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Airfoil database list (S).

S8038 (13%) to NREL's S817 Airfoil

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(s8038-il) S8038 (13%)

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S8038 (13%)Selig S8038 (13%) low Reynolds number airfoil
Max thickness 13% at 32.9% chord
Max camber 0.6% at 40.1% chord
Source UIUC Airfoil Coordinates Database

(s804-nr) NREL's S804 Airfoil

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NREL's S804 AirfoilNREL HAWT airfoil S804 root Not recommended
Max thickness 17.9% at 26.7% chord
Max camber 4.2% at 39.6% chord
Source NWTC National WInd Technology Center

(s8052-il) S8052 (11.88%)

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S8052 (11.88%)Selig S8052 low Reynolds number airfoil
Max thickness 11.9% at 33.3% chord
Max camber 1.2% at 44.2% chord
Source UIUC Airfoil Coordinates Database

(s8055-il) S8055 (12%)

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S8055 (12%)Selig S8055 (12%) low Reynolds number airfoil
Max thickness 12% at 33.9% chord
Max camber 1.6% at 44.7% chord
Source UIUC Airfoil Coordinates Database

(s805a-nr) NREL's S805A Airfoil

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NREL's S805A AirfoilNREL HAWT airfoil S805A primary
Max thickness 13.5% at 40% chord
Max camber 2.1% at 35% chord
Source NWTC National WInd Technology Center

(s8064-il) S8064

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S8064Selig airfoil for Q-500 (Q500) pylon racing (12.33%). Used on the Great Planes Viper 500 ARF.
Max thickness 12.3% at 37.8% chord
Max camber 1.1% at 56.2% chord
Source UIUC Airfoil Coordinates Database

(s8065-il) S8065 (11% version of S8064)

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S8065 (11% version of S8064)Selig airfoil for Q-40 pylon racing (11%).
Max thickness 11% at 37.8% chord
Max camber 1.1% at 56.3% chord
Source UIUC Airfoil Coordinates Database

(s8066-il) S8066 (10% version of S8065 w/ lower surface aerodynamically similar)

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S8066 (10% version of S8065 w/ lower surface aerodynamically similar)Selig airfoil for Q-40 pylon racing (10%).
Max thickness 10% at 37.7% chord
Max camber 0.8% at 56.3% chord
Source UIUC Airfoil Coordinates Database

(s806a-nr) NREL's S806A Airfoil (modified line 35)

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NREL's S806A Airfoil (modified line 35)NREL HAWT airfoil S806A tip
Max thickness 11.5% at 45% chord
Max camber 2.8% at 45% chord
Source NWTC National WInd Technology Center

(s807-nr) NREL's S807 Airfoil

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NREL's S807 AirfoilNREL 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

(s808-nr) NREL's S808 Airfoil

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NREL's S808 AirfoilNREL HAWT airfoil S808 root
Max thickness 21% at 24.4% chord
Max camber 2.4% at 72.9% chord
Source NWTC National WInd Technology Center

(s809-nr) NREL's S809 Airfoil

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NREL's S809 AirfoilNREL HAWT airfoil S809 primary 21.0% Re=2.0E+6 Clmax(S)=1.00 Restrained max lift coef
Max thickness 21% at 39.5% chord
Max camber 1% at 82.3% chord
Source NWTC National WInd Technology Center

(s810-nr) NREL's S810 Airfoil

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NREL's S810 AirfoilNREL 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

(s811-nr) NREL's S811 Airfoil

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NREL's S811 AirfoilNREL HAWT airfoil S811 root
Max thickness 26.3% at 27.4% chord
Max camber 1.7% at 76.4% chord
Source NWTC National WInd Technology Center

(s812-nr) NREL's S812 Airfoil

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NREL's S812 AirfoilNREL HAWT airfoil S812 primary
Max thickness 21% at 39.6% chord
Max camber 1.6% at 77% chord
Source NWTC National WInd Technology Center

(s813-nr) NREL's S813 Airfoil

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NREL's S813 AirfoilNREL HAWT airfoil S813 tip
Max thickness 16% at 40.4% chord
Max camber 2.3% at 54.4% chord
Source NWTC National WInd Technology Center

(s814-nr) NREL's S814 Airfoil

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NREL's S814 AirfoilNREL HAWT airfoil S814 root 24.0% Dia=20 to 30 m Re=1.5E+6 Clmax(S)=1.56 Clmax(R)=1.51 High max lift coef
Max thickness 24.1% at 28.4% chord
Max camber 3% at 74.5% chord
Source NWTC National WInd Technology Center

(s815-nr) NREL's S815 Airfoil

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NREL's S815 AirfoilNREL HAWT airfoil S815 root 26.0% Dia=20 to 30 m Re=1.2E+6 Clmax(S)=1.46 Clmax(R)=1.40 High max lift coef
Max thickness 26.2% at 25.7% chord
Max camber 2.9% at 77.9% chord
Source NWTC National WInd Technology Center

(s816-nr) NREL's S816 Airfoil

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NREL's S816 AirfoilNREL HAWT airfoil S816 primary 21.0% Dia=30 to 50 m Re=4.0E+6 Clmax(S)=1.20 Clmax(R)=1.17 Restrained max lift coef
Max thickness 21% at 39% chord
Max camber 1.8% at 67.6% chord
Source NWTC National WInd Technology Center

(s817-nr) NREL's S817 Airfoil

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NREL's S817 AirfoilNREL HAWT airfoil S817 tip 16.0% Dia=30 to 50 m Re=3.0E+6 Clmax(S)=1.10 Clmax(R)=1.08 Restrained max lift coef
Max thickness 16% at 51.1% chord
Max camber 2.8% at 41.1% chord
Source NWTC National WInd Technology Center
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