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NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NREL's S807 Airfoil (s807-nr)
Reynolds number: 100,000
Max Cl/Cd: 33.39 at α=12.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s807-nr-100000.txt
Download as CSV file: xf-s807-nr-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S807 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6142   0.13768   0.13211  -0.0316   1.0000   0.0735
 -15.500  -0.5991   0.13732   0.13176  -0.0301   1.0000   0.0743
 -15.250  -0.8065   0.09474   0.08858  -0.0559   1.0000   0.0625
 -15.000  -0.8290   0.08883   0.08252  -0.0578   1.0000   0.0622
 -14.750  -0.8504   0.08345   0.07698  -0.0593   1.0000   0.0619
 -14.500  -0.8710   0.07851   0.07186  -0.0604   1.0000   0.0616
 -14.250  -0.8900   0.07398   0.06714  -0.0611   1.0000   0.0615
 -14.000  -0.9059   0.06993   0.06289  -0.0614   1.0000   0.0614
 -13.750  -0.9194   0.06621   0.05896  -0.0612   1.0000   0.0614
 -13.500  -0.9299   0.06285   0.05536  -0.0608   1.0000   0.0615
 -13.250  -0.9379   0.05978   0.05207  -0.0600   1.0000   0.0617
 -13.000  -0.9424   0.05705   0.04910  -0.0590   1.0000   0.0620
 -12.750  -0.9453   0.05458   0.04640  -0.0578   1.0000   0.0625
 -12.500  -0.9204   0.05226   0.04407  -0.0567   1.0000   0.0645
 -12.250  -0.9023   0.05070   0.04250  -0.0555   1.0000   0.0664
 -12.000  -0.8883   0.04917   0.04090  -0.0542   1.0000   0.0687
 -11.750  -0.8710   0.04772   0.03932  -0.0526   1.0000   0.0709
 -11.500  -0.8550   0.04641   0.03781  -0.0510   1.0000   0.0729
 -11.250  -0.8146   0.04631   0.03798  -0.0487   1.0000   0.0778
 -11.000  -0.7986   0.04545   0.03709  -0.0469   1.0000   0.0824
 -10.750  -0.7741   0.04533   0.03715  -0.0444   1.0000   0.0890
 -10.500  -0.7586   0.04478   0.03660  -0.0420   1.0000   0.0967
 -10.250  -0.7450   0.04447   0.03657  -0.0391   1.0000   0.1088
 -10.000  -0.7427   0.04341   0.03578  -0.0363   1.0000   0.1253
  -9.750  -0.7524   0.04151   0.03421  -0.0335   1.0000   0.1433
  -9.500  -0.7716   0.03901   0.03202  -0.0304   1.0000   0.1643
  -9.250  -0.7970   0.03634   0.02964  -0.0268   1.0000   0.1856
  -9.000  -0.8271   0.03382   0.02735  -0.0223   1.0000   0.2022
  -8.750  -0.8584   0.03077   0.02455  -0.0186   1.0000   0.2238
  -8.500  -0.8495   0.03222   0.02725  -0.0145   1.0000   0.3618
  -8.250  -0.8515   0.02940   0.02422  -0.0164   1.0000   0.3985
  -8.000  -0.8180   0.03266   0.02737  -0.0135   1.0000   0.4198
  -7.750  -0.7809   0.03682   0.03143  -0.0098   1.0000   0.4341
  -7.500  -0.7396   0.04201   0.03654  -0.0052   1.0000   0.4477
  -7.250  -0.6457   0.05155   0.04589   0.0005   1.0000   0.4496
  -7.000  -0.5431   0.05750   0.05156   0.0001   1.0000   0.4585
  -6.750  -0.5117   0.05845   0.05243   0.0018   1.0000   0.4696
  -6.500  -0.5389   0.05702   0.05105   0.0069   1.0000   0.4821
