Aerodynamics interaction effects ahead of a sonic jet exhausing perpendicularly from a flat plate into a Mach number 6 free stream
1961
26 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1961
|Finite Mach number weak interaction on a flat plate.
NTRS | 1968
|Finite Mach number weak interaction on a flat plate.
AIAA | 1968
|