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NREL's S833 Airfoil (s833-nr) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NREL's S833 Airfoil (s833-nr)
Reynolds number: 100,000
Max Cl/Cd: 36.8 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s833-nr-100000-n5.txt
Download as CSV file: xf-s833-nr-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S833 Airfoil                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8155   0.10535   0.09926  -0.0654   1.0000   0.0939
 -16.500  -0.8691   0.09347   0.08714  -0.0704   1.0000   0.0961
 -16.250  -0.9022   0.08566   0.07909  -0.0732   1.0000   0.0981
 -16.000  -0.8995   0.08382   0.07731  -0.0729   1.0000   0.1008
 -15.750  -0.9051   0.08071   0.07417  -0.0733   1.0000   0.1034
 -15.500  -0.9190   0.07644   0.06980  -0.0741   1.0000   0.1062
 -15.250  -0.9359   0.07190   0.06509  -0.0748   1.0000   0.1090
 -15.000  -0.9497   0.06797   0.06102  -0.0752   1.0000   0.1117
 -14.750  -0.9500   0.06605   0.05915  -0.0745   1.0000   0.1146
 -14.500  -0.9568   0.06336   0.05641  -0.0741   1.0000   0.1176
 -14.250  -0.9668   0.06039   0.05332  -0.0737   1.0000   0.1207
 -14.000  -0.9791   0.05731   0.05007  -0.0730   1.0000   0.1239
 -13.750  -0.9816   0.05550   0.04829  -0.0718   1.0000   0.1270
 -13.500  -0.9875   0.05348   0.04625  -0.0706   1.0000   0.1303
 -13.250  -0.9951   0.05134   0.04402  -0.0692   1.0000   0.1338
 -13.000  -1.0038   0.04918   0.04171  -0.0676   1.0000   0.1373
 -12.750  -1.0085   0.04754   0.04007  -0.0657   1.0000   0.1407
 -12.500  -1.0142   0.04596   0.03849  -0.0636   1.0000   0.1442
 -12.250  -1.0215   0.04433   0.03679  -0.0614   1.0000   0.1480
 -12.000  -1.0293   0.04272   0.03505  -0.0589   1.0000   0.1519
 -11.750  -1.0346   0.04143   0.03377  -0.0562   1.0000   0.1554
 -11.500  -1.0416   0.04017   0.03250  -0.0533   1.0000   0.1590
 -11.250  -1.0406   0.03884   0.03107  -0.0521   0.9982   0.1640
 -11.000  -1.0286   0.03763   0.02976  -0.0526   0.9943   0.1700
 -10.750  -1.0198   0.03656   0.02865  -0.0524   0.9902   0.1755
 -10.500  -1.0114   0.03552   0.02745  -0.0520   0.9853   0.1818
 -10.250  -0.9961   0.03467   0.02659  -0.0526   0.9816   0.1880
 -10.000  -0.9865   0.03369   0.02552  -0.0517   0.9765   0.1946
  -9.750  -0.9697   0.03289   0.02465  -0.0519   0.9726   0.2016
  -9.500  -0.9474   0.03221   0.02388  -0.0529   0.9696   0.2099
  -9.250  -0.9346   0.03144   0.02304  -0.0517   0.9644   0.2166
  -9.000  -0.9151   0.03081   0.02237  -0.0518   0.9605   0.2246
  -8.750  -0.8910   0.03024   0.02173  -0.0526   0.9576   0.2333
  -8.500  -0.8720   0.02967   0.02110  -0.0523   0.9536   0.2417
  -8.250  -0.8527   0.02912   0.02050  -0.0519   0.9491   0.2499
  -8.000  -0.8283   0.02865   0.01996  -0.0524   0.9459   0.2596
  -7.750  -0.8007   0.02825   0.01954  -0.0535   0.9435   0.2687
  -7.500  -0.7816   0.02778   0.01895  -0.0529   0.9390   0.2785
  -7.250  -0.7594   0.02739   0.01860  -0.0527   0.9348   0.2873
  -7.000  -0.7324   0.02703   0.01817  -0.0535   0.9318   0.2975
  -6.750  -0.7022   0.02673   0.01783  -0.0548   0.9295   0.3084
  -6.500  -0.6823   0.02640   0.01750  -0.0540   0.9249   0.3176
