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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.04 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-1000000.txt
Download as CSV file: xf-rhodesg32-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 32                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0709   0.03398   0.03130  -0.1046   1.0000   0.0226
 -16.750  -1.0861   0.03157   0.02873  -0.1024   1.0000   0.0228
 -16.500  -1.0930   0.03019   0.02723  -0.0987   1.0000   0.0230
 -16.250  -1.0921   0.02876   0.02567  -0.0961   1.0000   0.0232
 -16.000  -1.0939   0.02724   0.02406  -0.0929   1.0000   0.0237
 -15.750  -1.0834   0.02662   0.02342  -0.0905   1.0000   0.0241
 -15.500  -1.0692   0.02635   0.02317  -0.0883   1.0000   0.0245
 -15.250  -1.0590   0.02610   0.02291  -0.0853   1.0000   0.0248
 -15.000  -1.0299   0.02587   0.02267  -0.0858   0.9990   0.0253
 -14.750  -0.9969   0.02559   0.02236  -0.0870   0.9974   0.0260
 -14.500  -0.9666   0.02459   0.02122  -0.0884   0.9950   0.0266
 -14.250  -0.9345   0.02404   0.02057  -0.0896   0.9925   0.0270
 -14.000  -0.9094   0.02246   0.01884  -0.0906   0.9879   0.0278
 -13.750  -0.8760   0.02224   0.01864  -0.0918   0.9852   0.0282
 -13.500  -0.8402   0.02237   0.01882  -0.0931   0.9831   0.0287
 -13.250  -0.8100   0.02220   0.01864  -0.0935   0.9781   0.0291
 -13.000  -0.7769   0.02215   0.01856  -0.0944   0.9741   0.0297
 -12.750  -0.7431   0.02155   0.01787  -0.0960   0.9711   0.0304
 -12.500  -0.7125   0.02083   0.01702  -0.0970   0.9657   0.0310
 -12.250  -0.6793   0.02055   0.01665  -0.0981   0.9604   0.0315
 -12.000  -0.6523   0.01888   0.01479  -0.0991   0.9535   0.0323
 -11.750  -0.6215   0.01870   0.01460  -0.0997   0.9452   0.0327
 -11.500  -0.5912   0.01866   0.01453  -0.1001   0.9374   0.0331
 -11.250  -0.5650   0.01836   0.01417  -0.0997   0.9287   0.0336
 -11.000  -0.5387   0.01828   0.01403  -0.0993   0.9206   0.0341
 -10.750  -0.5145   0.01792   0.01358  -0.0985   0.9126   0.0347
 -10.500  -0.4912   0.01738   0.01291  -0.0977   0.9054   0.0353
 -10.250  -0.4674   0.01705   0.01247  -0.0968   0.8978   0.0360
 -10.000  -0.4430   0.01671   0.01199  -0.0960   0.8908   0.0364
  -9.750  -0.4228   0.01545   0.01056  -0.0948   0.8840   0.0371
  -9.500  -0.3988   0.01492   0.00996  -0.0941   0.8777   0.0377
  -9.250  -0.3732   0.01474   0.00976  -0.0935   0.8717   0.0382
  -9.000  -0.3478   0.01454   0.00953  -0.0928   0.8647   0.0387
  -8.750  -0.3228   0.01419   0.00909  -0.0921   0.8573   0.0392
  -8.500  -0.2976   0.01384   0.00868  -0.0914   0.8491   0.0398
  -8.250  -0.2724   0.01346   0.00821  -0.0906   0.8411   0.0404
  -8.000  -0.2470   0.01306   0.00774  -0.0900   0.8326   0.0410
  -7.750  -0.2212   0.01281   0.00740  -0.0893   0.8242   0.0417
  -7.500  -0.1951   0.01262   0.00714  -0.0887   0.8138   0.0421
  -7.250  -0.1690   0.01245   0.00689  -0.0881   0.8036   0.0424
