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
Article (Journal)
Electronic Resource
English
Advanced rocket engine nozzles
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