An Innovative Integration Concept for Forebody and Two-Dimensional Hypersonic Inlet with Controllable Wall Pressure Distribution
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Forebody inlet comparison for hypersonic vehicles
AIAA | 1996
|Forebody Inlet Comparison for Hypersonic Vehicles
British Library Conference Proceedings | 1996
|