Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.64 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-1000000-n5.txt
Download as CSV file: xf-rhodesg34-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.4110   0.17882   0.17688  -0.0211   1.0000   0.0138
 -19.250  -0.4024   0.17639   0.17445  -0.0223   1.0000   0.0140
 -16.750  -0.8722   0.03375   0.03065  -0.1255   0.9515   0.0234
 -16.500  -0.8274   0.02952   0.02613  -0.1380   0.9310   0.0235
 -16.250  -0.7985   0.02739   0.02367  -0.1430   0.8847   0.0237
 -16.000  -0.8021   0.02622   0.02228  -0.1399   0.8589   0.0238
 -15.750  -0.8058   0.02514   0.02103  -0.1361   0.8467   0.0238
 -15.500  -0.8038   0.02433   0.02010  -0.1327   0.8384   0.0240
 -15.250  -0.7953   0.02348   0.01912  -0.1303   0.8324   0.0241
 -15.000  -0.7843   0.02261   0.01815  -0.1281   0.8278   0.0242
 -14.750  -0.7712   0.02179   0.01722  -0.1262   0.8237   0.0243
 -14.500  -0.7557   0.02110   0.01642  -0.1244   0.8201   0.0244
 -14.250  -0.7386   0.02047   0.01569  -0.1228   0.8166   0.0246
 -14.000  -0.7208   0.01981   0.01493  -0.1213   0.8136   0.0248
 -13.750  -0.7023   0.01916   0.01420  -0.1199   0.8097   0.0249
 -13.500  -0.6828   0.01857   0.01351  -0.1185   0.8058   0.0250
 -13.250  -0.6630   0.01803   0.01286  -0.1171   0.8007   0.0251
 -13.000  -0.6424   0.01750   0.01223  -0.1159   0.7971   0.0252
 -12.750  -0.6206   0.01698   0.01164  -0.1148   0.7947   0.0253
 -12.500  -0.5983   0.01650   0.01109  -0.1137   0.7918   0.0254
 -12.250  -0.5770   0.01591   0.01043  -0.1125   0.7883   0.0255
 -12.000  -0.5555   0.01536   0.00981  -0.1113   0.7843   0.0257
 -11.750  -0.5330   0.01489   0.00927  -0.1102   0.7809   0.0259
 -11.500  -0.5094   0.01447   0.00880  -0.1093   0.7781   0.0261
 -11.250  -0.4851   0.01409   0.00839  -0.1085   0.7751   0.0263
 -11.000  -0.4606   0.01374   0.00800  -0.1076   0.7713   0.0265
 -10.750  -0.4359   0.01342   0.00764  -0.1068   0.7675   0.0267
 -10.500  -0.4110   0.01312   0.00729  -0.1060   0.7637   0.0270
 -10.250  -0.3858   0.01281   0.00695  -0.1053   0.7596   0.0272
 -10.000  -0.3605   0.01252   0.00661  -0.1046   0.7530   0.0274
  -9.750  -0.3355   0.01224   0.00628  -0.1038   0.7469   0.0276
  -9.500  -0.3098   0.01197   0.00596  -0.1031   0.7414   0.0279
  -9.250  -0.2842   0.01171   0.00566  -0.1024   0.7335   0.0282
  -9.000  -0.2587   0.01147   0.00536  -0.1016   0.7255   0.0284
  -8.750  -0.2332   0.01125   0.00508  -0.1009   0.7140   0.0287
  -8.500  -0.2082   0.01107   0.00482  -0.1000   0.6967   0.0289
  -8.250  -0.1836   0.01095   0.00459  -0.0991   0.6747   0.0291
  -8.000  -0.1599   0.01075   0.00429  -0.0980   0.6534   0.0296
  -7.750  -0.1358   0.01064   0.00408  -0.0970   0.6324   0.0300
  -7.500  -0.1113   0.01054   0.00390  -0.0961   0.6136   0.0304
  -7.250  -0.0860   0.01044   0.00373  -0.0954   0.5996   0.0308
  -7.000  -0.0606   0.01035   0.00358  -0.0946   0.5864   0.0312
  -6.750  -0.0350   0.01026   0.00343  -0.0939   0.5717   0.0317
