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Airfoil database search (Symmetrical)

Search the 1636 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

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(s1014-il) S1014

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S1014Selig S1014 HPV airfoil
Max thickness 16.5% at 42.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1016-il) S1016

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S1016Selig S1016 HPV airfoil
Max thickness 17.5% at 41.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1046-il) S1046 17% (Danny Howell)

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S1046 17% (Danny Howell)Selig S1046 airfoil
Max thickness 17% at 30.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1048-il) S1048 14% (Danny Howell)

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S1048 14% (Danny Howell)Selig S1048 airfoil
Max thickness 14% at 27% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(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

(s9026-il) S9026 (9.5%)

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S9026 (9.5%)Selig S9026 (9.5%) symmetrical horizontal stab airfoil used on the Opus R/C sailplane
Max thickness 9.5% at 27.3% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9027-il) S9027 (8%)

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S9027 (8%)Selig S9027 (8%) symmetrical vertical stab airfoil used on the Opus R/C sailplane
Max thickness 8% at 22.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9032-il) S9032 (9%)

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S9032 (9%)Selig S9032 (9%) symmetrical horizontal stab airfoil used on the Blackhawk R/C sailplane
Max thickness 9% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9033-il) S9033 (7.5%)

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S9033 (7.5%)Selig S9033 (7.5%) symmetrical vertical stab airfoil used on the Blackhawk R/C sailplane
Max thickness 7.5% at 22.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sc20010-il) NASA SC(2)-0010 AIRFOIL

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NASA SC(2)-0010 AIRFOILNASA SC(2)-0010 airfoil (NASA TP-2969)
Max thickness 10% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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