Boundary-layer analysis of subsonic inlet diffuser geometries for engine nacelles
1974
29 S
graph. Darst
Book
English
Optimum subsonic, high-angle-of-attack nacelles
NTRS | 1979
|Optimum Subsonic, High–Angle–of–Attack Nacelles
SAE Technical Papers | 1980
|FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET
British Library Conference Proceedings | 2022
|