Thrust optimization of nozzle contour including finite rate chemicalkinetics
28th Joint Propulsion Conference and Exhibit ; 1992 ; Nashville , TN , U.S.A.
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
3D Unsteady Numerical Investigation of an Overexpanded Thrust Optimized Contour Nozzle
British Library Conference Proceedings | 2009
|Nozzle contour optimization for nonuniform rocket flow
AIAA | 1983
|