  -6.250  -0.4792   0.05862   0.05252   0.0065   1.0000   0.4923
  -6.000  -0.4488   0.05889   0.05273   0.0078   1.0000   0.5033
  -5.750  -0.5097   0.05664   0.05062   0.0153   1.0000   0.5146
  -5.500  -0.3462   0.06276   0.05648   0.0106   1.0000   0.5616
  -5.250  -0.3596   0.06092   0.05467   0.0135   1.0000   0.5621
  -5.000  -0.3745   0.05910   0.05287   0.0168   1.0000   0.5620
  -4.750  -0.4000   0.05735   0.05117   0.0214   1.0000   0.5624
  -4.500  -0.3266   0.06052   0.05432   0.0223   1.0000   0.6181
  -4.250  -0.2767   0.05867   0.05241   0.0200   1.0000   0.6245
  -4.000  -0.2987   0.05835   0.05218   0.0255   1.0000   0.6364
  -3.750  -0.2676   0.05711   0.05094   0.0252   1.0000   0.6435
  -3.500  -0.2793   0.05664   0.05055   0.0291   0.9988   0.6545
  -3.250  -0.2324   0.05577   0.04961   0.0219   0.9844   0.6690
  -3.000  -0.1475   0.05292   0.04668   0.0120   0.9760   0.6737
  -2.750  -0.1047   0.05160   0.04532   0.0061   0.9572   0.6866
  -2.500  -0.0329   0.04880   0.04250  -0.0017   0.9365   0.6914
  -2.250  -0.0085   0.04741   0.04112  -0.0029   0.8951   0.7038
  -2.000   0.1003   0.04372   0.03721  -0.0179   0.8266   0.7086
  -1.750   0.2106   0.04198   0.03446  -0.0365   0.6905   0.7201
  -1.500   0.2584   0.04071   0.03269  -0.0405   0.6306   0.7236
  -1.000   0.1664   0.03782   0.02962  -0.0313   0.6099   0.6510
  -0.750   0.1927   0.03718   0.02874  -0.0315   0.5867   0.6529
  -0.500   0.2136   0.03628   0.02768  -0.0319   0.5677   0.6461
  -0.250   0.2210   0.03505   0.02633  -0.0321   0.5541   0.6400
   0.000   0.2341   0.03411   0.02530  -0.0324   0.5409   0.6389
   0.250   0.2499   0.03295   0.02399  -0.0343   0.5300   0.6369
   0.500   0.2725   0.03240   0.02333  -0.0349   0.5190   0.6377
   0.750   0.2955   0.03208   0.02299  -0.0349   0.5089   0.6397
   1.000   0.3205   0.03171   0.02250  -0.0356   0.5005   0.6416
   1.250   0.3438   0.03122   0.02200  -0.0366   0.4918   0.6427
   1.500   0.3703   0.03079   0.02147  -0.0381   0.4840   0.6441
   1.750   0.3965   0.03042   0.02109  -0.0395   0.4765   0.6462
   2.000   0.4252   0.03002   0.02063  -0.0418   0.4693   0.6493
   2.250   0.4576   0.02977   0.02023  -0.0444   0.4637   0.6519
   2.500   0.4803   0.02971   0.02032  -0.0439   0.4576   0.6536
   2.750   0.5059   0.02971   0.02035  -0.0440   0.4520   0.6556
   3.000   0.5347   0.02979   0.02035  -0.0448   0.4471   0.6579
   3.250   0.5600   0.02984   0.02054  -0.0452   0.4415   0.6609
   3.500   0.5888   0.02988   0.02061  -0.0465   0.4361   0.6646
   3.750   0.6238   0.02991   0.02057  -0.0496   0.4316   0.6683
   4.000   0.6489   0.03021   0.02092  -0.0493   0.4279   0.6704
   4.250   0.6711   0.03052   0.02144  -0.0488   0.4235   0.6728
   4.500   0.6968   0.03080   0.02182  -0.0490   0.4188   0.6756
   4.750   0.7260   0.03107   0.02210  -0.0500   0.4146   0.6793
   5.000   0.7584   0.03155   0.02254  -0.0519   0.4110   0.6838
