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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 100,000
Max Cl/Cd: 45.6 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-100000-n5.txt
Download as CSV file: xf-rhodesg34-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2538   0.12533   0.12007  -0.0422   1.0000   0.0761
 -13.000  -0.2663   0.12355   0.11839  -0.0425   1.0000   0.0767
 -12.750  -0.2828   0.12228   0.11721  -0.0414   1.0000   0.0769
 -12.250  -0.2537   0.11434   0.10929  -0.0459   0.9906   0.0780
 -12.000  -0.2345   0.11093   0.10587  -0.0477   0.9854   0.0791
 -11.750  -0.2182   0.10760   0.10254  -0.0505   0.9799   0.0810
 -11.500  -0.2101   0.10401   0.09895  -0.0550   0.9725   0.0847
 -11.250  -0.2204   0.09923   0.09418  -0.0643   0.9627   0.0862
 -10.750  -0.1965   0.08605   0.08090  -0.0719   0.9515   0.0617
 -10.500  -0.1797   0.08249   0.07732  -0.0747   0.9447   0.0596
 -10.250  -0.1656   0.07771   0.07251  -0.0802   0.9389   0.0583
 -10.000  -0.1641   0.07273   0.06752  -0.0853   0.9285   0.0572
  -9.750  -0.1692   0.06647   0.06120  -0.0925   0.9178   0.0564
  -9.500  -0.1699   0.06011   0.05470  -0.0988   0.9083   0.0564
  -9.250  -0.1776   0.05381   0.04815  -0.1023   0.8977   0.0560
  -9.000  -0.1890   0.04544   0.03915  -0.1054   0.8891   0.0551
  -8.750  -0.1899   0.04137   0.03462  -0.1043   0.8788   0.0549
  -8.500  -0.1725   0.03837   0.03125  -0.1046   0.8719   0.0551
  -8.250  -0.1588   0.03623   0.02882  -0.1034   0.8636   0.0555
  -8.000  -0.1400   0.03421   0.02650  -0.1027   0.8562   0.0560
  -7.750  -0.1161   0.03246   0.02446  -0.1027   0.8502   0.0570
  -7.500  -0.1002   0.03109   0.02282  -0.1009   0.8410   0.0582
  -7.250  -0.0748   0.02937   0.02069  -0.1007   0.8348   0.0596
  -7.000  -0.0566   0.02810   0.01906  -0.0990   0.8259   0.0604
  -6.750  -0.0315   0.02682   0.01744  -0.0983   0.8188   0.0612
  -6.500  -0.0068   0.02578   0.01633  -0.0976   0.8115   0.0621
  -6.250   0.0164   0.02493   0.01539  -0.0966   0.8027   0.0632
  -6.000   0.0439   0.02408   0.01441  -0.0962   0.7956   0.0650
  -5.750   0.0653   0.02344   0.01364  -0.0947   0.7856   0.0671
  -5.500   0.0921   0.02267   0.01270  -0.0941   0.7776   0.0692
  -5.250   0.1138   0.02199   0.01205  -0.0927   0.7667   0.0709
  -5.000   0.1370   0.02138   0.01142  -0.0915   0.7567   0.0729
  -4.750   0.1617   0.02079   0.01076  -0.0906   0.7474   0.0753
  -4.500   0.1823   0.02029   0.01027  -0.0890   0.7359   0.0784
  -4.250   0.2053   0.01977   0.00979  -0.0878   0.7251   0.0823
  -3.750   0.2492   0.01889   0.00893  -0.0850   0.6994   0.0910
  -3.500   0.2720   0.01851   0.00857  -0.0837   0.6855   0.0979
  -3.250   0.2963   0.01815   0.00825  -0.0826   0.6709   0.1073
  -3.000   0.3215   0.01784   0.00798  -0.0817   0.6549   0.1248
  -2.750   0.3469   0.01756   0.00764  -0.0808   0.6373   0.1546
  -2.500   0.3714   0.01725   0.00733  -0.0798   0.6176   0.1876
  -2.250   0.3950   0.01701   0.00710  -0.0788   0.5955   0.2253
  -2.000   0.4178   0.01676   0.00696  -0.0777   0.5705   0.2876
  -1.750   0.4378   0.01628   0.00693  -0.0763   0.5415   0.4369
  -1.250   0.5680   0.01588   0.00713  -0.0899   0.4638   1.0000
  -1.000   0.5848   0.01618   0.00716  -0.0878   0.4482   1.0000
  -0.750   0.6030   0.01646   0.00723  -0.0861   0.4366   1.0000
  -0.500   0.6218   0.01677   0.00732  -0.0844   0.4274   1.0000
  -0.250   0.6418   0.01704   0.00744  -0.0829   0.4197   1.0000
