  -0.4120   0.01302   0.00700  -0.1063   0.7061   0.0317
 -10.750  -0.3860   0.01282   0.00672  -0.1057   0.6905   0.0320
 -10.500  -0.3600   0.01264   0.00646  -0.1051   0.6742   0.0324
 -10.250  -0.3338   0.01246   0.00621  -0.1044   0.6614   0.0327
 -10.000  -0.3076   0.01229   0.00596  -0.1038   0.6511   0.0331
  -9.750  -0.2808   0.01211   0.00573  -0.1033   0.6435   0.0336
  -9.500  -0.2542   0.01195   0.00551  -0.1028   0.6353   0.0340
  -9.250  -0.2275   0.01180   0.00530  -0.1023   0.6280   0.0344
  -9.000  -0.2007   0.01162   0.00507  -0.1018   0.6206   0.0347
  -8.750  -0.1745   0.01144   0.00485  -0.1012   0.6131   0.0353
  -8.500  -0.1474   0.01128   0.00467  -0.1008   0.6071   0.0358
  -8.250  -0.1203   0.01115   0.00451  -0.1003   0.6004   0.0363
  -8.000  -0.0935   0.01103   0.00435  -0.0999   0.5938   0.0368
  -7.750  -0.0662   0.01091   0.00420  -0.0995   0.5880   0.0374
  -7.500  -0.0390   0.01079   0.00404  -0.0991   0.5800   0.0380
  -7.250  -0.0123   0.01071   0.00390  -0.0986   0.5711   0.0385
  -7.000   0.0148   0.01059   0.00375  -0.0982   0.5617   0.0391
  -6.750   0.0411   0.01051   0.00363  -0.0976   0.5492   0.0399
  -6.500   0.0671   0.01049   0.00354  -0.0971   0.5281   0.0407
  -6.250   0.0853   0.01094   0.00359  -0.0952   0.4346   0.0414
  -6.000   0.1086   0.01110   0.00359  -0.0942   0.4020   0.0423
  -5.750   0.1335   0.01115   0.00354  -0.0935   0.3848   0.0430
  -5.500   0.1593   0.01113   0.00347  -0.0929   0.3737   0.0437
  -5.250   0.1846   0.01112   0.00342  -0.0922   0.3637   0.0446
  -5.000   0.2107   0.01110   0.00338  -0.0917   0.3564   0.0456
  -4.750   0.2363   0.01110   0.00334  -0.0911   0.3487   0.0466
  -4.500   0.2622   0.01110   0.00330  -0.0905   0.3429   0.0475
  -4.250   0.2883   0.01109   0.00327  -0.0900   0.3380   0.0484
  -4.000   0.3137   0.01106   0.00323  -0.0894   0.3330   0.0497
  -3.750   0.3390   0.01107   0.00322  -0.0888   0.3280   0.0509
  -3.500   0.3646   0.01107   0.00320  -0.0882   0.3240   0.0520
  -3.250   0.3904   0.01107   0.00318  -0.0877   0.3209   0.0532
  -3.000   0.4156   0.01106   0.00317  -0.0871   0.3173   0.0544
  -2.750   0.4405   0.01107   0.00316  -0.0864   0.3136   0.0560
  -2.500   0.4652   0.01110   0.00317  -0.0857   0.3102   0.0575
  -2.000   0.5146   0.01113   0.00319  -0.0844   0.3051   0.0605
  -1.750   0.5393   0.01113   0.00321  -0.0837   0.3034   0.0627
  -1.500   0.5637   0.01114   0.00323  -0.0830   0.3014   0.0648
  -1.250   0.5877   0.01117   0.00325  -0.0822   0.2994   0.0668
  -1.000   0.6110   0.01119   0.00328  -0.0813   0.2973   0.0700
  -0.750   0.6329   0.01122   0.00331  -0.0801   0.2952   0.0736
  -0.500   0.6532   0.01125   0.00334  -0.0786   0.2930   0.0801
  -0.250   0.6724   0.01120   0.00343  -0.0770   0.2908   0.1288
   0.000   0.6928   0.01129   0.00353  -0.0756   0.2884   0.1389
   0.250   0.7150   0.01135   0.00362  -0.0746   0.2874   0.1465
   0.500   0.7376   0.01144   0.00372  -0.0737   0.2863   0.1507
   0.750   0.7600   0.01152   0.00382  -0.0727   0.2848   0.1554
   1.000   0.7824   0.01162   0.00394  -0.0718   0.2832   0.1596
   1.250   0.8047   0.01173   0.00406  -0.0708   0.2817   0.1633
   1.500   0.8267   0.01185   0.00419  -0.0699   0.2802   0.1681
   1.750   0.8484   0.01197   0.00433  -0.0689   0.2786   0.1740
   2.000   0.8701   0.01211   0.00448  -0.0679   0.2771   0.1808
   2.250   0.9600   0.01078   0.00514  -0.0820   0.2741   0.9835