  -7.000  -0.1461   0.01132   0.00566  -0.0872   0.7919   0.0435
  -6.750  -0.1207   0.01098   0.00528  -0.0865   0.7783   0.0441
  -6.500  -0.0951   0.01077   0.00502  -0.0858   0.7637   0.0447
  -6.250  -0.0695   0.01059   0.00476  -0.0852   0.7477   0.0454
  -6.000  -0.0441   0.01046   0.00455  -0.0844   0.7294   0.0462
  -5.750  -0.0190   0.01030   0.00430  -0.0837   0.7097   0.0469
  -5.500   0.0061   0.01015   0.00405  -0.0829   0.6874   0.0476
  -5.250   0.0309   0.01005   0.00384  -0.0821   0.6642   0.0483
  -5.000   0.0562   0.00999   0.00367  -0.0813   0.6425   0.0488
  -4.750   0.0817   0.00997   0.00356  -0.0807   0.6198   0.0492
  -4.500   0.1043   0.00955   0.00303  -0.0795   0.5946   0.0505
  -4.250   0.1279   0.00949   0.00283  -0.0786   0.5568   0.0516
  -4.000   0.1483   0.00976   0.00277  -0.0771   0.4710   0.0526
  -3.750   0.1684   0.01011   0.00278  -0.0755   0.3890   0.0535
  -3.500   0.1930   0.01016   0.00271  -0.0748   0.3643   0.0545
  -3.250   0.2185   0.01016   0.00263  -0.0742   0.3518   0.0555
  -3.000   0.2448   0.01013   0.00256  -0.0738   0.3448   0.0565
  -2.750   0.2710   0.01013   0.00252  -0.0733   0.3388   0.0572
  -2.500   0.2965   0.01003   0.00237  -0.0727   0.3334   0.0589
  -2.250   0.3228   0.00992   0.00227  -0.0723   0.3309   0.0611
  -2.000   0.3493   0.00988   0.00222  -0.0719   0.3281   0.0630
  -1.750   0.3758   0.00986   0.00219  -0.0715   0.3253   0.0648
  -1.500   0.4021   0.00988   0.00218  -0.0711   0.3221   0.0664
  -1.250   0.4278   0.00990   0.00217  -0.0706   0.3180   0.0695
  -1.000   0.4542   0.00987   0.00216  -0.0703   0.3159   0.0749
  -0.500   0.5061   0.00966   0.00222  -0.0695   0.3130   0.1625
  -0.250   0.5322   0.00961   0.00225  -0.0691   0.3108   0.1919
   0.000   0.5558   0.00932   0.00232  -0.0684   0.3088   0.3269
   0.250   0.5754   0.00875   0.00241  -0.0670   0.3069   0.5746
   0.500   0.5893   0.00815   0.00253  -0.0641   0.3051   0.8154
   1.000   0.7164   0.00833   0.00297  -0.0796   0.2995   0.9963
   1.250   0.7603   0.00842   0.00305  -0.0832   0.2984   1.0000
   1.500   0.7834   0.00851   0.00312  -0.0822   0.2974   1.0000
   1.750   0.8065   0.00860   0.00321  -0.0813   0.2964   1.0000
   2.000   0.8298   0.00869   0.00329  -0.0804   0.2950   1.0000
   2.250   0.8533   0.00878   0.00337  -0.0795   0.2934   1.0000
   2.500   0.8767   0.00887   0.00345  -0.0786   0.2913   1.0000
   2.750   0.8998   0.00899   0.00355  -0.0777   0.2886   1.0000
   3.000   0.9220   0.00917   0.00370  -0.0767   0.2853   1.0000
   3.250   0.9453   0.00929   0.00382  -0.0758   0.2835   1.0000
   3.500   0.9697   0.00936   0.00391  -0.0752   0.2823   1.0000
   3.750   0.9942   0.00942   0.00399  -0.0746   0.2803   1.0000
   4.000   1.0185   0.00951   0.00408  -0.0740   0.2781   1.0000
   4.250   1.0426   0.00960   0.00418  -0.0733   0.2757   1.0000
   4.500   1.0662   0.00972   0.00430  -0.0726   0.2728   1.0000
   4.750   1.0887   0.00990   0.00445  -0.0717   0.2690   1.0000
