Differential Model and Evaluation of the Formal Kinetic Law in the Analysis of Combustion in a Solid-Propellant Gas Generator
- 作者: Kartovitskii L.L.1, Levin V.M.1, Yanovskii L.S.2,3
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隶属关系:
- Moscow Aviation Institute (National Research University)
- Baranov Central Institute of Aviation Motors
- Institute of Problems of Chemical Physics
- 期: 卷 54, 编号 2 (2018)
- 页面: 170-178
- 栏目: Article
- URL: https://journals.rcsi.science/0010-5082/article/view/153102
- DOI: https://doi.org/10.1134/S0010508218020065
- ID: 153102
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详细
This paper presents an approach to the generalization of the features of solid propellant combustion in gas generators of propulsion systems based on a one-dimensional differential model. The heat release rate function represented by mutually orthogonal Laguerre polynomials in the differential model is identified by solving the inverse problem of combustion theory and using measured gas parameters in the gas generator. This makes it possible to establish the relationship between the solid propellant combustion features and the gas generator operating modes and formulate boundary conditions for numerical investigation of the solid propellant gas generator.
作者简介
L. Kartovitskii
Moscow Aviation Institute (National Research University)
Email: levka_58@mail.ru
俄罗斯联邦, Moscow, 125993
V. Levin
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: levka_58@mail.ru
俄罗斯联邦, Moscow, 125993
L. Yanovskii
Baranov Central Institute of Aviation Motors; Institute of Problems of Chemical Physics
Email: levka_58@mail.ru
俄罗斯联邦, Moscow, 111116; Chernogolovka, 142432
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