Email this article Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
- Authors: Kryukov V.G.1, Abdullin A.L.1, Demin A.V.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 1 (2017)
- Pages: 103-109
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/230014
- DOI: https://doi.org/10.3103/S1068799817010159
- ID: 230014
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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.
About the authors
V. G. Kryukov
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. L. Abdullin
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. V. Demin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: alexei_demin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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