Pressure distribution and damping in steady roll at supersonic mach numbers of flat swept-back wings with subsonic edges
1950
57 S
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1950
|