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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 200,000
Max Cl/Cd: 58.84 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-200000.txt
Download as CSV file: xf-rhodesg34-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.1734   0.09201   0.08846  -0.0656   0.9708   0.0725
 -10.750  -0.1571   0.08846   0.08491  -0.0694   0.9659   0.0745
 -10.500  -0.1754   0.07950   0.07596  -0.0889   0.9559   0.0788
 -10.250  -0.1410   0.07735   0.07380  -0.0864   0.9549   0.0797
 -10.000  -0.1193   0.07506   0.07150  -0.0868   0.9490   0.0808
  -9.750  -0.0971   0.07180   0.06823  -0.0907   0.9438   0.0830
  -9.500  -0.1271   0.06184   0.05805  -0.1094   0.9275   0.0890
  -9.250  -0.0916   0.06033   0.05663  -0.1084   0.9246   0.0902
  -9.000  -0.0711   0.05882   0.05511  -0.1079   0.9174   0.0921
  -8.750  -0.0831   0.05254   0.04846  -0.1151   0.9061   0.1002
  -8.500  -0.0660   0.05107   0.04707  -0.1133   0.8972   0.1012
  -8.250  -0.0438   0.04939   0.04537  -0.1133   0.8906   0.1034
  -8.000  -0.0497   0.04603   0.04164  -0.1136   0.8798   0.1123
  -7.750  -0.0268   0.04429   0.03996  -0.1131   0.8733   0.1139
  -7.500  -0.0098   0.04287   0.03850  -0.1121   0.8657   0.1172
  -7.250  -0.0331   0.02949   0.02347  -0.1092   0.8560   0.0767
  -7.000  -0.0145   0.02703   0.02071  -0.1079   0.8492   0.0748
  -6.750  -0.0011   0.02409   0.01702  -0.1052   0.8405   0.0710
  -6.500   0.0255   0.02269   0.01524  -0.1045   0.8347   0.0706
  -6.250   0.0461   0.02163   0.01404  -0.1029   0.8257   0.0709
  -6.000   0.0728   0.02056   0.01281  -0.1023   0.8183   0.0717
  -5.750   0.0967   0.01981   0.01201  -0.1012   0.8094   0.0733
  -5.500   0.1228   0.01907   0.01115  -0.1004   0.8012   0.0753
  -5.250   0.1483   0.01841   0.01035  -0.0994   0.7933   0.0769
  -5.000   0.1736   0.01783   0.00964  -0.0984   0.7847   0.0782
  -4.750   0.2003   0.01686   0.00867  -0.0978   0.7775   0.0803
  -4.500   0.2234   0.01627   0.00814  -0.0966   0.7677   0.0830
  -4.250   0.2499   0.01576   0.00758  -0.0959   0.7598   0.0870
  -4.000   0.2722   0.01516   0.00703  -0.0945   0.7491   0.0907
  -3.750   0.2961   0.01467   0.00658  -0.0933   0.7389   0.0956
  -3.500   0.3204   0.01419   0.00612  -0.0922   0.7277   0.1022
  -3.250   0.3433   0.01386   0.00584  -0.0909   0.7133   0.1120
  -3.000   0.3671   0.01353   0.00559  -0.0896   0.6972   0.1277
  -2.750   0.3905   0.01315   0.00527  -0.0883   0.6783   0.1637
  -2.500   0.4120   0.01272   0.00493  -0.0868   0.6549   0.2160
  -2.250   0.4325   0.01244   0.00471  -0.0851   0.6256   0.2742
  -2.000   0.4477   0.01200   0.00462  -0.0826   0.5908   0.4167
  -1.750   0.4548   0.01111   0.00479  -0.0778   0.5517   0.7719
  -1.500   0.5662   0.01181   0.00509  -0.0941   0.4726   0.9859
  -1.250   0.6100   0.01228   0.00518  -0.0976   0.4500   1.0000
  -1.000   0.6276   0.01256   0.00528  -0.0957   0.4387   1.0000
  -0.750   0.6455   0.01289   0.00540  -0.0939   0.4304   1.0000
  -0.500   0.6656   0.01312   0.00553  -0.0924   0.4233   1.0000
  -0.250   0.6859   0.01341   0.00567  -0.0910   0.4175   1.0000
   0.000   0.7075   0.01375   0.00584  -0.0899   0.4126   1.0000
   0.250   0.7295   0.01398   0.00602  -0.0888   0.4082   1.0000
   0.500   0.7517   0.01423   0.00620  -0.0877   0.4040   1.0000
   0.750   0.7743   0.01453   0.00639  -0.0868   0.3999   1.0000
   1.000   0.7988   0.01494   0.00663  -0.0863   0.3958   1.0000
   1.250   0.8210   0.01517   0.00685  -0.0853   0.3923   1.0000
   1.500   0.8440   0.01542   0.00709  -0.0844   0.3891   1.0000
