Abstract The problem of determining the “potential” number of integration steps by explicit difference schemes is solved within the framework of the prediction model for chemically non-equilibrium processes.
Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
Russian Aeronautics ; 60 , 1 ; 103-109
2017-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Advanced rocket engine nozzles
AIAA | 1996
|Robotic Processing Of Rocket-Engine Nozzles
NTRS | 1994
|Thermocouple cements for nuclear rocket engine nozzles
Tema Archiv | 1969
|Performance of rocket engine nozzles with slot injection
AIAA | 1996
|