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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.99 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-1000000.txt
Download as CSV file: xf-rhodesg36-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.5321   0.03954   0.03684  -0.1469   0.9658   0.0317
 -15.750  -0.5933   0.03300   0.03000  -0.1492   0.9551   0.0316
 -15.500  -0.6161   0.03111   0.02797  -0.1457   0.9473   0.0317
 -15.250  -0.6399   0.02907   0.02576  -0.1413   0.9389   0.0318
 -15.000  -0.6532   0.02791   0.02446  -0.1361   0.9323   0.0319
 -14.750  -0.6569   0.02661   0.02302  -0.1324   0.9254   0.0320
 -14.500  -0.6542   0.02554   0.02182  -0.1291   0.9209   0.0322
 -14.250  -0.6418   0.02451   0.02067  -0.1273   0.9141   0.0325
 -14.000  -0.6315   0.02347   0.01949  -0.1249   0.9085   0.0327
 -13.750  -0.6159   0.02252   0.01843  -0.1233   0.9004   0.0329
 -13.500  -0.6000   0.02164   0.01742  -0.1215   0.8914   0.0330
 -13.250  -0.5852   0.02060   0.01622  -0.1196   0.8786   0.0332
 -13.000  -0.5747   0.01903   0.01445  -0.1172   0.8622   0.0336
 -12.750  -0.5563   0.01835   0.01363  -0.1155   0.8463   0.0339
 -12.500  -0.5349   0.01786   0.01304  -0.1142   0.8335   0.0341
 -12.250  -0.5120   0.01747   0.01257  -0.1132   0.8229   0.0344
 -12.000  -0.4888   0.01711   0.01211  -0.1122   0.8132   0.0346
 -11.750  -0.4647   0.01671   0.01164  -0.1114   0.8053   0.0349
 -11.500  -0.4406   0.01633   0.01117  -0.1105   0.7975   0.0353
 -11.250  -0.4162   0.01593   0.01068  -0.1097   0.7907   0.0357
 -11.000  -0.3913   0.01549   0.01017  -0.1091   0.7839   0.0360
 -10.750  -0.3665   0.01510   0.00968  -0.1083   0.7761   0.0364
 -10.500  -0.3410   0.01472   0.00922  -0.1076   0.7695   0.0368
 -10.250  -0.3150   0.01440   0.00882  -0.1070   0.7619   0.0371
 -10.000  -0.2894   0.01408   0.00840  -0.1064   0.7542   0.0374
  -9.750  -0.2653   0.01337   0.00766  -0.1057   0.7464   0.0381
  -9.500  -0.2393   0.01310   0.00734  -0.1051   0.7371   0.0386
  -9.250  -0.2125   0.01287   0.00709  -0.1046   0.7285   0.0390
  -9.000  -0.1860   0.01266   0.00682  -0.1041   0.7183   0.0395
  -8.750  -0.1593   0.01243   0.00654  -0.1036   0.7079   0.0401
  -8.500  -0.1330   0.01222   0.00624  -0.1030   0.6961   0.0407
  -8.250  -0.1063   0.01202   0.00597  -0.1025   0.6844   0.0412
  -8.000  -0.0797   0.01186   0.00573  -0.1020   0.6742   0.0417
  -7.750  -0.0542   0.01150   0.00530  -0.1014   0.6649   0.0423
  -7.500  -0.0283   0.01125   0.00502  -0.1008   0.6566   0.0431
  -7.250  -0.0013   0.01111   0.00486  -0.1004   0.6487   0.0437
  -7.000   0.0253   0.01102   0.00471  -0.0999   0.6399   0.0445
  -6.750   0.0526   0.01090   0.00456  -0.0995   0.6319   0.0454
  -6.500   0.0794   0.01084   0.00444  -0.0991   0.6231   0.0463
  -6.250   0.1067   0.01075   0.00430  -0.0987   0.6156   0.0469
  -6.000   0.1318   0.01044   0.00397  -0.0980   0.6069   0.0481
