Boundary-layer analysis of subsonic inlet diffuser geometries for engine nacelles
1974
29 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Optimum subsonic, high-angle-of-attack nacelles
NTRS | 1979
|Optimum Subsonic, High-Angle-of-Attack Nacelles
NTIS | 1979
|Optimum Subsonic, High–Angle–of–Attack Nacelles
SAE Technical Papers | 1980
|Optimum subsonic, high-angle-of-attack nacelles
NTRS | 1980
|