Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
- Autores: Kryukov V.G.1, Abdullin A.L.1, Demin A.V.1
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Afiliações:
- Tupolev Kazan National Research Technical University
- Edição: Volume 60, Nº 1 (2017)
- Páginas: 103-109
- Seção: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230014
- DOI: https://doi.org/10.3103/S1068799817010159
- ID: 230014
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Resumo
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.
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Sobre autores
V. Kryukov
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Abdullin
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Demin
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: alexei_demin@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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