   1.750   0.8672   0.01570   0.00733  -0.0837   0.3857   1.0000
   2.000   0.8909   0.01601   0.00757  -0.0830   0.3824   1.0000
   2.250   0.9161   0.01639   0.00786  -0.0827   0.3795   1.0000
   2.500   0.9423   0.01682   0.00822  -0.0826   0.3770   1.0000
   2.750   0.9652   0.01710   0.00853  -0.0818   0.3749   1.0000
   3.000   0.9889   0.01740   0.00886  -0.0811   0.3729   1.0000
   3.250   1.0129   0.01773   0.00921  -0.0806   0.3709   1.0000
   3.500   1.0370   0.01806   0.00955  -0.0801   0.3686   1.0000
   3.750   1.0611   0.01840   0.00988  -0.0797   0.3661   1.0000
   4.000   1.0859   0.01877   0.01019  -0.0793   0.3628   1.0000
   4.250   1.1140   0.01937   0.01070  -0.0798   0.3596   1.0000
   4.500   1.1333   0.01959   0.01102  -0.0784   0.3570   1.0000
   4.750   1.1543   0.01988   0.01139  -0.0774   0.3541   1.0000
   5.000   1.1758   0.02018   0.01173  -0.0765   0.3508   1.0000
   5.250   1.1987   0.02049   0.01203  -0.0759   0.3475   1.0000
   5.500   1.2237   0.02087   0.01238  -0.0757   0.3445   1.0000
   5.750   1.2501   0.02144   0.01292  -0.0759   0.3414   1.0000
   6.000   1.2674   0.02169   0.01330  -0.0743   0.3387   1.0000
   6.250   1.2869   0.02201   0.01372  -0.0732   0.3358   1.0000
   6.500   1.3074   0.02233   0.01411  -0.0723   0.3329   1.0000
   6.750   1.3290   0.02264   0.01443  -0.0715   0.3296   1.0000
   7.000   1.3534   0.02300   0.01477  -0.0713   0.3267   1.0000
   7.250   1.3784   0.02355   0.01532  -0.0714   0.3235   1.0000
   7.500   1.3921   0.02383   0.01577  -0.0693   0.3208   1.0000
   7.750   1.4063   0.02409   0.01615  -0.0673   0.3169   1.0000
   8.000   1.4232   0.02432   0.01644  -0.0658   0.3130   1.0000
   8.250   1.4442   0.02460   0.01671  -0.0651   0.3097   1.0000
   8.500   1.4660   0.02503   0.01714  -0.0646   0.3060   1.0000
   8.750   1.4710   0.02530   0.01760  -0.0611   0.3024   1.0000
   9.000   1.4783   0.02556   0.01797  -0.0580   0.2984   1.0000
   9.250   1.4895   0.02578   0.01824  -0.0556   0.2945   1.0000
   9.500   1.5069   0.02603   0.01844  -0.0544   0.2905   1.0000
   9.750   1.5092   0.02648   0.01908  -0.0508   0.2868   1.0000
  10.000   1.5135   0.02695   0.01970  -0.0478   0.2825   1.0000
  10.250   1.5206   0.02734   0.02018  -0.0454   0.2780   1.0000
  10.500   1.5331   0.02771   0.02050  -0.0438   0.2737   1.0000
  10.750   1.5322   0.02854   0.02158  -0.0407   0.2687   1.0000
  11.000   1.5356   0.02928   0.02246  -0.0384   0.2630   1.0000
  11.250   1.5411   0.03000   0.02321  -0.0364   0.2575   1.0000
  11.500   1.5422   0.03113   0.02456  -0.0344   0.2491   1.0000
  11.750   1.5449   0.03224   0.02576  -0.0326   0.2409   1.0000
  12.000   1.5464   0.03359   0.02721  -0.0309   0.2299   1.0000
  12.250   1.5459   0.03522   0.02891  -0.0294   0.2127   1.0000
  12.500   1.5369   0.03756   0.03117  -0.0275   0.1908   1.0000
  12.750   1.5197   0.04090   0.03440  -0.0257   0.1739   1.0000
  13.000   1.5014   0.04475   0.03818  -0.0244   0.1621   1.0000
  13.250   1.4856   0.04872   0.04216  -0.0236   0.1531   1.0000
  13.500   1.4700   0.05293   0.04642  -0.0232   0.1457   1.0000
  13.750   1.4521   0.05767   0.05119  -0.0231   0.1390   1.0000
  14.000   1.4374   0.06225   0.05585  -0.0233   0.1329   1.0000
  14.250   1.4184   0.06756   0.06121  -0.0239   0.1267   1.0000
  14.500   1.4021   0.07275   0.06648  -0.0248   0.1211   1.0000
  14.750   1.3852   0.07821   0.07201  -0.0259   0.1152   1.0000
  15.000   1.3692   0.08364   0.07748  -0.0271   0.1098   1.0000
  15.250   1.3554   0.08895   0.08286  -0.0285   0.1036   1.0000
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