   5.250   0.7797   0.03210   0.02336  -0.0516   0.4071   0.6870
   5.500   0.8008   0.03265   0.02409  -0.0509   0.4029   0.6900
   5.750   0.8273   0.03307   0.02458  -0.0511   0.3988   0.6934
   6.000   0.8579   0.03358   0.02506  -0.0523   0.3953   0.6973
   6.250   0.8823   0.03451   0.02620  -0.0531   0.3913   0.7016
   6.500   0.8987   0.03536   0.02732  -0.0519   0.3867   0.7049
   6.750   0.9208   0.03599   0.02808  -0.0513   0.3825   0.7089
   7.000   0.9509   0.03646   0.02855  -0.0520   0.3787   0.7139
   7.250   0.9731   0.03765   0.02990  -0.0525   0.3742   0.7188
   7.500   0.9837   0.03887   0.03143  -0.0507   0.3689   0.7220
   7.750   1.0076   0.03939   0.03204  -0.0504   0.3642   0.7263
   8.000   1.0447   0.03956   0.03211  -0.0518   0.3600   0.7320
   8.250   1.0453   0.04168   0.03466  -0.0497   0.3540   0.7366
   8.500   1.0604   0.04253   0.03569  -0.0482   0.3484   0.7412
   8.750   1.1008   0.04214   0.03521  -0.0495   0.3438   0.7480
   9.000   1.0992   0.04452   0.03795  -0.0474   0.3374   0.7530
   9.250   1.1115   0.04543   0.03905  -0.0457   0.3312   0.7578
   9.500   1.1673   0.04388   0.03727  -0.0483   0.3259   0.7658
   9.750   1.1428   0.04738   0.04129  -0.0439   0.3186   0.7703
  10.000   1.1804   0.04624   0.04015  -0.0440   0.3121   0.7782
  10.250   1.2010   0.04681   0.04081  -0.0435   0.3056   0.7864
  10.500   1.1968   0.04837   0.04264  -0.0403   0.2983   0.7927
  10.750   1.2689   0.04504   0.03902  -0.0437   0.2915   0.8046
  11.000   1.2309   0.04873   0.04323  -0.0377   0.2842   0.8104
  11.250   1.3106   0.04426   0.03843  -0.0412   0.2763   0.8252
  11.500   1.2788   0.04748   0.04212  -0.0358   0.2692   0.8344
  11.750   1.3436   0.04351   0.03791  -0.0376   0.2606   0.8523
  12.000   1.3163   0.04582   0.04062  -0.0319   0.2541   0.8658
  12.250   1.3585   0.04281   0.03749  -0.0313   0.2455   0.8913
  12.500   1.3332   0.04403   0.03904  -0.0249   0.2402   0.9376
  12.750   1.3864   0.04152   0.03629  -0.0277   0.2282   1.0000
  13.000   1.3619   0.04439   0.03949  -0.0246   0.2204   1.0000
  13.250   1.3823   0.04401   0.03903  -0.0245   0.2099   1.0000
  13.500   1.4028   0.04347   0.03830  -0.0240   0.1989   1.0000
  13.750   1.3766   0.04705   0.04216  -0.0218   0.1916   1.0000
  14.000   1.3797   0.04834   0.04336  -0.0211   0.1821   1.0000
  14.250   1.3742   0.05070   0.04569  -0.0207   0.1732   1.0000
  14.500   1.3557   0.05502   0.05012  -0.0212   0.1661   1.0000
  14.750   1.3615   0.05679   0.05168  -0.0211   0.1566   1.0000
  15.000   1.3321   0.06329   0.05842  -0.0233   0.1516   1.0000
  15.250   1.3401   0.06513   0.06004  -0.0234   0.1426   1.0000
  15.500   1.3102   0.07247   0.06763  -0.0266   0.1385   1.0000
  15.750   0.8846   0.16162   0.15743  -0.0747   0.1409   1.0000
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