Differential Model and Evaluation of the Formal Kinetic Law in the Analysis of Combustion in a Solid-Propellant Gas Generator


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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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