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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.38 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-1000000-n5.txt
Download as CSV file: xf-rhodesg30-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 30                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5056   0.11388   0.11213  -0.0209   1.0000   0.0038
 -13.750  -0.5290   0.10388   0.10209  -0.0254   1.0000   0.0037
 -13.500  -0.5472   0.09567   0.09384  -0.0295   1.0000   0.0037
 -13.250  -0.5643   0.08817   0.08631  -0.0335   1.0000   0.0037
 -13.000  -0.5796   0.08150   0.07961  -0.0373   1.0000   0.0036
 -12.750  -0.6035   0.07353   0.07161  -0.0421   1.0000   0.0035
 -12.500  -0.6259   0.06611   0.06418  -0.0468   1.0000   0.0035
 -12.250  -0.6807   0.05530   0.05335  -0.0548   1.0000   0.0034
 -11.750  -0.7138   0.03277   0.03012  -0.0718   0.9888   0.0034
 -11.500  -0.6953   0.02952   0.02663  -0.0740   0.9804   0.0034
 -11.250  -0.6709   0.02687   0.02376  -0.0764   0.9743   0.0035
 -11.000  -0.6449   0.02468   0.02137  -0.0782   0.9665   0.0035
 -10.750  -0.6170   0.02270   0.01919  -0.0800   0.9576   0.0036
 -10.500  -0.5884   0.02112   0.01744  -0.0815   0.9468   0.0037
 -10.250  -0.5623   0.01985   0.01599  -0.0820   0.9332   0.0039
  -9.750  -0.5189   0.01765   0.01344  -0.0807   0.9079   0.0041
  -9.500  -0.4972   0.01671   0.01234  -0.0798   0.8988   0.0042
  -9.250  -0.4746   0.01591   0.01139  -0.0790   0.8907   0.0043
  -9.000  -0.4514   0.01519   0.01055  -0.0783   0.8828   0.0043
  -8.750  -0.4288   0.01436   0.00957  -0.0774   0.8740   0.0044
  -8.500  -0.4052   0.01363   0.00871  -0.0767   0.8654   0.0047
  -8.250  -0.3804   0.01310   0.00808  -0.0761   0.8586   0.0048
  -8.000  -0.3552   0.01261   0.00749  -0.0755   0.8504   0.0050
  -7.750  -0.3300   0.01217   0.00695  -0.0749   0.8426   0.0051
  -7.500  -0.3045   0.01175   0.00645  -0.0743   0.8326   0.0053
  -7.250  -0.2789   0.01137   0.00597  -0.0738   0.8219   0.0055
  -7.000  -0.2532   0.01103   0.00553  -0.0732   0.8107   0.0058
  -6.750  -0.2272   0.01076   0.00516  -0.0727   0.7983   0.0060
  -6.500  -0.2011   0.01055   0.00487  -0.0721   0.7846   0.0063
  -6.250  -0.1749   0.01039   0.00463  -0.0716   0.7692   0.0068
  -6.000  -0.1490   0.01018   0.00433  -0.0711   0.7529   0.0073
  -5.750  -0.1232   0.00995   0.00400  -0.0705   0.7361   0.0077
  -5.500  -0.0976   0.00972   0.00365  -0.0699   0.7172   0.0082
  -5.250  -0.0723   0.00952   0.00332  -0.0693   0.6950   0.0086
  -5.000  -0.0474   0.00924   0.00288  -0.0686   0.6733   0.0093
  -4.750  -0.0223   0.00906   0.00255  -0.0679   0.6491   0.0103
  -4.500   0.0036   0.00894   0.00231  -0.0674   0.6297   0.0114
  -4.250   0.0297   0.00880   0.00208  -0.0669   0.6133   0.0128
  -4.000   0.0559   0.00868   0.00186  -0.0664   0.5961   0.0153
  -3.750   0.0820   0.00860   0.00180  -0.0660   0.5764   0.0353
  -3.500   0.1089   0.00877   0.00195  -0.0658   0.5517   0.0380
  -3.250   0.1349   0.00892   0.00198  -0.0653   0.5152   0.0391
  -3.000   0.1601   0.00921   0.00208  -0.0648   0.4641   0.0398
  -2.750   0.1852   0.00934   0.00205  -0.0642   0.4238   0.0405
  -2.500   0.2110   0.00941   0.00203  -0.0638   0.3978   0.0415
  -2.250   0.2376   0.00952   0.00209  -0.0635   0.3787   0.0423
  -2.000   0.2640   0.00955   0.00207  -0.0632   0.3637   0.0429
  -1.750   0.2904   0.00955   0.00201  -0.0629   0.3507   0.0433
  -1.500   0.3168   0.00955   0.00196  -0.0625   0.3396   0.0438
  -1.250   0.3437   0.00951   0.00190  -0.0623   0.3332   0.0443
  -1.000   0.3703   0.00952   0.00187  -0.0620   0.3266   0.0448
  -0.750   0.3974   0.00950   0.00184  -0.0618   0.3214   0.0453
  -0.500   0.4243   0.00948   0.00182  -0.0616   0.3174   0.0457
  -0.250   0.4512   0.00950   0.00182  -0.0614   0.3131   0.0462
   0.000   0.4781   0.00950   0.00182  -0.0612   0.3079   0.0465
   0.250   0.5048   0.00953   0.00184  -0.0610   0.3012   0.0468
   0.500   0.5315   0.00957   0.00186  -0.0608   0.2959   0.0470
   0.750   0.5583   0.00953   0.00182  -0.0605   0.2934   0.0484
