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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 200,000
Max Cl/Cd: 59.06 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-200000-n5.txt
Download as CSV file: xf-rhodesg34-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 34                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.2572   0.12983   0.12594  -0.0416   1.0000   0.0461
 -14.000  -0.2582   0.12683   0.12297  -0.0426   1.0000   0.0473
 -13.750  -0.2632   0.12374   0.11993  -0.0438   1.0000   0.0478
 -13.500  -0.2590   0.11938   0.11559  -0.0474   0.9931   0.0479
 -13.250  -0.2525   0.11432   0.11052  -0.0525   0.9833   0.0481
 -13.000  -0.2436   0.10954   0.10572  -0.0571   0.9726   0.0482
 -12.500  -0.2100   0.10057   0.09669  -0.0628   0.9544   0.0423
 -12.250  -0.1904   0.09708   0.09317  -0.0661   0.9455   0.0415
 -12.000  -0.1739   0.09255   0.08860  -0.0712   0.9368   0.0407
 -11.750  -0.1607   0.08743   0.08344  -0.0769   0.9278   0.0399
 -11.500  -0.1479   0.08205   0.07802  -0.0832   0.9188   0.0395
 -11.250  -0.1339   0.07720   0.07311  -0.0892   0.9091   0.0400
 -11.000  -0.1247   0.07186   0.06772  -0.0954   0.8983   0.0401
 -10.750  -0.1223   0.06572   0.06152  -0.1022   0.8866   0.0399
 -10.500  -0.2527   0.04086   0.03597  -0.1174   0.8674   0.0385
 -10.250  -0.2606   0.03696   0.03170  -0.1161   0.8590   0.0386
 -10.000  -0.2557   0.03415   0.02855  -0.1150   0.8524   0.0389
  -9.750  -0.2490   0.03178   0.02588  -0.1133   0.8452   0.0392
  -9.500  -0.2359   0.03003   0.02386  -0.1119   0.8386   0.0397
  -9.250  -0.2199   0.02835   0.02186  -0.1108   0.8332   0.0404
  -9.000  -0.2058   0.02672   0.01993  -0.1090   0.8263   0.0410
  -8.750  -0.1888   0.02514   0.01800  -0.1076   0.8201   0.0417
  -8.500  -0.1689   0.02371   0.01620  -0.1064   0.8146   0.0422
  -8.250  -0.1496   0.02255   0.01474  -0.1050   0.8078   0.0426
  -8.000  -0.1268   0.02170   0.01381  -0.1041   0.8015   0.0431
  -7.750  -0.1027   0.02103   0.01303  -0.1033   0.7958   0.0436
  -7.500  -0.0801   0.02040   0.01234  -0.1023   0.7885   0.0442
  -7.250  -0.0557   0.01976   0.01159  -0.1014   0.7820   0.0448
  -7.000  -0.0319   0.01920   0.01092  -0.1005   0.7749   0.0458
  -6.750  -0.0079   0.01863   0.01023  -0.0996   0.7671   0.0469
  -6.500   0.0168   0.01809   0.00951  -0.0987   0.7591   0.0481
  -6.250   0.0407   0.01753   0.00898  -0.0978   0.7498   0.0490
  -6.000   0.0651   0.01707   0.00851  -0.0969   0.7406   0.0499
  -5.750   0.0896   0.01663   0.00803  -0.0960   0.7305   0.0510
  -5.500   0.1135   0.01621   0.00756  -0.0950   0.7180   0.0522
  -5.250   0.1378   0.01581   0.00709  -0.0941   0.7041   0.0537
  -5.000   0.1620   0.01542   0.00667  -0.0931   0.6900   0.0553
  -4.750   0.1863   0.01512   0.00632  -0.0922   0.6748   0.0572
  -4.500   0.2105   0.01485   0.00595  -0.0912   0.6580   0.0596
  -4.250   0.2342   0.01461   0.00559  -0.0901   0.6399   0.0617
  -4.000   0.2572   0.01439   0.00529  -0.0890   0.6211   0.0641
  -3.750   0.2803   0.01426   0.00505  -0.0878   0.6013   0.0672
  -3.500   0.3027   0.01413   0.00482  -0.0866   0.5793   0.0707
  -3.250   0.3247   0.01406   0.00463  -0.0853   0.5532   0.0751
  -3.000   0.3454   0.01402   0.00445  -0.0838   0.5168   0.0800
  -2.750   0.3633   0.01412   0.00433  -0.0818   0.4698   0.0869
  -2.500   0.3810   0.01421   0.00434  -0.0798   0.4372   0.1012
  -2.250   0.4009   0.01433   0.00445  -0.0783   0.4169   0.1430
  -2.000   0.4220   0.01443   0.00450  -0.0770   0.4033   0.1650
  -1.500   0.4654   0.01455   0.00460  -0.0746   0.3852   0.2047
  -1.250   0.4868   0.01456   0.00468  -0.0734   0.3785   0.2387
  -1.000   0.5068   0.01443   0.00478  -0.0721   0.3733   0.3247
  -0.750   0.5235   0.01394   0.00491  -0.0701   0.3690   0.5161
  -0.500   0.5401   0.01337   0.00513  -0.0675   0.3648   0.7646
  -0.250   0.6640   0.01381   0.00564  -0.0873   0.3564   1.0000