  -6.500  -0.0097   0.01020   0.00329  -0.0932   0.5534   0.0322
  -6.250   0.0150   0.01018   0.00316  -0.0923   0.5270   0.0327
  -6.000   0.0343   0.01048   0.00312  -0.0905   0.4478   0.0331
  -5.750   0.0567   0.01059   0.00306  -0.0893   0.4065   0.0336
  -5.500   0.0809   0.01061   0.00299  -0.0884   0.3835   0.0344
  -5.250   0.1059   0.01061   0.00292  -0.0877   0.3680   0.0352
  -4.750   0.1573   0.01058   0.00279  -0.0864   0.3480   0.0372
  -4.500   0.1830   0.01055   0.00273  -0.0858   0.3405   0.0384
  -4.250   0.2090   0.01052   0.00268  -0.0852   0.3347   0.0399
  -4.000   0.2353   0.01048   0.00264  -0.0847   0.3305   0.0414
  -3.750   0.2614   0.01046   0.00259  -0.0842   0.3260   0.0429
  -3.500   0.2872   0.01045   0.00256  -0.0837   0.3214   0.0449
  -3.250   0.3131   0.01045   0.00255  -0.0831   0.3165   0.0471
  -3.000   0.3395   0.01042   0.00252  -0.0827   0.3137   0.0492
  -2.750   0.3654   0.01041   0.00251  -0.0822   0.3097   0.0519
  -2.500   0.3915   0.01042   0.00250  -0.0817   0.3068   0.0545
  -2.250   0.4172   0.01042   0.00250  -0.0811   0.3042   0.0579
  -2.000   0.4430   0.01043   0.00251  -0.0806   0.3014   0.0608
  -1.750   0.4687   0.01044   0.00252  -0.0801   0.2987   0.0647
  -1.500   0.4949   0.01043   0.00252  -0.0797   0.2973   0.0688
  -1.250   0.5207   0.01041   0.00252  -0.0792   0.2954   0.0755
  -1.000   0.5454   0.01030   0.00256  -0.0786   0.2938   0.1223
  -0.750   0.5710   0.01031   0.00261  -0.0781   0.2922   0.1409
  -0.500   0.5966   0.01034   0.00266  -0.0776   0.2903   0.1489
  -0.250   0.6221   0.01038   0.00271  -0.0771   0.2886   0.1549
   0.000   0.6474   0.01044   0.00276  -0.0765   0.2867   0.1598
   0.250   0.6724   0.01049   0.00282  -0.0760   0.2849   0.1654
   0.500   0.6971   0.01056   0.00290  -0.0754   0.2828   0.1714
   0.750   0.7218   0.01060   0.00297  -0.0747   0.2813   0.1819
   1.000   0.7465   0.01058   0.00304  -0.0742   0.2804   0.2093
   1.250   0.7667   0.01019   0.00315  -0.0729   0.2784   0.4098
   1.500   0.7719   0.00927   0.00332  -0.0684   0.2765   0.8010
   1.750   0.8778   0.00932   0.00370  -0.0855   0.2715   0.9876
   2.000   0.9112   0.00949   0.00383  -0.0869   0.2690   0.9966
   2.250   0.9485   0.00968   0.00397  -0.0892   0.2651   0.9999
   2.500   0.9713   0.00978   0.00406  -0.0882   0.2633   1.0000
   2.750   0.9925   0.00989   0.00416  -0.0870   0.2613   1.0000
   3.000   1.0136   0.01000   0.00427  -0.0857   0.2591   1.0000
   3.250   1.0342   0.01014   0.00438  -0.0844   0.2557   1.0000
   3.500   1.0541   0.01030   0.00451  -0.0830   0.2516   1.0000
   3.750   1.0747   0.01045   0.00464  -0.0817   0.2487   1.0000
   4.000   1.0955   0.01059   0.00478  -0.0805   0.2450   1.0000
   4.250   1.1152   0.01076   0.00492  -0.0790   0.2397   1.0000
   4.500   1.1318   0.01096   0.00508  -0.0770   0.2326   1.0000
   4.750   1.1467   0.01122   0.00527  -0.0747   0.2211   1.0000
   5.000   1.1377   0.01242   0.00607  -0.0683   0.1543   1.0000
   5.250   1.1454   0.01314   0.00665  -0.0650   0.1304   1.0000
