An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distribution
1960
19 S., [10] Bl.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
DDC: | 629.13432 |