  -5.750   0.1585   0.01035   0.00386  -0.0976   0.5986   0.0490
  -5.500   0.1855   0.01026   0.00375  -0.0972   0.5893   0.0500
  -5.250   0.2119   0.01020   0.00364  -0.0967   0.5795   0.0511
  -5.000   0.2386   0.01017   0.00355  -0.0963   0.5664   0.0520
  -4.750   0.2634   0.01000   0.00333  -0.0956   0.5493   0.0535
  -4.500   0.2870   0.01006   0.00327  -0.0946   0.5139   0.0547
  -4.250   0.3036   0.01051   0.00336  -0.0925   0.4367   0.0559
  -4.000   0.3254   0.01071   0.00339  -0.0913   0.4056   0.0572
  -3.750   0.3492   0.01083   0.00341  -0.0904   0.3882   0.0581
  -3.500   0.3721   0.01077   0.00330  -0.0894   0.3757   0.0599
  -3.250   0.3965   0.01080   0.00329  -0.0886   0.3657   0.0616
  -3.000   0.4209   0.01085   0.00329  -0.0879   0.3576   0.0633
  -2.750   0.4459   0.01087   0.00328  -0.0872   0.3517   0.0648
  -2.500   0.4694   0.01083   0.00322  -0.0863   0.3457   0.0672
  -2.250   0.4932   0.01086   0.00322  -0.0855   0.3402   0.0695
  -2.000   0.5183   0.01087   0.00322  -0.0849   0.3370   0.0717
  -1.750   0.5422   0.01083   0.00319  -0.0841   0.3334   0.0756
  -1.500   0.5656   0.01086   0.00320  -0.0832   0.3296   0.0794
  -1.250   0.5876   0.01087   0.00323  -0.0820   0.3255   0.0913
  -1.000   0.6094   0.01086   0.00336  -0.0809   0.3220   0.1444
  -0.750   0.6329   0.01087   0.00342  -0.0800   0.3203   0.1569
  -0.500   0.6550   0.01090   0.00346  -0.0789   0.3182   0.1639
  -0.250   0.6758   0.01093   0.00351  -0.0775   0.3158   0.1707
   0.000   0.6964   0.01101   0.00358  -0.0761   0.3132   0.1756
   0.250   0.7164   0.01110   0.00368  -0.0747   0.3105   0.1840
   0.500   0.7361   0.01123   0.00382  -0.0732   0.3075   0.1926
   0.750   0.7545   0.01135   0.00402  -0.0716   0.3045   0.2251
   1.000   0.7732   0.01108   0.00419  -0.0701   0.3037   0.3963
   1.250   0.7794   0.01034   0.00445  -0.0661   0.3027   0.7505
   1.500   0.9300   0.01041   0.00499  -0.0920   0.2992   1.0000
   1.750   0.9417   0.01052   0.00509  -0.0890   0.2977   1.0000
   2.000   0.9560   0.01066   0.00522  -0.0865   0.2962   1.0000
   2.250   0.9718   0.01083   0.00536  -0.0843   0.2946   1.0000
   2.500   0.9886   0.01102   0.00553  -0.0824   0.2928   1.0000
   2.750   1.0051   0.01126   0.00573  -0.0805   0.2907   1.0000
   3.000   1.0211   0.01155   0.00600  -0.0785   0.2881   1.0000
   3.250   1.0409   0.01174   0.00619  -0.0772   0.2868   1.0000
   3.500   1.0633   0.01184   0.00629  -0.0765   0.2853   1.0000
   3.750   1.0842   0.01201   0.00646  -0.0755   0.2839   1.0000
   4.000   1.1052   0.01218   0.00663  -0.0745   0.2821   1.0000
   4.250   1.1259   0.01238   0.00683  -0.0735   0.2807   1.0000
   4.500   1.1465   0.01260   0.00704  -0.0726   0.2792   1.0000
   4.750   1.1666   0.01284   0.00728  -0.0716   0.2776   1.0000
   5.000   1.1858   0.01313   0.00755  -0.0705   0.2756   1.0000
   5.250   1.2044   0.01345   0.00786  -0.0693   0.2737   1.0000