   1.000   0.5852   0.00953   0.00183  -0.0604   0.2893   0.0498
   1.250   0.6119   0.00956   0.00186  -0.0602   0.2841   0.0512
   1.500   0.6385   0.00962   0.00191  -0.0600   0.2780   0.0527
   1.750   0.6654   0.00966   0.00197  -0.0598   0.2728   0.0541
   2.000   0.6919   0.00973   0.00203  -0.0596   0.2669   0.0554
   2.250   0.7185   0.00980   0.00211  -0.0594   0.2601   0.0564
   2.500   0.7446   0.00991   0.00219  -0.0591   0.2500   0.0573
   2.750   0.7703   0.01005   0.00229  -0.0588   0.2354   0.0607
   3.000   0.7869   0.01100   0.00279  -0.0571   0.1368   0.0684
   3.250   0.8092   0.01095   0.00309  -0.0564   0.1175   0.2937
   3.750   0.8782   0.01042   0.00393  -0.0607   0.0547   1.0000
   4.000   0.9011   0.01073   0.00420  -0.0599   0.0432   1.0000
   4.250   0.9245   0.01100   0.00444  -0.0592   0.0391   1.0000
   4.500   0.9481   0.01125   0.00470  -0.0585   0.0358   1.0000
   4.750   0.9719   0.01149   0.00495  -0.0578   0.0341   1.0000
   5.000   0.9957   0.01172   0.00519  -0.0572   0.0336   1.0000
   5.250   1.0194   0.01197   0.00546  -0.0566   0.0331   1.0000
   5.500   1.0430   0.01222   0.00574  -0.0560   0.0326   1.0000
   5.750   1.0664   0.01249   0.00604  -0.0553   0.0319   1.0000
   6.000   1.0896   0.01277   0.00632  -0.0547   0.0305   1.0000
   6.250   1.1123   0.01308   0.00664  -0.0540   0.0290   1.0000
   6.500   1.1346   0.01341   0.00699  -0.0532   0.0276   1.0000
   6.750   1.1564   0.01378   0.00738  -0.0524   0.0262   1.0000
   7.000   1.1776   0.01419   0.00784  -0.0514   0.0250   1.0000
   7.250   1.2006   0.01443   0.00809  -0.0509   0.0246   1.0000
   7.500   1.2233   0.01468   0.00838  -0.0502   0.0240   1.0000
   7.750   1.2455   0.01495   0.00868  -0.0495   0.0228   1.0000
   8.000   1.2669   0.01528   0.00901  -0.0487   0.0202   1.0000
   8.250   1.2864   0.01571   0.00939  -0.0477   0.0158   1.0000
   8.500   1.3047   0.01621   0.00985  -0.0464   0.0119   1.0000
   8.750   1.3222   0.01674   0.01039  -0.0450   0.0099   1.0000
   9.000   1.3386   0.01728   0.01096  -0.0435   0.0083   1.0000
   9.250   1.3530   0.01780   0.01152  -0.0415   0.0075   1.0000
   9.500   1.3650   0.01840   0.01215  -0.0392   0.0067   1.0000
   9.750   1.3763   0.01904   0.01284  -0.0368   0.0060   1.0000
  10.000   1.3889   0.01963   0.01349  -0.0348   0.0057   1.0000
  10.250   1.4005   0.02031   0.01422  -0.0328   0.0053   1.0000
  10.500   1.4112   0.02105   0.01503  -0.0308   0.0050   1.0000
  10.750   1.4201   0.02193   0.01596  -0.0287   0.0046   1.0000
  11.000   1.4281   0.02292   0.01701  -0.0266   0.0043   1.0000
  11.250   1.4369   0.02390   0.01807  -0.0249   0.0041   1.0000
  11.500   1.4453   0.02496   0.01920  -0.0232   0.0040   1.0000
  11.750   1.4527   0.02614   0.02046  -0.0216   0.0038   1.0000
  12.000   1.4593   0.02744   0.02183  -0.0201   0.0036   1.0000
  12.250   1.4646   0.02891   0.02339  -0.0187   0.0036   1.0000
  12.500   1.4689   0.03055   0.02511  -0.0175   0.0033   1.0000
  12.750   1.4729   0.03230   0.02695  -0.0165   0.0033   1.0000
  13.000   1.4743   0.03440   0.02913  -0.0156   0.0031   1.0000
  13.250   1.4759   0.03658   0.03140  -0.0150   0.0030   1.0000
  13.500   1.4759   0.03908   0.03400  -0.0146   0.0030   1.0000
  13.750   1.4737   0.04193   0.03695  -0.0144   0.0029   1.0000
  14.000   1.4661   0.04555   0.04069  -0.0145   0.0028   1.0000
  14.250   1.4622   0.04893   0.04417  -0.0150   0.0027   1.0000
  14.500   1.4564   0.05268   0.04803  -0.0157   0.0027   1.0000
  14.750   1.4507   0.05660   0.05207  -0.0166   0.0027   1.0000
  15.000   1.4452   0.06064   0.05622  -0.0178   0.0026   1.0000
  15.250   1.4362   0.06533   0.06103  -0.0193   0.0026   1.0000
  15.500   1.4287   0.06993   0.06574  -0.0209   0.0025   1.0000
  15.750   1.4164   0.07542   0.07135  -0.0229   0.0025   1.0000
  16.000   1.4090   0.08018   0.07621  -0.0247   0.0025   1.0000
  16.250   1.3946   0.08613   0.08228  -0.0270   0.0025   1.0000
  16.500   1.3820   0.09190   0.08817  -0.0293   0.0025   1.0000
  16.750   1.3694   0.09769   0.09406  -0.0317   0.0025   1.0000
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