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NREL's S807 Airfoil (s807-nr)

NREL's S807 Airfoil - NREL HAWT airfoil S807 root


Airfoil s807-nr
Details Dat file Parser  
(s807-nr) NREL's S807 Airfoil
NREL HAWT airfoil S807 root
Max thickness 18% at 28.7% chord.
Max camber 1.9% at 78.3% chord
Source NWTC National WInd Technology Center
Source dat file
The dat file is in Selig format
NREL's S807 Airfoil
   x/c       y/c
1.00000   0.00000
0.99646   0.00082
0.98629   0.00351
0.97045   0.00810
0.94987   0.01410
0.92503   0.02067
0.89590   0.02712
0.86227   0.03329
0.82433   0.03941
0.78256   0.04554
0.73751   0.05167
0.68974   0.05777
0.63986   0.06376
0.58850   0.06958
0.53634   0.07514
0.48405   0.08033
0.43231   0.08503
0.38181   0.08909
0.33324   0.09233
0.28733   0.09444
0.24461   0.09497
0.20533   0.09343
0.16944   0.08940
0.13650   0.08294
0.10642   0.07466
0.07953   0.06509
0.05614   0.05453
0.03650   0.04332
0.02084   0.03177
0.00939   0.02024
0.00237   0.00909
0.00000   0.00000
0.00003  -0.00105
0.00364  -0.01032
0.01334  -0.01969
0.02802  -0.02928
0.04736  -0.03877
0.07102  -0.04800
0.09863  -0.05674
0.12982  -0.06479
0.16418  -0.07192
0.20129  -0.07791
0.24069  -0.08252
0.28191  -0.08547
0.32444  -0.08628
0.36824  -0.08429
0.41366  -0.07933
0.46091  -0.07162
0.51026  -0.06166
0.56158  -0.05048
0.61419  -0.03902
0.66725  -0.02798
0.71982  -0.01798
0.77085  -0.00950
0.81926  -0.00289
0.86392   0.00170
0.90376   0.00427
0.93778   0.00500
0.96509   0.00420
0.98477   0.00238
0.99628   0.00066
1.00000   0.00000
Dat file parser warnings
  • Line 2 - Invalid characters : x/c y/c
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Polars for NREL's S807 Airfoil (s807-nr)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s807-nr50,000920.3 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s807-nr50,000522 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s807-nr100,000933.4 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s807-nr100,000540.3 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s807-nr200,000956.4 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s807-nr200,000559.4 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s807-nr500,000984.9 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s807-nr500,000583.9 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s807-nr1,000,0009106.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s807-nr1,000,0005101.7 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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