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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.64 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-1000000.txt
Download as CSV file: xf-rhodesg34-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4910   0.03433   0.03144  -0.1375   0.8824   0.0285
 -13.500  -0.5308   0.03125   0.02802  -0.1320   0.8625   0.0286
 -13.250  -0.5502   0.02845   0.02486  -0.1280   0.8518   0.0287
 -13.000  -0.5521   0.02643   0.02259  -0.1251   0.8451   0.0288
 -12.750  -0.5467   0.02478   0.02071  -0.1227   0.8401   0.0289
 -12.500  -0.5341   0.02368   0.01940  -0.1208   0.8359   0.0291
 -12.250  -0.5190   0.02269   0.01825  -0.1192   0.8321   0.0292
 -12.000  -0.5146   0.02011   0.01538  -0.1166   0.8284   0.0295
 -11.750  -0.4966   0.01910   0.01427  -0.1152   0.8249   0.0298
 -11.500  -0.4760   0.01842   0.01351  -0.1140   0.8212   0.0300
 -11.250  -0.4543   0.01782   0.01282  -0.1130   0.8172   0.0302
 -11.000  -0.4318   0.01732   0.01227  -0.1120   0.8134   0.0305
 -10.750  -0.4090   0.01679   0.01168  -0.1110   0.8100   0.0308
 -10.500  -0.3858   0.01629   0.01110  -0.1100   0.8065   0.0311
 -10.250  -0.3621   0.01586   0.01060  -0.1091   0.8027   0.0314
 -10.000  -0.3381   0.01542   0.01006  -0.1083   0.7985   0.0318
  -9.750  -0.3143   0.01488   0.00946  -0.1074   0.7952   0.0321
  -9.500  -0.2901   0.01437   0.00887  -0.1065   0.7916   0.0324
  -9.250  -0.2656   0.01391   0.00834  -0.1057   0.7872   0.0327
  -9.000  -0.2406   0.01354   0.00789  -0.1049   0.7826   0.0330
  -8.750  -0.2151   0.01323   0.00751  -0.1042   0.7781   0.0332
  -8.500  -0.1920   0.01242   0.00664  -0.1032   0.7736   0.0337
  -8.250  -0.1676   0.01192   0.00612  -0.1024   0.7684   0.0342
  -8.000  -0.1421   0.01163   0.00579  -0.1017   0.7632   0.0346
  -7.750  -0.1161   0.01136   0.00551  -0.1011   0.7579   0.0351
  -7.500  -0.0901   0.01109   0.00523  -0.1005   0.7512   0.0356
  -7.250  -0.0645   0.01085   0.00493  -0.0997   0.7445   0.0361
  -7.000  -0.0382   0.01060   0.00466  -0.0992   0.7371   0.0367
  -6.750  -0.0125   0.01040   0.00440  -0.0984   0.7270   0.0373
  -6.500   0.0138   0.01025   0.00420  -0.0978   0.7137   0.0377
  -6.250   0.0370   0.00985   0.00373  -0.0967   0.6960   0.0387
  -6.000   0.0609   0.00972   0.00351  -0.0957   0.6729   0.0395
  -5.750   0.0852   0.00965   0.00335  -0.0947   0.6513   0.0403
  -5.500   0.1097   0.00960   0.00321  -0.0938   0.6321   0.0412
  -5.250   0.1347   0.00955   0.00308  -0.0930   0.6160   0.0421
  -5.000   0.1597   0.00950   0.00295  -0.0922   0.6006   0.0429
  -4.750   0.1840   0.00936   0.00276  -0.0913   0.5840   0.0445
  -4.500   0.2089   0.00935   0.00268  -0.0905   0.5632   0.0459
  -4.250   0.2325   0.00943   0.00263  -0.0895   0.5290   0.0475
  -4.000   0.2506   0.00974   0.00261  -0.0875   0.4527   0.0491
  -3.750   0.2707   0.00998   0.00264  -0.0859   0.4044   0.0513
  -3.500   0.2942   0.01010   0.00265  -0.0849   0.3814   0.0534
  -3.250   0.3186   0.01011   0.00260  -0.0841   0.3676   0.0560
  -3.000   0.3434   0.01013   0.00258  -0.0833   0.3575   0.0590
  -2.750   0.3690   0.01015   0.00257  -0.0827   0.3507   0.0617
  -2.500   0.3935   0.01013   0.00253  -0.0820   0.3440   0.0665
  -2.250   0.4192   0.01013   0.00251  -0.0814   0.3395   0.0709
  -2.000   0.4445   0.01008   0.00247  -0.0808   0.3350   0.0775
  -1.750   0.4684   0.00997   0.00248  -0.0800   0.3305   0.1178
  -1.500   0.4929   0.01000   0.00257  -0.0793   0.3260   0.1498
  -1.250   0.5185   0.01002   0.00261  -0.0788   0.3231   0.1622
  -1.000   0.5446   0.01004   0.00264  -0.0783   0.3207   0.1696
  -0.750   0.5701   0.01004   0.00267  -0.0778   0.3183   0.1807
  -0.500   0.5952   0.01006   0.00272  -0.0772   0.3158   0.1942
  -0.250   0.6194   0.01004   0.00278  -0.0765   0.3136   0.2271
   0.000   0.6404   0.00979   0.00288  -0.0753   0.3111   0.3645
   0.250   0.6571   0.00937   0.00302  -0.0733   0.3083   0.5789
   0.500   0.6684   0.00888   0.00316  -0.0699   0.3064   0.7936
