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Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 36 (rhodesg36-il)
Reynolds number: 500,000
Max Cl/Cd: 70.08 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg36-il-500000-n5.txt
Download as CSV file: xf-rhodesg36-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 36                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.5391   0.03790   0.03416  -0.1428   0.9423   0.0315
 -15.250  -0.5745   0.03369   0.02972  -0.1430   0.9336   0.0315
 -15.000  -0.5891   0.03169   0.02758  -0.1406   0.9258   0.0316
 -14.750  -0.5958   0.03023   0.02601  -0.1376   0.9176   0.0317
 -14.500  -0.6003   0.02903   0.02470  -0.1341   0.9092   0.0318
 -14.000  -0.5863   0.02682   0.02228  -0.1298   0.8874   0.0321
 -13.750  -0.5764   0.02580   0.02114  -0.1275   0.8752   0.0323
 -13.500  -0.5663   0.02477   0.01996  -0.1251   0.8630   0.0325
 -13.250  -0.5546   0.02379   0.01881  -0.1227   0.8513   0.0328
 -12.750  -0.5246   0.02198   0.01662  -0.1189   0.8299   0.0333
 -12.500  -0.5073   0.02116   0.01559  -0.1173   0.8198   0.0336
 -12.250  -0.4883   0.02039   0.01463  -0.1160   0.8098   0.0340
 -12.000  -0.4683   0.01969   0.01373  -0.1147   0.8007   0.0343
 -11.750  -0.4468   0.01903   0.01291  -0.1136   0.7916   0.0345
 -11.250  -0.4015   0.01800   0.01172  -0.1117   0.7758   0.0351
 -11.000  -0.3777   0.01762   0.01126  -0.1109   0.7668   0.0354
 -10.750  -0.3532   0.01726   0.01085  -0.1101   0.7585   0.0357
 -10.500  -0.3284   0.01694   0.01047  -0.1094   0.7496   0.0361
 -10.250  -0.3034   0.01661   0.01006  -0.1087   0.7417   0.0366
 -10.000  -0.2785   0.01625   0.00962  -0.1080   0.7319   0.0371
  -9.750  -0.2536   0.01588   0.00915  -0.1072   0.7218   0.0376
  -9.500  -0.2288   0.01550   0.00866  -0.1065   0.7109   0.0381
  -9.250  -0.2036   0.01514   0.00818  -0.1058   0.7002   0.0386
  -9.000  -0.1789   0.01480   0.00774  -0.1050   0.6892   0.0390
  -8.750  -0.1536   0.01451   0.00741  -0.1044   0.6782   0.0395
  -8.500  -0.1281   0.01430   0.00713  -0.1037   0.6681   0.0399
  -8.250  -0.1023   0.01409   0.00687  -0.1031   0.6592   0.0405
  -8.000  -0.0767   0.01390   0.00660  -0.1024   0.6511   0.0411
  -7.750  -0.0506   0.01368   0.00633  -0.1019   0.6430   0.0418
  -7.500  -0.0251   0.01349   0.00605  -0.1012   0.6342   0.0425
  -7.250   0.0009   0.01332   0.00579  -0.1006   0.6254   0.0433
  -7.000   0.0262   0.01313   0.00556  -0.1000   0.6161   0.0440
  -6.750   0.0522   0.01299   0.00539  -0.0994   0.6085   0.0448
  -6.500   0.0784   0.01285   0.00522  -0.0989   0.6000   0.0456
  -6.250   0.1038   0.01274   0.00504  -0.0982   0.5915   0.0464
  -6.000   0.1300   0.01259   0.00485  -0.0977   0.5815   0.0474
  -5.750   0.1552   0.01250   0.00467  -0.0970   0.5706   0.0483
  -5.500   0.1802   0.01235   0.00450  -0.0963   0.5558   0.0492
  -5.250   0.2041   0.01232   0.00439  -0.0953   0.5320   0.0502
  -5.000   0.2230   0.01252   0.00433  -0.0936   0.4730   0.0513
  -4.750   0.2401   0.01283   0.00436  -0.0916   0.4221   0.0524
  -4.500   0.2620   0.01294   0.00433  -0.0903   0.4012   0.0535
  -4.250   0.2844   0.01295   0.00427  -0.0892   0.3873   0.0546
  -4.000   0.3080   0.01294   0.00423  -0.0883   0.3777   0.0558
  -3.750   0.3313   0.01296   0.00420  -0.0874   0.3687   0.0571
  -3.500   0.3549   0.01298   0.00417  -0.0865   0.3618   0.0587
  -3.250   0.3787   0.01297   0.00413  -0.0856   0.3556   0.0603
  -3.000   0.4016   0.01296   0.00411  -0.0846   0.3496   0.0618
  -2.750   0.4244   0.01299   0.00411  -0.0836   0.3444   0.0635
  -2.500   0.4483   0.01299   0.00410  -0.0827   0.3406   0.0654
  -2.250   0.4714   0.01299   0.00408  -0.0817   0.3364   0.0675
  -2.000   0.4938   0.01301   0.00409  -0.0807   0.3322   0.0699
  -1.750   0.5154   0.01308   0.00411  -0.0794   0.3280   0.0723
  -1.500   0.5360   0.01310   0.00412  -0.0780   0.3245   0.0757
  -1.250   0.5571   0.01309   0.00413  -0.0767   0.3221   0.0802
  -1.000   0.5773   0.01304   0.00416  -0.0752   0.3197   0.0945
  -0.750   0.5977   0.01305   0.00429  -0.0739   0.3171   0.1393
  -0.500   0.6185   0.01315   0.00439  -0.0726   0.3144   0.1503