   0.000   0.6841   0.01399   0.00575  -0.0858   0.3535   1.0000
   0.250   0.7048   0.01416   0.00586  -0.0844   0.3507   1.0000
   0.500   0.7255   0.01435   0.00599  -0.0831   0.3478   1.0000
   0.750   0.7461   0.01456   0.00612  -0.0818   0.3449   1.0000
   1.000   0.7666   0.01478   0.00627  -0.0804   0.3421   1.0000
   1.250   0.7868   0.01503   0.00643  -0.0790   0.3391   1.0000
   1.500   0.8074   0.01533   0.00662  -0.0778   0.3363   1.0000
   1.750   0.8291   0.01551   0.00679  -0.0767   0.3341   1.0000
   2.000   0.8506   0.01571   0.00698  -0.0756   0.3316   1.0000
   2.250   0.8725   0.01593   0.00718  -0.0745   0.3297   1.0000
   2.500   0.8942   0.01616   0.00739  -0.0735   0.3276   1.0000
   2.750   0.9156   0.01639   0.00760  -0.0724   0.3251   1.0000
   3.000   0.9370   0.01665   0.00782  -0.0714   0.3228   1.0000
   3.250   0.9584   0.01693   0.00805  -0.0704   0.3206   1.0000
   3.500   0.9808   0.01724   0.00832  -0.0696   0.3187   1.0000
   3.750   1.0032   0.01755   0.00860  -0.0688   0.3167   1.0000
   4.000   1.0245   0.01777   0.00886  -0.0678   0.3148   1.0000
   4.250   1.0454   0.01801   0.00914  -0.0667   0.3125   1.0000
   4.500   1.0651   0.01824   0.00940  -0.0655   0.3095   1.0000
   4.750   1.0833   0.01848   0.00965  -0.0640   0.3063   1.0000
   5.000   1.1014   0.01875   0.00991  -0.0625   0.3033   1.0000
   5.250   1.1203   0.01907   0.01020  -0.0612   0.3006   1.0000
   5.500   1.1403   0.01940   0.01052  -0.0601   0.2983   1.0000
   5.750   1.1588   0.01966   0.01086  -0.0587   0.2961   1.0000
   6.000   1.1774   0.01994   0.01121  -0.0575   0.2937   1.0000
   6.250   1.1954   0.02024   0.01156  -0.0561   0.2909   1.0000
   6.500   1.2125   0.02054   0.01191  -0.0547   0.2878   1.0000
   6.750   1.2296   0.02088   0.01227  -0.0533   0.2849   1.0000
   7.000   1.2478   0.02126   0.01266  -0.0522   0.2828   1.0000
   7.250   1.2660   0.02164   0.01308  -0.0511   0.2805   1.0000
   7.500   1.2835   0.02200   0.01355  -0.0499   0.2779   1.0000
   7.750   1.3002   0.02238   0.01404  -0.0486   0.2746   1.0000
   8.000   1.3145   0.02280   0.01452  -0.0471   0.2701   1.0000
   8.250   1.3281   0.02327   0.01501  -0.0456   0.2663   1.0000
   8.500   1.3437   0.02375   0.01558  -0.0444   0.2622   1.0000
   8.750   1.3592   0.02424   0.01619  -0.0432   0.2576   1.0000
   9.000   1.3730   0.02480   0.01682  -0.0419   0.2532   1.0000
   9.250   1.3861   0.02542   0.01750  -0.0406   0.2486   1.0000
   9.500   1.4005   0.02603   0.01823  -0.0395   0.2414   1.0000
   9.750   1.4118   0.02678   0.01904  -0.0382   0.2333   1.0000
  10.000   1.4230   0.02759   0.01991  -0.0370   0.2222   1.0000
  10.250   1.4290   0.02869   0.02099  -0.0353   0.2013   1.0000
  10.500   1.4179   0.03093   0.02299  -0.0326   0.1716   1.0000
  10.750   1.4125   0.03312   0.02510  -0.0305   0.1573   1.0000
  11.000   1.4102   0.03522   0.02721  -0.0289   0.1480   1.0000
  11.250   1.4073   0.03748   0.02950  -0.0275   0.1403   1.0000
  11.500   1.4074   0.03960   0.03167  -0.0264   0.1351   1.0000
  11.750   1.4045   0.04209   0.03422  -0.0254   0.1307   1.0000
  12.000   1.4052   0.04437   0.03660  -0.0247   0.1265   1.0000
  12.250   1.4033   0.04700   0.03932  -0.0242   0.1225   1.0000
  12.500   1.3975   0.05018   0.04259  -0.0238   0.1186   1.0000
  12.750   1.3938   0.05328   0.04579  -0.0237   0.1150   1.0000
  13.000   1.3892   0.05659   0.04921  -0.0237   0.1107   1.0000
  13.250   1.3809   0.06048   0.05319  -0.0239   0.1069   1.0000
  13.500   1.3710   0.06471   0.05752  -0.0244   0.1033   1.0000
  13.750   1.3636   0.06877   0.06170  -0.0250   0.0976   1.0000
  14.000   1.3508   0.07370   0.06673  -0.0260   0.0929   1.0000
  14.250   1.3425   0.07813   0.07128  -0.0270   0.0842   1.0000
  14.500   1.3247   0.08401   0.07721  -0.0284   0.0743   1.0000
  14.750   1.3049   0.09030   0.08350  -0.0301   0.0695   1.0000
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