Design and experimental calibration of the profile rotating wind tunnel with Mach number varying from 2.0 to 4.0
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
2015-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Optimization design of variable Mach number wind tunnel nozzle by rotating profile
Online Contents | 2014
|Movable panel rotating mechanism of variable mach number spray pipe of hypersonic wind tunnel
Europäisches Patentamt | 2022
|A Mach Number Monitor for a Transonic Wind Tunnel
NTIS | 1967
|