  -6.250  -0.6581   0.02609   0.01710  -0.0541   0.9207   0.3285
  -6.000  -0.6297   0.02585   0.01689  -0.0549   0.9178   0.3389
  -5.750  -0.5980   0.02563   0.01664  -0.0563   0.9154   0.3501
  -5.500  -0.5766   0.02539   0.01633  -0.0558   0.9108   0.3611
  -5.250  -0.5523   0.02520   0.01619  -0.0556   0.9065   0.3711
  -5.000  -0.5223   0.02501   0.01599  -0.0566   0.9035   0.3828
  -4.750  -0.4895   0.02483   0.01575  -0.0581   0.9011   0.3956
  -4.500  -0.4679   0.02472   0.01569  -0.0574   0.8964   0.4056
  -4.250  -0.4429   0.02459   0.01556  -0.0573   0.8919   0.4167
  -4.000  -0.4121   0.02446   0.01539  -0.0584   0.8888   0.4296
  -3.750  -0.3795   0.02437   0.01534  -0.0596   0.8864   0.4412
  -3.500  -0.3569   0.02433   0.01532  -0.0590   0.8816   0.4521
  -3.250  -0.3319   0.02426   0.01525  -0.0589   0.8767   0.4643
  -3.000  -0.3015   0.02422   0.01525  -0.0596   0.8735   0.4759
  -2.750  -0.2683   0.02417   0.01523  -0.0608   0.8712   0.4879
  -2.500  -0.2458   0.02420   0.01527  -0.0602   0.8659   0.4993
  -2.250  -0.2211   0.02424   0.01535  -0.0599   0.8609   0.5107
  -2.000  -0.1902   0.02426   0.01540  -0.0606   0.8576   0.5220
  -1.750  -0.1564   0.02422   0.01539  -0.0618   0.8552   0.5341
  -1.500  -0.1363   0.02437   0.01556  -0.0608   0.8491   0.5451
  -1.250  -0.1106   0.02448   0.01573  -0.0605   0.8442   0.5550
  -1.000  -0.0781   0.02447   0.01573  -0.0614   0.8410   0.5666
  -0.750  -0.0443   0.02449   0.01579  -0.0625   0.8387   0.5771
  -0.500  -0.0284   0.02477   0.01611  -0.0606   0.8307   0.5861
  -0.250   0.0020   0.02480   0.01615  -0.0612   0.8265   0.5973
   0.000   0.0343   0.02483   0.01625  -0.0617   0.8236   0.6054
   0.500   0.0823   0.02514   0.01664  -0.0606   0.8114   0.6233
   0.750   0.1168   0.02505   0.01655  -0.0618   0.8081   0.6334
   1.000   0.1516   0.02495   0.01652  -0.0626   0.8057   0.6410
   1.250   0.1669   0.02528   0.01687  -0.0609   0.7956   0.6501
   1.500   0.1988   0.02519   0.01685  -0.0612   0.7918   0.6569
   1.750   0.2375   0.02489   0.01657  -0.0630   0.7894   0.6666
   2.000   0.2498   0.02530   0.01707  -0.0603   0.7786   0.6722
   2.250   0.2857   0.02501   0.01681  -0.0614   0.7750   0.6809
   2.500   0.3170   0.02480   0.01668  -0.0616   0.7706   0.6873
   2.750   0.3361   0.02497   0.01692  -0.0600   0.7608   0.6940
   3.000   0.3749   0.02449   0.01649  -0.0616   0.7574   0.7020
   3.250   0.3912   0.02470   0.01680  -0.0594   0.7468   0.7074
   3.500   0.4278   0.02425   0.01640  -0.0604   0.7418   0.7150
   3.750   0.4504   0.02424   0.01648  -0.0593   0.7321   0.7210
   4.000   0.4827   0.02383   0.01616  -0.0594   0.7253   0.7268
   4.250   0.5087   0.02376   0.01615  -0.0591   0.7146   0.7346
   4.500   0.5428   0.02323   0.01573  -0.0593   0.7072   0.7394
   4.750   0.5626   0.02326   0.01585  -0.0576   0.6940   0.7453
   5.000   0.5923   0.02304   0.01569  -0.0579   0.6815   0.7525
   5.250   0.6204   0.02270   0.01544  -0.0571   0.6689   0.7570
   5.500   0.6500   0.02240   0.01521  -0.0568   0.6541   0.7627
   5.750   0.6790   0.02224   0.01510  -0.0569   0.6358   0.7695
   6.000   0.7025   0.02210   0.01503  -0.0555   0.6159   0.7739
   6.250   0.7310   0.02191   0.01485  -0.0551   0.5927   0.7794
