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NREL's S810 Airfoil (s810-nr)

NREL's S810 Airfoil - NREL HAWT airfoil S810 tip


Airfoil s810-nr
Details Dat file Parser  
(s810-nr) NREL's S810 Airfoil
NREL HAWT airfoil S810 tip
Max thickness 18% at 44.2% chord.
Max camber 0.9% at 10.9% chord
Source NWTC National WInd Technology Center
Source dat file
The dat file is in Selig format
NREL's S810 Airfoil
   x/c	    y/c
1.00000	 0.00000
0.99626	 0.00044
0.98531	 0.00205
0.96786	 0.00522
0.94473	 0.00994
0.91657	 0.01593
0.88380	 0.02289
0.84676	 0.03078
0.80612	 0.03971
0.76278	 0.04960
0.71769	 0.06015
0.67191	 0.07091
0.62652	 0.08079
0.58155	 0.08816
0.53586	 0.09249
0.48909	 0.09466
0.44186	 0.09515
0.39470	 0.09415
0.34815	 0.09179
0.30273	 0.08820
0.25895	 0.08349
0.21727	 0.07777
0.17816	 0.07118
0.14205	 0.06384
0.10934	 0.05589
0.08038	 0.04747
0.05550	 0.03874
0.03497	 0.02989
0.01903	 0.02110
0.00786	 0.01261
0.00163	 0.00470
0.00000	 0.00000
0.00031	-0.00183
0.00573	-0.00687
0.01878	-0.01197
0.03790	-0.01805
0.06237	-0.02507
0.09136	-0.03299
0.12403	-0.04145
0.15989	-0.04991
0.19860	-0.05809
0.23960	-0.06584
0.28221	-0.07277
0.32604	-0.07833
0.37090	-0.08224
0.41642	-0.08442
0.46207	-0.08459
0.50762	-0.08229
0.55310	-0.07728
0.59877	-0.06938
0.64530	-0.05915
0.69265	-0.04792
0.74000	-0.03683
0.78635	-0.02660
0.83065	-0.01778
0.87180	-0.01070
0.90873	-0.00550
0.94044	-0.00213
0.96603	-0.00036
0.98478	 0.00022
0.99618	 0.00013
1.00000	 0.00000
Dat file parser warnings
  • Line 2 - Invalid characters : x/c y/c
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Polars for NREL's S810 Airfoil (s810-nr)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s810-nr50,000920.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s810-nr50,000516.5 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s810-nr100,000924.9 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s810-nr100,000527.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   s810-nr200,000950 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s810-nr200,000552.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s810-nr500,000983.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s810-nr500,000577.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s810-nr1,000,0009105.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s810-nr1,000,000592.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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