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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 500,000
Max Cl/Cd: 81.62 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-500000.txt
Download as CSV file: xf-rhodesg34-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.1982   0.10382   0.10140  -0.0596   0.9603   0.0397
 -12.500  -0.1785   0.09949   0.09703  -0.0652   0.9514   0.0409
 -12.250  -0.1821   0.08917   0.08667  -0.0790   0.9433   0.0430
 -12.000  -0.1501   0.08581   0.08327  -0.0841   0.9353   0.0433
 -11.750  -0.1187   0.08291   0.08032  -0.0889   0.9268   0.0438
 -11.500  -0.0905   0.07927   0.07662  -0.0951   0.9162   0.0444
 -11.250  -0.0673   0.07553   0.07279  -0.1010   0.9033   0.0456
 -11.000  -0.1072   0.06260   0.05975  -0.1157   0.8833   0.0486
 -10.750  -0.0992   0.06060   0.05770  -0.1160   0.8739   0.0489
 -10.500  -0.0952   0.05855   0.05563  -0.1164   0.8659   0.0491
 -10.250  -0.1064   0.05532   0.05235  -0.1174   0.8569   0.0494
 -10.000  -0.2413   0.03300   0.02885  -0.1180   0.8459   0.0424
  -9.750  -0.2316   0.03060   0.02632  -0.1166   0.8403   0.0419
  -9.500  -0.2252   0.02767   0.02306  -0.1146   0.8347   0.0413
  -9.250  -0.2165   0.02505   0.02010  -0.1125   0.8296   0.0413
  -9.000  -0.2028   0.02306   0.01778  -0.1106   0.8243   0.0416
  -8.750  -0.1857   0.02133   0.01574  -0.1090   0.8192   0.0417
  -8.500  -0.1658   0.01997   0.01411  -0.1077   0.8143   0.0418
  -8.250  -0.1450   0.01883   0.01276  -0.1064   0.8090   0.0421
  -8.000  -0.1223   0.01798   0.01170  -0.1052   0.8033   0.0425
  -7.750  -0.0985   0.01711   0.01062  -0.1043   0.7977   0.0429
  -7.500  -0.0754   0.01604   0.00952  -0.1034   0.7919   0.0435
  -7.250  -0.0506   0.01547   0.00891  -0.1027   0.7854   0.0441
  -7.000  -0.0247   0.01509   0.00845  -0.1021   0.7797   0.0449
  -6.750   0.0002   0.01464   0.00800  -0.1013   0.7732   0.0458
  -6.500   0.0256   0.01419   0.00748  -0.1005   0.7663   0.0466
  -6.250   0.0512   0.01374   0.00693  -0.0998   0.7594   0.0474
  -6.000   0.0765   0.01336   0.00649  -0.0989   0.7504   0.0481
  -5.750   0.1012   0.01268   0.00578  -0.0981   0.7422   0.0492
  -5.500   0.1262   0.01230   0.00542  -0.0974   0.7319   0.0502
  -5.250   0.1515   0.01200   0.00511  -0.0966   0.7214   0.0515
  -5.000   0.1765   0.01174   0.00479  -0.0957   0.7084   0.0530
  -4.750   0.2017   0.01160   0.00456  -0.0949   0.6921   0.0545
  -4.500   0.2243   0.01117   0.00409  -0.0937   0.6732   0.0564
  -4.250   0.2477   0.01103   0.00387  -0.0925   0.6523   0.0584
  -4.000   0.2711   0.01096   0.00368  -0.0914   0.6319   0.0605
  -3.750   0.2933   0.01080   0.00343  -0.0901   0.6113   0.0630
  -3.500   0.3155   0.01075   0.00329  -0.0888   0.5883   0.0660
  -3.250   0.3378   0.01078   0.00320  -0.0875   0.5564   0.0693
  -3.000   0.3548   0.01085   0.00305  -0.0853   0.4954   0.0736
  -2.500   0.3898   0.01133   0.00305  -0.0812   0.4056   0.0847
  -2.250   0.4113   0.01133   0.00307  -0.0799   0.3911   0.1031
  -2.000   0.4337   0.01137   0.00319  -0.0788   0.3808   0.1563
  -1.750   0.4573   0.01140   0.00325  -0.0779   0.3736   0.1778
  -1.500   0.4810   0.01144   0.00330  -0.0771   0.3677   0.1948
  -1.250   0.5037   0.01149   0.00338  -0.0761   0.3623   0.2194
  -1.000   0.5260   0.01139   0.00346  -0.0751   0.3579   0.2837
  -0.750   0.5445   0.01088   0.00355  -0.0735   0.3542   0.4837
  -0.500   0.5542   0.01020   0.00369  -0.0697   0.3507   0.7479
  -0.250   0.6516   0.01032   0.00417  -0.0842   0.3440   0.9749
   0.000   0.7005   0.01060   0.00437  -0.0887   0.3404   0.9938
   0.250   0.7457   0.01076   0.00448  -0.0925   0.3376   1.0000
   0.500   0.7660   0.01087   0.00456  -0.0910   0.3351   1.0000
   0.750   0.7859   0.01101   0.00465  -0.0895   0.3321   1.0000