   0.000   0.6620   0.01736   0.00756  -0.0815   0.4133   1.0000
   0.250   0.6833   0.01765   0.00771  -0.0803   0.4080   1.0000
   0.500   0.7050   0.01793   0.00789  -0.0792   0.4030   1.0000
   0.750   0.7270   0.01824   0.00807  -0.0782   0.3985   1.0000
   1.000   0.7498   0.01858   0.00826  -0.0773   0.3946   1.0000
   1.250   0.7730   0.01890   0.00848  -0.0766   0.3909   1.0000
   1.500   0.7960   0.01920   0.00874  -0.0758   0.3871   1.0000
   1.750   0.8193   0.01953   0.00900  -0.0751   0.3837   1.0000
   2.000   0.8432   0.01987   0.00927  -0.0745   0.3807   1.0000
   2.250   0.8676   0.02024   0.00956  -0.0740   0.3781   1.0000
   2.500   0.8932   0.02063   0.00986  -0.0738   0.3758   1.0000
   2.750   0.9188   0.02104   0.01020  -0.0735   0.3736   1.0000
   3.000   0.9420   0.02140   0.01059  -0.0729   0.3712   1.0000
   3.250   0.9655   0.02178   0.01099  -0.0723   0.3686   1.0000
   3.500   0.9890   0.02218   0.01140  -0.0718   0.3660   1.0000
   3.750   1.0125   0.02259   0.01180  -0.0713   0.3632   1.0000
   4.000   1.0364   0.02301   0.01219  -0.0709   0.3604   1.0000
   4.250   1.0612   0.02345   0.01260  -0.0706   0.3578   1.0000
   4.500   1.0875   0.02395   0.01303  -0.0707   0.3553   1.0000
   4.750   1.1078   0.02439   0.01357  -0.0697   0.3528   1.0000
   5.000   1.1286   0.02485   0.01413  -0.0688   0.3502   1.0000
   5.250   1.1496   0.02531   0.01466  -0.0680   0.3475   1.0000
   5.500   1.1708   0.02578   0.01517  -0.0673   0.3444   1.0000
   5.750   1.1926   0.02622   0.01563  -0.0666   0.3412   1.0000
   6.000   1.2165   0.02668   0.01605  -0.0663   0.3379   1.0000
   6.250   1.2365   0.02719   0.01661  -0.0654   0.3348   1.0000
   6.500   1.2500   0.02767   0.01726  -0.0635   0.3309   1.0000
   6.750   1.2649   0.02812   0.01780  -0.0617   0.3266   1.0000
   7.000   1.2828   0.02854   0.01825  -0.0605   0.3225   1.0000
   7.250   1.3041   0.02897   0.01868  -0.0599   0.3193   1.0000
   7.500   1.3238   0.02951   0.01927  -0.0591   0.3165   1.0000
   7.750   1.3332   0.03012   0.02007  -0.0566   0.3134   1.0000
   8.000   1.3415   0.03068   0.02078  -0.0540   0.3097   1.0000
   8.250   1.3523   0.03119   0.02137  -0.0518   0.3058   1.0000
   8.500   1.3671   0.03162   0.02184  -0.0502   0.3020   1.0000
   8.750   1.3839   0.03207   0.02229  -0.0491   0.2985   1.0000
   9.000   1.3821   0.03293   0.02339  -0.0454   0.2944   1.0000
   9.250   1.3858   0.03374   0.02435  -0.0428   0.2899   1.0000
   9.500   1.3947   0.03442   0.02513  -0.0409   0.2861   1.0000
   9.750   1.4078   0.03499   0.02575  -0.0395   0.2827   1.0000
  10.000   1.4105   0.03607   0.02700  -0.0373   0.2790   1.0000
  10.250   1.4088   0.03745   0.02860  -0.0348   0.2746   1.0000
  10.500   1.4111   0.03865   0.02995  -0.0329   0.2702   1.0000
  10.750   1.4183   0.03953   0.03089  -0.0314   0.2658   1.0000
  11.000   1.4118   0.04155   0.03315  -0.0293   0.2610   1.0000
  11.250   1.4053   0.04369   0.03549  -0.0275   0.2556   1.0000
  11.500   1.4063   0.04527   0.03717  -0.0262   0.2506   1.0000
  11.750   1.3901   0.04865   0.04081  -0.0247   0.2445   1.0000
  12.000   1.3755   0.05208   0.04442  -0.0236   0.2379   1.0000
  12.250   1.3464   0.05752   0.05009  -0.0231   0.2312   1.0000
  12.500   1.2884   0.06740   0.06020  -0.0242   0.2238   1.0000
  12.750   1.1788   0.08701   0.08001  -0.0294   0.2090   1.0000
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