Supersonic Combustion of Hydrogen in Mach 2 Flows Over an Axisymmetric Model
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
SUPERSONIC COMBUSTION OF HYDROGEN IN MACH 2 FLOWS OVER AN AXISYMMETRIC MODEL (AIAA 2018-5252)
British Library Conference Proceedings | 2018
|