Thermal/structural analyses of several hydrogen-cooled leading-edge concepts for hypersonic flight vehicles
28th Aerospace Sciences Meeting ; 1990 ; Reno , NV , U.S.A.
01.01.1990
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Thermal–structural analysis of the platelet heat-pipe-cooled leading edge of hypersonic vehicle
Online Contents | 2016
|Wing Leading-Edge Design Concepts for Airbreathing Hypersonic Waveriders
British Library Conference Proceedings | 1994
|Wing Leading-Edge Design Concepts for Airbreathing Hypersonic Waveriders
British Library Conference Proceedings | 1994
|