H2/O2 rocket combustor flow field modeling, simulation and analysis
33rd Joint Propulsion Conference and Exhibit ; 1997 ; Seattle , WA , U.S.A.
1997-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
3D rocket combustor acoustics model
Tema Archiv | 1992
|Performance Prediction of a Variable Flow Ducted Rocket Combustor
British Library Conference Proceedings | 2013
|