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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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(ag455ct02r-il) AG455ct -02f rot.

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AG455ct -02f rot.Drela AG455ct -02f airfoil
Max thickness 6.5% at 23.3% chord
Max camber 1.8% at 33.1% chord
Source UIUC Airfoil Coordinates Database

(ag45c03-il) AG45c -03f

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AG45c -03fDrela AG45c -03f airfoil
Max thickness 6.9% at 23.5% chord
Max camber 2% at 31.7% chord
Source UIUC Airfoil Coordinates Database

(ag45ct02r-il) AG45ct -02f

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AG45ct -02fDrela AG45ct -02f airfoil
Max thickness 6.9% at 23.3% chord
Max camber 1.8% at 33.1% chord
Source UIUC Airfoil Coordinates Database
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