   5.500   1.2217   0.01386   0.00825  -0.0680   0.2708   1.0000
   5.750   1.2436   0.01407   0.00847  -0.0674   0.2700   1.0000
   6.000   1.2650   0.01429   0.00872  -0.0668   0.2690   1.0000
   6.250   1.2859   0.01456   0.00901  -0.0661   0.2679   1.0000
   6.500   1.3069   0.01483   0.00929  -0.0655   0.2667   1.0000
   6.750   1.3276   0.01511   0.00960  -0.0649   0.2655   1.0000
   7.000   1.3480   0.01541   0.00992  -0.0642   0.2639   1.0000
   7.250   1.3679   0.01575   0.01026  -0.0636   0.2625   1.0000
   7.500   1.3874   0.01611   0.01063  -0.0629   0.2606   1.0000
   7.750   1.4055   0.01655   0.01107  -0.0621   0.2586   1.0000
   8.000   1.4223   0.01707   0.01158  -0.0611   0.2560   1.0000
   8.250   1.4412   0.01750   0.01203  -0.0604   0.2544   1.0000
   8.500   1.4619   0.01784   0.01242  -0.0601   0.2533   1.0000
   8.750   1.4822   0.01820   0.01282  -0.0597   0.2520   1.0000
   9.000   1.5023   0.01859   0.01323  -0.0593   0.2503   1.0000
   9.250   1.5217   0.01902   0.01369  -0.0589   0.2482   1.0000
   9.500   1.5402   0.01951   0.01420  -0.0584   0.2460   1.0000
   9.750   1.5574   0.02008   0.01478  -0.0578   0.2440   1.0000
  10.000   1.5730   0.02075   0.01545  -0.0571   0.2414   1.0000
  10.250   1.5895   0.02139   0.01612  -0.0565   0.2393   1.0000
  10.500   1.6092   0.02185   0.01664  -0.0563   0.2376   1.0000
  10.750   1.6284   0.02234   0.01717  -0.0561   0.2350   1.0000
  11.000   1.6456   0.02297   0.01782  -0.0557   0.2316   1.0000
  11.250   1.6603   0.02377   0.01862  -0.0552   0.2281   1.0000
  11.500   1.6748   0.02459   0.01945  -0.0546   0.2247   1.0000
  11.750   1.6925   0.02520   0.02012  -0.0543   0.2214   1.0000
  12.000   1.7075   0.02601   0.02096  -0.0539   0.2168   1.0000
  12.250   1.7186   0.02711   0.02203  -0.0532   0.2102   1.0000
  12.500   1.7275   0.02838   0.02327  -0.0523   0.1990   1.0000
  12.750   1.7309   0.03008   0.02490  -0.0511   0.1846   1.0000
  13.000   1.7216   0.03281   0.02750  -0.0491   0.1606   1.0000
  13.250   1.6928   0.03729   0.03178  -0.0461   0.1297   1.0000
  13.500   1.6839   0.04034   0.03480  -0.0447   0.1185   1.0000
  13.750   1.6746   0.04357   0.03802  -0.0436   0.1089   1.0000
  14.000   1.6663   0.04681   0.04127  -0.0428   0.1010   1.0000
  14.250   1.6563   0.05034   0.04482  -0.0421   0.0933   1.0000
  14.500   1.6423   0.05441   0.04889  -0.0414   0.0819   1.0000
  14.750   1.6132   0.06028   0.05474  -0.0408   0.0679   1.0000
  15.000   1.5940   0.06529   0.05980  -0.0406   0.0631   1.0000
  15.250   1.5780   0.07009   0.06468  -0.0408   0.0606   1.0000
  15.500   1.5630   0.07495   0.06964  -0.0411   0.0595   1.0000
  15.750   1.5438   0.08049   0.07528  -0.0417   0.0584   1.0000
  16.000   1.5203   0.08673   0.08164  -0.0425   0.0573   1.0000
  16.250   1.4976   0.09294   0.08796  -0.0435   0.0565   1.0000
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