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Airfoil database list (S).

S4158 to S8037 (16%)

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(s4158-il) S4158

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S4158Selig S4158 low Reynolds number airfoil
Max thickness 10.9% at 35.3% chord
Max camber 3.7% at 44.7% chord
Source UIUC Airfoil Coordinates Database

(s4180-il) S4180-098-84

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S4180-098-84Selig S4180 low Reynolds number airfoil
Max thickness 9.8% at 26.1% chord
Max camber 4% at 39.4% chord
Source UIUC Airfoil Coordinates Database

(s4233-il) S4233-136-84

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S4233-136-84Selig S4233 low Reynolds number airfoil
Max thickness 13.6% at 34.9% chord
Max camber 2.7% at 48.8% chord
Source UIUC Airfoil Coordinates Database

(s4310-il) S4310

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S4310Selig S4310 low Reynolds number airfoil
Max thickness 10.9% at 30.7% chord
Max camber 4.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(s4320-il) S4320

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S4320Selig S4320 low Reynolds number airfoil
Max thickness 9.4% at 26.8% chord
Max camber 4.5% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(s5010-il) S5010

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S5010Selig S5010 low Reynolds number airfoil
Max thickness 9.8% at 27.6% chord
Max camber 1.8% at 32% chord
Source UIUC Airfoil Coordinates Database

(s5020-il) S5020

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S5020Selig S5020 low Reynolds number airfoil
Max thickness 8.4% at 27.8% chord
Max camber 2.2% at 27.8% chord
Source UIUC Airfoil Coordinates Database

(s6061-il) S6061 9%

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S6061 9%Selig S6061 low Reynolds number airfoil
Max thickness 9% at 34% chord
Max camber 1.5% at 43.6% chord
Source UIUC Airfoil Coordinates Database

(s6062-il) S6062 8%

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S6062 8%Selig S6062 low Reynolds number airfoil
Max thickness 7.9% at 29.4% chord
Max camber 1.4% at 43.7% chord
Source UIUC Airfoil Coordinates Database

(s6063-il) S6063 7.05%

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S6063 7.05%Selig S6063 low Reynolds number airfoil
Max thickness 7% at 29.4% chord
Max camber 1.3% at 43.8% chord
Source UIUC Airfoil Coordinates Database

(s7012-il) S7012 8.75%

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S7012 8.75%Selig S7012 low Reynolds number airfoil
Max thickness 8.7% at 27.7% chord
Max camber 1.7% at 38.1% chord
Source UIUC Airfoil Coordinates Database

(s7055-il) S7055 (10.5%) Flat-Bottomed

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S7055 (10.5%) Flat-BottomedSelig S7055 low Reynolds number airfoil
Max thickness 10.5% at 31.8% chord
Max camber 3.3% at 38.6% chord
Source UIUC Airfoil Coordinates Database

(s7075-il) S7075 (9%)

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S7075 (9%)Selig S7075 low Reynolds number airfoil
Max thickness 9% at 29% chord
Max camber 2.8% at 46.8% chord
Source UIUC Airfoil Coordinates Database

(s801-nr) NREL's S801 Airfoil

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NREL's S801 AirfoilNREL HAWT airfoil S801 primary 13.5% Not recommended
Max thickness 13.5% at 37.8% chord
Max camber 3.7% at 47.1% chord
Source NWTC National WInd Technology Center

(s802-nr) NREL's S802 Airfoil

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NREL's S802 AirfoilNREL HAWT airfoil S802 tip Not recommended
Max thickness 11.5% at 37.9% chord
Max camber 3.8% at 47.3% chord
Source NWTC National WInd Technology Center

(s8025-il) S8025 (8%)

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S8025 (8%)Selig S8025 low Reynolds number airfoil
Max thickness 8% at 22.9% chord
Max camber 0.4% at 18.8% chord
Source UIUC Airfoil Coordinates Database

(s803-nr) NREL's S803 Airfoil

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NREL's S803 AirfoilNREL HAWT airfoil S803 tip Not recommended
Max thickness 11.5% at 37.5% chord
Max camber 3.7% at 46.9% chord
Source NWTC National WInd Technology Center

(s8035-il) S8035 for RC aerobatic 14% thick

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S8035 for RC aerobatic  14% thickSelig S8035 low Reynolds number airfoil
Max thickness 14% at 29.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s8036-il) S8036 (16%)

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S8036 (16%)Selig S8036 low Reynolds number airfoil
Max thickness 16% at 36.8% chord
Max camber 1.3% at 40.4% chord
Source UIUC Airfoil Coordinates Database

(s8037-il) S8037 (16%)

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S8037 (16%)Selig S8037 low Reynolds number airfoil
Max thickness 16% at 33.5% chord
Max camber 1.9% at 40.4% chord
Source UIUC Airfoil Coordinates Database
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