Numerical Investigation on the Supersonic Hydrogen Jet Flame Affected by Shocks
21st AIAA International Space Planes and Hypersonics Technologies Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Investigation on the Supersonic Hydrogen Jet Flame Affected by Shocks (AIAA 2017-2356)
British Library Conference Proceedings | 2017
|Investigation of crossflow shocks on delta wings in supersonic flow
Tema Archiv | 1980
|