A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
1951
17 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1951
|General theory of airfoil sections having arbitrary shape or pressure distribution
Engineering Index Backfile | 1945
|Calculation of airfoil section with arbitrary pressure distribution
Engineering Index Backfile | 1938
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