Pressure distribution over a symmetrical airfoil section with trailing edge flap
1930
19 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
Engineering Index Backfile | 1929
|Aeroelastic Stability of a 2D Airfoil Section equipped with a Trailing Edge Flap
BASE | 2008
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