  -0.250   0.6390   0.01326   0.00450  -0.0713   0.3120   0.1575
   0.000   0.6597   0.01340   0.00463  -0.0700   0.3095   0.1635
   0.250   0.6801   0.01357   0.00479  -0.0687   0.3070   0.1688
   0.500   0.7018   0.01368   0.00492  -0.0677   0.3054   0.1759
   1.000   0.7458   0.01387   0.00521  -0.0657   0.3022   0.1985
   1.250   0.7659   0.01382   0.00541  -0.0646   0.3004   0.2882
   1.750   0.8820   0.01294   0.00629  -0.0782   0.2949   1.0000
   2.000   0.8996   0.01315   0.00646  -0.0765   0.2932   1.0000
   2.250   0.9172   0.01338   0.00666  -0.0748   0.2914   1.0000
   2.500   0.9348   0.01364   0.00688  -0.0731   0.2897   1.0000
   2.750   0.9528   0.01391   0.00712  -0.0716   0.2880   1.0000
   3.000   0.9731   0.01411   0.00731  -0.0705   0.2871   1.0000
   3.250   0.9933   0.01433   0.00753  -0.0694   0.2861   1.0000
   3.500   1.0134   0.01455   0.00776  -0.0683   0.2849   1.0000
   3.750   1.0336   0.01480   0.00800  -0.0672   0.2838   1.0000
   4.000   1.0538   0.01505   0.00825  -0.0662   0.2824   1.0000
   4.250   1.0737   0.01532   0.00852  -0.0652   0.2809   1.0000
   4.500   1.0933   0.01560   0.00880  -0.0642   0.2791   1.0000
   4.750   1.1127   0.01590   0.00909  -0.0632   0.2775   1.0000
   5.000   1.1314   0.01624   0.00940  -0.0621   0.2750   1.0000
   5.250   1.1484   0.01666   0.00978  -0.0608   0.2716   1.0000
   5.500   1.1682   0.01697   0.01010  -0.0600   0.2695   1.0000
   5.750   1.1888   0.01726   0.01042  -0.0593   0.2677   1.0000
   6.000   1.2086   0.01759   0.01077  -0.0585   0.2658   1.0000
   6.250   1.2281   0.01795   0.01114  -0.0577   0.2642   1.0000
   6.500   1.2474   0.01833   0.01154  -0.0570   0.2628   1.0000
   6.750   1.2662   0.01873   0.01196  -0.0562   0.2612   1.0000
   7.000   1.2847   0.01917   0.01240  -0.0554   0.2597   1.0000
   7.250   1.3029   0.01963   0.01286  -0.0546   0.2582   1.0000
   7.500   1.3201   0.02014   0.01338  -0.0538   0.2564   1.0000
   7.750   1.3369   0.02070   0.01394  -0.0529   0.2546   1.0000
   8.000   1.3561   0.02114   0.01442  -0.0524   0.2532   1.0000
   8.250   1.3751   0.02159   0.01493  -0.0518   0.2518   1.0000
   8.500   1.3937   0.02207   0.01545  -0.0513   0.2496   1.0000
   8.750   1.4114   0.02261   0.01603  -0.0507   0.2474   1.0000
   9.000   1.4283   0.02320   0.01664  -0.0501   0.2449   1.0000
   9.250   1.4446   0.02384   0.01731  -0.0494   0.2428   1.0000
   9.500   1.4599   0.02456   0.01804  -0.0487   0.2407   1.0000
   9.750   1.4751   0.02529   0.01879  -0.0481   0.2386   1.0000
  10.000   1.4929   0.02589   0.01945  -0.0477   0.2369   1.0000
  10.250   1.5098   0.02654   0.02016  -0.0472   0.2349   1.0000
  10.500   1.5262   0.02723   0.02091  -0.0468   0.2328   1.0000
  10.750   1.5412   0.02803   0.02175  -0.0463   0.2300   1.0000
  11.000   1.5541   0.02899   0.02273  -0.0457   0.2266   1.0000
  11.250   1.5666   0.02999   0.02375  -0.0450   0.2236   1.0000
  11.500   1.5817   0.03083   0.02465  -0.0447   0.2199   1.0000
  11.750   1.5955   0.03177   0.02564  -0.0442   0.2162   1.0000
  12.000   1.6045   0.03311   0.02700  -0.0436   0.2109   1.0000
  12.250   1.6159   0.03428   0.02821  -0.0431   0.2049   1.0000
  12.750   1.6274   0.03764   0.03157  -0.0418   0.1870   1.0000
  13.000   1.6267   0.03995   0.03386  -0.0409   0.1744   1.0000
  13.250   1.6099   0.04385   0.03765  -0.0395   0.1516   1.0000
  13.500   1.5845   0.04875   0.04246  -0.0380   0.1307   1.0000
  13.750   1.5701   0.05278   0.04651  -0.0373   0.1208   1.0000
  14.000   1.5558   0.05695   0.05071  -0.0368   0.1133   1.0000
  14.250   1.5467   0.06068   0.05451  -0.0366   0.1085   1.0000
  14.500   1.5348   0.06487   0.05876  -0.0366   0.1041   1.0000
  14.750   1.5207   0.06945   0.06343  -0.0367   0.1004   1.0000
  15.000   1.5071   0.07413   0.06821  -0.0371   0.0960   1.0000
  15.250   1.4843   0.08018   0.07435  -0.0378   0.0914   1.0000
  15.500   1.4684   0.08545   0.07974  -0.0386   0.0874   1.0000
  15.750   1.4407   0.09247   0.08685  -0.0398   0.0802   1.0000
  16.000   1.4099   0.10005   0.09450  -0.0413   0.0724   1.0000
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