Abstract Multiparameter studies of the discharge coefficient dependence on the nozzle geometry and the presence of a condensed phase in combustion products were performed. The simulation results obtained satisfactorily agree with the well-known generalized data. The modern computational fluid dynamics methods were shown to be able to refine the generalized empirical relations.
Simulation of a Rocket Engine Nozzle Discharge Coefficient
Russian Aeronautics ; 61 , 2 ; 257-264
2018-04-01
8 pages
Article (Journal)
Electronic Resource
English
Simulation of a Rocket Engine Nozzle Discharge Coefficient
Online Contents | 2018
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|AIAA | 2004
|Rocket engine nozzle photographic system
NTRS | 1968
|Drag coefficient of particles in a rocket nozzle.
AIAA | 1967
|