电邮这篇文章 Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
- 作者: Kryukov V.G.1, Abdullin A.L.1, Demin A.V.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 60, 编号 1 (2017)
- 页面: 103-109
- 栏目: 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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详细
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.
作者简介
V. Kryukov
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Abdullin
Tupolev Kazan National Research Technical University
Email: alexei_demin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. Demin
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: alexei_demin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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