A Design Method for Shape Transition Nozzles for Hypersonic Vehicles
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
2018-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A DESIGN METHOD FOR SHAPE TRANSITION NOZZLES FOR HYPERSONIC VEHICLES (AIAA 2018-5318)
British Library Conference Proceedings | 2018
|Aerodynamic Shape Optimization of Hypersonic Vehicles
AIAA | 2006
|