   5.500   1.1619   0.01351   0.00699  -0.0633   0.1234   1.0000
   5.750   1.1785   0.01390   0.00735  -0.0617   0.1178   1.0000
   6.000   1.1968   0.01422   0.00767  -0.0604   0.1144   1.0000
   6.250   1.2150   0.01457   0.00801  -0.0591   0.1115   1.0000
   6.500   1.2323   0.01497   0.00840  -0.0578   0.1080   1.0000
   6.750   1.2498   0.01538   0.00880  -0.0565   0.1042   1.0000
   7.000   1.2682   0.01576   0.00918  -0.0555   0.1014   1.0000
   7.250   1.2853   0.01623   0.00964  -0.0543   0.0973   1.0000
   7.500   1.3015   0.01675   0.01014  -0.0530   0.0925   1.0000
   7.750   1.3085   0.01783   0.01105  -0.0508   0.0626   1.0000
   8.000   1.3192   0.01874   0.01193  -0.0490   0.0542   1.0000
   8.250   1.3341   0.01942   0.01262  -0.0479   0.0521   1.0000
   8.500   1.3483   0.02015   0.01337  -0.0467   0.0505   1.0000
   8.750   1.3625   0.02091   0.01415  -0.0456   0.0491   1.0000
   9.000   1.3777   0.02162   0.01489  -0.0447   0.0483   1.0000
   9.250   1.3926   0.02236   0.01567  -0.0438   0.0477   1.0000
   9.500   1.4067   0.02316   0.01650  -0.0429   0.0471   1.0000
   9.750   1.4202   0.02403   0.01741  -0.0420   0.0465   1.0000
  10.000   1.4328   0.02497   0.01838  -0.0411   0.0458   1.0000
  10.250   1.4448   0.02597   0.01942  -0.0401   0.0452   1.0000
  10.500   1.4549   0.02712   0.02061  -0.0391   0.0445   1.0000
  10.750   1.4640   0.02838   0.02190  -0.0381   0.0436   1.0000
  11.000   1.4723   0.02973   0.02329  -0.0371   0.0428   1.0000
  11.250   1.4829   0.03091   0.02453  -0.0364   0.0424   1.0000
  11.500   1.4937   0.03212   0.02578  -0.0357   0.0418   1.0000
  11.750   1.5025   0.03351   0.02723  -0.0350   0.0412   1.0000
  12.000   1.5102   0.03506   0.02883  -0.0344   0.0407   1.0000
  12.250   1.5171   0.03671   0.03053  -0.0338   0.0400   1.0000
  12.500   1.5225   0.03855   0.03242  -0.0332   0.0394   1.0000
  12.750   1.5270   0.04056   0.03449  -0.0327   0.0389   1.0000
  13.000   1.5301   0.04279   0.03678  -0.0324   0.0385   1.0000
  13.250   1.5310   0.04532   0.03938  -0.0321   0.0379   1.0000
  13.500   1.5330   0.04779   0.04192  -0.0319   0.0374   1.0000
  13.750   1.5349   0.05034   0.04454  -0.0319   0.0371   1.0000
  14.000   1.5359   0.05304   0.04732  -0.0319   0.0368   1.0000
  14.250   1.5357   0.05592   0.05028  -0.0321   0.0363   1.0000
  14.500   1.5334   0.05909   0.05353  -0.0323   0.0360   1.0000
  14.750   1.5291   0.06259   0.05713  -0.0326   0.0355   1.0000
  15.000   1.5241   0.06626   0.06087  -0.0331   0.0350   1.0000
  15.250   1.5166   0.07031   0.06501  -0.0336   0.0348   1.0000
  15.500   1.5069   0.07476   0.06956  -0.0344   0.0345   1.0000
  15.750   1.4963   0.07940   0.07429  -0.0353   0.0339   1.0000
  16.000   1.4852   0.08416   0.07915  -0.0363   0.0336   1.0000
  16.250   1.4727   0.08911   0.08418  -0.0374   0.0331   1.0000
<< Back to Rhode St. Genese 34 (rhodesg34-il)

Polar data table (+)

Polar graphs


<< Back to Rhode St. Genese 34 (rhodesg34-il)