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
01.01.2017
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Advanced rocket engine nozzles
AIAA | 1996
|Advanced Rocket Engine Nozzles
British Library Conference Proceedings | 1996
|Robotic Processing Of Rocket-Engine Nozzles
NTRS | 1994
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