Integration methodology for waverider-derived hypersonic inlet and vehicle forebody
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Integration Methodology for Waverider-Derived Hypersonic Inlet and Vehicle Forebody (AIAA 2014-3229)
British Library Conference Proceedings | 2014
|Dual Waverider Concept for the Integration of Hypersonic Inward-Turning Inlet and Airframe Forebody
British Library Conference Proceedings | 2009
|Novel inlet–airframe integration methodology for hypersonic waverider vehicles
Online Contents | 2015
|