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Airfoil database list (I).

I.S.A. 571 to I.S.A. 962

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(isa571-il) I.S.A. 571

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I.S.A. 571I.S.A. 571 airfoil
Max thickness 7.4% at 30% chord
Max camber 3.6% at 30% chord
Source UIUC Airfoil Coordinates Database

(isa960-il) I.S.A. 960

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I.S.A. 960I.S.A. 960 airfoil
Max thickness 9.5% at 30% chord
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(isa961-il) I.S.A. 961

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I.S.A. 961I.S.A. 961 airfoil
Max thickness 9.3% at 20% chord
Max camber 4.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(isa962-il) I.S.A. 962

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I.S.A. 962I.S.A. 962 airfoil
Max thickness 9.6% at 20% chord
Max camber 4.6% at 40% chord
Source UIUC Airfoil Coordinates Database
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