   2.500   0.9890   0.01105   0.00538  -0.0827   0.2719   1.0000
   2.750   1.0076   0.01122   0.00553  -0.0811   0.2703   1.0000
   3.000   1.0279   0.01137   0.00568  -0.0799   0.2693   1.0000
   3.250   1.0484   0.01152   0.00583  -0.0788   0.2675   1.0000
   3.500   1.0685   0.01170   0.00600  -0.0776   0.2659   1.0000
   3.750   1.0887   0.01190   0.00618  -0.0765   0.2637   1.0000
   4.000   1.1086   0.01212   0.00637  -0.0754   0.2610   1.0000
   4.250   1.1282   0.01236   0.00659  -0.0742   0.2586   1.0000
   4.500   1.1472   0.01263   0.00684  -0.0730   0.2561   1.0000
   4.750   1.1667   0.01289   0.00710  -0.0719   0.2543   1.0000
   5.000   1.1879   0.01310   0.00732  -0.0711   0.2534   1.0000
   5.250   1.2090   0.01333   0.00756  -0.0704   0.2524   1.0000
   5.500   1.2295   0.01358   0.00782  -0.0695   0.2513   1.0000
   5.750   1.2500   0.01384   0.00809  -0.0687   0.2497   1.0000
   6.000   1.2704   0.01412   0.00837  -0.0680   0.2480   1.0000
   6.250   1.2904   0.01442   0.00867  -0.0672   0.2457   1.0000
   6.500   1.3097   0.01476   0.00901  -0.0663   0.2440   1.0000
   6.750   1.3290   0.01511   0.00936  -0.0655   0.2420   1.0000
   7.000   1.3477   0.01550   0.00975  -0.0646   0.2398   1.0000
   7.250   1.3668   0.01588   0.01014  -0.0639   0.2385   1.0000
   7.500   1.3871   0.01622   0.01050  -0.0633   0.2372   1.0000
   7.750   1.4071   0.01658   0.01088  -0.0627   0.2348   1.0000
   8.000   1.4260   0.01700   0.01131  -0.0621   0.2315   1.0000
   8.250   1.4443   0.01746   0.01177  -0.0614   0.2289   1.0000
   8.500   1.4615   0.01799   0.01230  -0.0606   0.2257   1.0000
   8.750   1.4793   0.01850   0.01283  -0.0599   0.2233   1.0000
   9.000   1.4980   0.01898   0.01333  -0.0594   0.2203   1.0000
   9.250   1.5153   0.01954   0.01390  -0.0588   0.2165   1.0000
   9.500   1.5303   0.02026   0.01460  -0.0579   0.2110   1.0000
   9.750   1.5464   0.02092   0.01527  -0.0573   0.2065   1.0000
  10.000   1.5602   0.02174   0.01606  -0.0564   0.1985   1.0000
  10.250   1.5721   0.02270   0.01699  -0.0554   0.1895   1.0000
  10.750   1.5593   0.02719   0.02114  -0.0503   0.1354   1.0000
  11.000   1.5535   0.02958   0.02344  -0.0481   0.1172   1.0000
  11.250   1.5579   0.03127   0.02512  -0.0470   0.1097   1.0000
  11.500   1.5619   0.03305   0.02690  -0.0459   0.1036   1.0000
  11.750   1.5699   0.03456   0.02843  -0.0453   0.1001   1.0000
  12.000   1.5715   0.03664   0.03051  -0.0443   0.0926   1.0000
  12.250   1.5652   0.03949   0.03332  -0.0430   0.0772   1.0000
  12.500   1.5483   0.04351   0.03727  -0.0416   0.0607   1.0000
  12.750   1.5480   0.04606   0.03986  -0.0411   0.0577   1.0000
  13.000   1.5490   0.04852   0.04237  -0.0407   0.0558   1.0000
  13.250   1.5472   0.05135   0.04525  -0.0404   0.0540   1.0000
  13.500   1.5462   0.05416   0.04812  -0.0402   0.0528   1.0000
  13.750   1.5441   0.05711   0.05115  -0.0400   0.0516   1.0000
  14.000   1.5414   0.06020   0.05431  -0.0400   0.0506   1.0000
  14.250   1.5357   0.06370   0.05788  -0.0400   0.0499   1.0000
  14.500   1.5288   0.06746   0.06173  -0.0401   0.0493   1.0000
  14.750   1.5181   0.07174   0.06611  -0.0404   0.0486   1.0000
  15.000   1.5050   0.07648   0.07095  -0.0409   0.0480   1.0000
  15.250   1.4919   0.08134   0.07591  -0.0415   0.0476   1.0000
  15.500   1.4762   0.08661   0.08129  -0.0423   0.0472   1.0000
  15.750   1.4586   0.09219   0.08699  -0.0432   0.0469   1.0000
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