   0.750   0.7625   0.00883   0.00349  -0.0841   0.3043   0.9782
   1.000   0.8134   0.00902   0.00365  -0.0891   0.3025   0.9948
   1.250   0.8671   0.00917   0.00375  -0.0948   0.2997   1.0000
   1.500   0.8875   0.00928   0.00383  -0.0934   0.2975   1.0000
   1.750   0.9077   0.00940   0.00392  -0.0919   0.2952   1.0000
   2.000   0.9274   0.00955   0.00404  -0.0903   0.2930   1.0000
   2.250   0.9461   0.00974   0.00420  -0.0886   0.2898   1.0000
   2.500   0.9683   0.00981   0.00427  -0.0875   0.2888   1.0000
   2.750   0.9901   0.00990   0.00436  -0.0864   0.2876   1.0000
   3.000   1.0117   0.00999   0.00447  -0.0853   0.2862   1.0000
   3.250   1.0333   0.01010   0.00457  -0.0841   0.2848   1.0000
   3.500   1.0546   0.01021   0.00468  -0.0829   0.2831   1.0000
   3.750   1.0757   0.01034   0.00481  -0.0817   0.2813   1.0000
   4.000   1.0964   0.01049   0.00494  -0.0805   0.2791   1.0000
   4.250   1.1162   0.01067   0.00510  -0.0790   0.2766   1.0000
   4.500   1.1341   0.01086   0.00527  -0.0773   0.2733   1.0000
   4.750   1.1548   0.01093   0.00537  -0.0760   0.2717   1.0000
   5.000   1.1748   0.01104   0.00549  -0.0746   0.2697   1.0000
   5.250   1.1946   0.01116   0.00563  -0.0733   0.2676   1.0000
   5.500   1.2140   0.01131   0.00578  -0.0719   0.2648   1.0000
   5.750   1.2330   0.01150   0.00595  -0.0704   0.2614   1.0000
   6.000   1.2512   0.01173   0.00617  -0.0689   0.2580   1.0000
   6.250   1.2731   0.01185   0.00633  -0.0681   0.2553   1.0000
   6.500   1.2938   0.01202   0.00650  -0.0671   0.2498   1.0000
   6.750   1.3120   0.01230   0.00673  -0.0657   0.2432   1.0000
   7.000   1.3324   0.01251   0.00695  -0.0648   0.2358   1.0000
   7.250   1.3494   0.01288   0.00726  -0.0633   0.2222   1.0000
   7.500   1.3427   0.01443   0.00838  -0.0585   0.1600   1.0000
   7.750   1.3487   0.01546   0.00928  -0.0557   0.1381   1.0000
   8.000   1.3623   0.01612   0.00991  -0.0541   0.1292   1.0000
   8.250   1.3769   0.01676   0.01053  -0.0527   0.1224   1.0000
   8.500   1.3911   0.01744   0.01118  -0.0514   0.1161   1.0000
   8.750   1.4060   0.01810   0.01183  -0.0502   0.1105   1.0000
   9.000   1.4210   0.01876   0.01249  -0.0491   0.1054   1.0000
   9.250   1.4347   0.01953   0.01324  -0.0479   0.0990   1.0000
   9.500   1.4464   0.02044   0.01410  -0.0466   0.0882   1.0000
   9.750   1.4447   0.02225   0.01573  -0.0440   0.0610   1.0000
  10.000   1.4538   0.02340   0.01689  -0.0427   0.0567   1.0000
  10.250   1.4638   0.02451   0.01804  -0.0415   0.0549   1.0000
  10.500   1.4710   0.02585   0.01941  -0.0401   0.0529   1.0000
  10.750   1.4778   0.02724   0.02083  -0.0388   0.0511   1.0000
  11.000   1.4872   0.02848   0.02212  -0.0378   0.0500   1.0000
  11.250   1.4969   0.02972   0.02342  -0.0369   0.0494   1.0000
  11.500   1.5053   0.03108   0.02484  -0.0361   0.0488   1.0000
  11.750   1.5122   0.03261   0.02643  -0.0352   0.0481   1.0000
  12.000   1.5175   0.03433   0.02821  -0.0343   0.0472   1.0000
  12.250   1.5207   0.03629   0.03024  -0.0335   0.0465   1.0000
  12.500   1.5224   0.03847   0.03248  -0.0328   0.0458   1.0000
  12.750   1.5208   0.04110   0.03519  -0.0321   0.0450   1.0000
  13.000   1.5165   0.04413   0.03832  -0.0316   0.0443   1.0000
  13.250   1.5195   0.04647   0.04074  -0.0314   0.0439   1.0000
  13.500   1.5228   0.04884   0.04317  -0.0313   0.0435   1.0000
  13.750   1.5232   0.05160   0.04602  -0.0313   0.0430   1.0000
  14.000   1.5224   0.05455   0.04905  -0.0314   0.0426   1.0000
  14.250   1.5186   0.05790   0.05249  -0.0316   0.0420   1.0000
  14.500   1.5134   0.06150   0.05619  -0.0319   0.0416   1.0000
  14.750   1.5058   0.06552   0.06029  -0.0324   0.0412   1.0000
  15.000   1.4977   0.06967   0.06453  -0.0330   0.0408   1.0000
  15.250   1.4861   0.07439   0.06934  -0.0338   0.0402   1.0000
  15.500   1.4724   0.07950   0.07455  -0.0348   0.0398   1.0000
  15.750   1.4568   0.08492   0.08008  -0.0359   0.0394   1.0000
  16.000   1.4419   0.09025   0.08550  -0.0370   0.0392   1.0000
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