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Airfoil database search

Search the 1638 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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(e169-il) E169 (14.4%)

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E169  (14.4%)Eppler E169 low Reynolds number airfoil
Max thickness 14.4% at 26.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e171-il) (Dicke 12.28%)

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(Dicke 12.28%)Eppler E171 low Reynolds number airfoil
Max thickness 12.3% at 32.4% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e174-il) E174 (Dicke 8.92%)

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E174  (Dicke 8.92%)Eppler E174 low Reynolds number airfoil
Max thickness 8.9% at 31.2% chord
Max camber 3.3% at 44.9% chord
Source UIUC Airfoil Coordinates Database

(e176-il) E176 (8.83%)

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E176  (8.83%)Eppler E176 low Reynolds number airfoil
Max thickness 8.8% at 30.5% chord
Max camber 2.9% at 44.2% chord
Source UIUC Airfoil Coordinates Database

(e178-il) E178 (8.69%)

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E178  (8.69%)Eppler E178 low Reynolds number airfoil
Max thickness 8.7% at 29.8% chord
Max camber 2.8% at 38.8% chord
Source UIUC Airfoil Coordinates Database

(e180-il) E180 (8.59%)

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E180  (8.59%)Eppler E180 low Reynolds number airfoil
Max thickness 8.6% at 33.5% chord
Max camber 2% at 38.1% chord
Source UIUC Airfoil Coordinates Database

(e182-il) E182 (8.47%)

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E182 (8.47%)Eppler E182 low Reynolds number airfoil
Max thickness 8.5% at 32.4% chord
Max camber 1.2% at 37.5% chord
Source UIUC Airfoil Coordinates Database

(e184-il) E184 (8.33%)

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E184  (8.33%)Eppler E184 low Reynolds number airfoil
Max thickness 8.3% at 33.3% chord
Max camber 0.8% at 38.3% chord
Source UIUC Airfoil Coordinates Database

(e186-il) E186 (10.27%)

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E186  (10.27%)Eppler E186 low Reynolds number airfoil
Max thickness 10.2% at 29% chord
Max camber 0.8% at 29% chord
Source UIUC Airfoil Coordinates Database

(e193-il) E193 (10.22%)

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E193  (10.22%)Eppler E193 low Reynolds number airfoil
Max thickness 10.2% at 31% chord
Max camber 3% at 44.7% chord
Source UIUC Airfoil Coordinates Database
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