   1.000   0.8058   0.01118   0.00477  -0.0880   0.3298   1.0000
   1.250   0.8254   0.01138   0.00492  -0.0864   0.3275   1.0000
   1.500   0.8451   0.01163   0.00510  -0.0849   0.3252   1.0000
   1.750   0.8660   0.01182   0.00527  -0.0836   0.3236   1.0000
   2.000   0.8875   0.01195   0.00540  -0.0824   0.3223   1.0000
   2.250   0.9090   0.01208   0.00553  -0.0812   0.3206   1.0000
   2.500   0.9302   0.01222   0.00567  -0.0800   0.3184   1.0000
   2.750   0.9511   0.01236   0.00579  -0.0788   0.3157   1.0000
   3.000   0.9718   0.01252   0.00594  -0.0775   0.3133   1.0000
   3.250   0.9922   0.01273   0.00611  -0.0762   0.3111   1.0000
   3.500   1.0126   0.01299   0.00634  -0.0749   0.3087   1.0000
   3.750   1.0339   0.01327   0.00659  -0.0739   0.3064   1.0000
   4.000   1.0548   0.01340   0.00675  -0.0727   0.3052   1.0000
   4.250   1.0748   0.01355   0.00693  -0.0713   0.3037   1.0000
   4.500   1.0941   0.01371   0.00711  -0.0698   0.3021   1.0000
   4.750   1.1132   0.01387   0.00729  -0.0683   0.3002   1.0000
   5.000   1.1316   0.01403   0.00746  -0.0668   0.2977   1.0000
   5.250   1.1503   0.01422   0.00765  -0.0653   0.2954   1.0000
   5.500   1.1690   0.01446   0.00787  -0.0639   0.2928   1.0000
   5.750   1.1893   0.01481   0.00819  -0.0629   0.2898   1.0000
   6.000   1.2085   0.01495   0.00839  -0.0616   0.2883   1.0000
   6.250   1.2278   0.01512   0.00861  -0.0603   0.2861   1.0000
   6.500   1.2473   0.01531   0.00885  -0.0592   0.2837   1.0000
   6.750   1.2660   0.01551   0.00908  -0.0580   0.2806   1.0000
   7.000   1.2843   0.01577   0.00935  -0.0567   0.2777   1.0000
   7.250   1.3020   0.01612   0.00968  -0.0555   0.2746   1.0000
   7.500   1.3213   0.01637   0.01000  -0.0545   0.2719   1.0000
   7.750   1.3409   0.01660   0.01030  -0.0536   0.2685   1.0000
   8.000   1.3594   0.01687   0.01061  -0.0526   0.2641   1.0000
   8.250   1.3763   0.01725   0.01100  -0.0514   0.2601   1.0000
   8.500   1.3948   0.01759   0.01139  -0.0505   0.2550   1.0000
   8.750   1.4129   0.01795   0.01178  -0.0496   0.2479   1.0000
   9.000   1.4294   0.01842   0.01226  -0.0486   0.2412   1.0000
   9.500   1.4537   0.01992   0.01362  -0.0459   0.1979   1.0000
   9.750   1.4448   0.02209   0.01548  -0.0425   0.1566   1.0000
  10.000   1.4490   0.02352   0.01685  -0.0405   0.1437   1.0000
  10.250   1.4548   0.02490   0.01821  -0.0389   0.1346   1.0000
  10.500   1.4624   0.02617   0.01949  -0.0375   0.1278   1.0000
  10.750   1.4702   0.02746   0.02081  -0.0363   0.1223   1.0000
  11.000   1.4783   0.02876   0.02213  -0.0351   0.1166   1.0000
  11.250   1.4832   0.03034   0.02371  -0.0339   0.1097   1.0000
  11.500   1.4877   0.03199   0.02537  -0.0327   0.1024   1.0000
  11.750   1.4917   0.03375   0.02714  -0.0316   0.0915   1.0000
  12.000   1.4850   0.03649   0.02978  -0.0302   0.0705   1.0000
  12.250   1.4766   0.03956   0.03280  -0.0290   0.0635   1.0000
  12.500   1.4744   0.04223   0.03554  -0.0284   0.0615   1.0000
  12.750   1.4688   0.04537   0.03875  -0.0278   0.0597   1.0000
  13.000   1.4623   0.04877   0.04222  -0.0275   0.0582   1.0000
  13.250   1.4552   0.05237   0.04592  -0.0274   0.0570   1.0000
  13.500   1.4503   0.05581   0.04947  -0.0275   0.0564   1.0000
  13.750   1.4420   0.05977   0.05355  -0.0277   0.0557   1.0000
  14.000   1.4327   0.06397   0.05787  -0.0282   0.0551   1.0000
  14.250   1.4195   0.06880   0.06282  -0.0289   0.0544   1.0000
  14.500   1.4056   0.07386   0.06800  -0.0297   0.0539   1.0000
  14.750   1.3913   0.07909   0.07334  -0.0307   0.0534   1.0000
  15.000   1.3761   0.08447   0.07883  -0.0318   0.0528   1.0000
  15.250   1.3613   0.08981   0.08425  -0.0330   0.0522   1.0000
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