   6.500   0.7607   0.02185   0.01475  -0.0553   0.5643   0.7857
   6.750   0.7830   0.02187   0.01473  -0.0538   0.5330   0.7902
   7.000   0.8041   0.02206   0.01482  -0.0524   0.4979   0.7954
   7.250   0.8250   0.02242   0.01502  -0.0513   0.4594   0.8015
   7.500   0.8392   0.02290   0.01537  -0.0489   0.4231   0.8062
   7.750   0.8516   0.02350   0.01583  -0.0465   0.3883   0.8114
   8.000   0.8652   0.02422   0.01640  -0.0446   0.3544   0.8173
   8.250   0.8761   0.02496   0.01703  -0.0423   0.3231   0.8221
   8.500   0.8865   0.02574   0.01771  -0.0399   0.2940   0.8274
   8.750   0.8982   0.02664   0.01849  -0.0380   0.2664   0.8331
   9.000   0.9094   0.02749   0.01927  -0.0360   0.2403   0.8380
   9.250   0.9190   0.02841   0.02011  -0.0339   0.2175   0.8432
   9.500   0.9315   0.02937   0.02102  -0.0323   0.1946   0.8489
   9.750   0.9419   0.03036   0.02196  -0.0305   0.1745   0.8541
  10.000   0.9517   0.03140   0.02295  -0.0286   0.1567   0.8596
  10.250   0.9628   0.03255   0.02405  -0.0272   0.1401   0.8655
  10.500   0.9720   0.03365   0.02514  -0.0254   0.1255   0.8711
  10.750   0.9820   0.03481   0.02630  -0.0238   0.1125   0.8772
  11.000   0.9920   0.03605   0.02757  -0.0225   0.1008   0.8835
  11.250   1.0000   0.03729   0.02885  -0.0207   0.0910   0.8902
  11.750   1.0143   0.04010   0.03172  -0.0176   0.0753   0.9053
  12.000   1.0214   0.04156   0.03326  -0.0161   0.0689   0.9144
  12.250   1.0257   0.04319   0.03492  -0.0146   0.0639   0.9258
  12.750   1.0360   0.04643   0.03836  -0.0125   0.0550   1.0000
  13.000   1.0455   0.04851   0.04056  -0.0124   0.0506   1.0000
  13.250   1.0526   0.05080   0.04289  -0.0124   0.0475   1.0000
  13.500   1.0598   0.05317   0.04534  -0.0123   0.0444   1.0000
  13.750   1.0664   0.05560   0.04786  -0.0124   0.0418   1.0000
  14.000   1.0700   0.05833   0.05060  -0.0126   0.0398   1.0000
  14.250   1.0768   0.06089   0.05334  -0.0127   0.0374   1.0000
  14.500   1.0812   0.06370   0.05625  -0.0131   0.0356   1.0000
  14.750   1.0838   0.06671   0.05931  -0.0135   0.0342   1.0000
  15.000   1.0872   0.06978   0.06252  -0.0140   0.0327   1.0000
  15.250   1.0897   0.07303   0.06594  -0.0146   0.0312   1.0000
  15.500   1.0905   0.07647   0.06949  -0.0155   0.0300   1.0000
  15.750   1.0909   0.08001   0.07308  -0.0166   0.0291   1.0000
  16.000   1.0911   0.08371   0.07690  -0.0177   0.0283   1.0000
  16.250   1.0897   0.08781   0.08123  -0.0189   0.0275   1.0000
  16.500   1.0868   0.09219   0.08580  -0.0206   0.0267   1.0000
  16.750   1.0821   0.09690   0.09068  -0.0226   0.0259   1.0000
  17.000   1.0778   0.10164   0.09556  -0.0248   0.0254   1.0000
  17.250   1.0735   0.10645   0.10048  -0.0273   0.0249   1.0000
  17.500   1.0710   0.11095   0.10505  -0.0298   0.0244   1.0000
  17.750   1.0631   0.11667   0.11093  -0.0330   0.0240   1.0000
  18.000   1.0474   0.12419   0.11874  -0.0375   0.0237   1.0000
  18.250   1.0302   0.13235   0.12715  -0.0428   0.0235   1.0000
  18.500   1.0080   0.14205   0.13709  -0.0493   0.0234   1.0000
  18.750   0.9792   0.15398   0.14927  -0.0573   0.0236   1.0000
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