   5.000   1.1136   0.00995   0.00454  -0.0713   0.2656   1.0000
   5.250   1.1379   0.01004   0.00463  -0.0707   0.2607   1.0000
   5.500   1.1609   0.01019   0.00475  -0.0700   0.2550   1.0000
   5.750   1.1845   0.01030   0.00488  -0.0693   0.2485   1.0000
   6.000   1.2068   0.01049   0.00502  -0.0685   0.2361   1.0000
   6.250   1.2129   0.01157   0.00565  -0.0650   0.1619   1.0000
   6.750   1.2465   0.01255   0.00650  -0.0615   0.1360   1.0000
   7.000   1.2649   0.01293   0.00686  -0.0601   0.1281   1.0000
   7.250   1.2818   0.01330   0.00720  -0.0583   0.1206   1.0000
   7.500   1.2982   0.01365   0.00754  -0.0565   0.1132   1.0000
   7.750   1.3128   0.01410   0.00794  -0.0544   0.1026   1.0000
   8.000   1.3221   0.01485   0.00850  -0.0516   0.0719   1.0000
   8.250   1.3290   0.01574   0.00926  -0.0485   0.0552   1.0000
   8.500   1.3429   0.01629   0.00982  -0.0466   0.0509   1.0000
   8.750   1.3566   0.01687   0.01041  -0.0447   0.0481   1.0000
   9.000   1.3683   0.01757   0.01113  -0.0427   0.0450   1.0000
   9.500   1.3987   0.01863   0.01227  -0.0398   0.0420   1.0000
  10.000   1.4215   0.02021   0.01391  -0.0364   0.0381   1.0000
  10.250   1.4353   0.02090   0.01465  -0.0351   0.0370   1.0000
  10.500   1.4495   0.02158   0.01538  -0.0339   0.0357   1.0000
  10.750   1.4618   0.02242   0.01624  -0.0326   0.0342   1.0000
  11.000   1.4706   0.02351   0.01735  -0.0311   0.0325   1.0000
  11.250   1.4809   0.02454   0.01844  -0.0299   0.0312   1.0000
  11.500   1.4935   0.02544   0.01939  -0.0289   0.0300   1.0000
  11.750   1.5033   0.02658   0.02056  -0.0278   0.0286   1.0000
  12.000   1.5099   0.02801   0.02202  -0.0267   0.0273   1.0000
  12.250   1.5164   0.02951   0.02358  -0.0256   0.0262   1.0000
  12.500   1.5265   0.03076   0.02489  -0.0249   0.0249   1.0000
  12.750   1.5322   0.03243   0.02660  -0.0241   0.0239   1.0000
  13.000   1.5349   0.03445   0.02866  -0.0234   0.0228   1.0000
  13.250   1.5377   0.03654   0.03082  -0.0227   0.0218   1.0000
  13.500   1.5413   0.03862   0.03298  -0.0223   0.0212   1.0000
  13.750   1.5433   0.04097   0.03539  -0.0221   0.0204   1.0000
  14.000   1.5425   0.04370   0.03819  -0.0219   0.0196   1.0000
  14.250   1.5358   0.04721   0.04178  -0.0219   0.0188   1.0000
  14.500   1.5302   0.05072   0.04538  -0.0221   0.0184   1.0000
  14.750   1.5272   0.05404   0.04879  -0.0225   0.0181   1.0000
  15.000   1.5225   0.05763   0.05248  -0.0230   0.0176   1.0000
  15.250   1.5156   0.06163   0.05658  -0.0237   0.0172   1.0000
  15.500   1.5063   0.06605   0.06110  -0.0247   0.0170   1.0000
  15.750   1.4952   0.07081   0.06595  -0.0258   0.0166   1.0000
  16.000   1.4830   0.07581   0.07105  -0.0270   0.0164   1.0000
  16.250   1.4687   0.08117   0.07651  -0.0284   0.0161   1.0000
  16.500   1.4528   0.08676   0.08218  -0.0299   0.0157   1.0000
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