Numerical Research of Intra-Chamber Transient Processes Dynamics during Starting Operation of the Solid Propellant Rocket Engine with Special Arrangement


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Abstract

A conjugate problem statement of the computational experiment performing level is formulated. A complex of computer application programs was developed and tested for its implementation. The results of numerical study are given.

About the authors

M. Yu. Egorov

Perm National Research Polytechnic University

Author for correspondence.
Email: egorov-m-j@yandex.ru
Russian Federation, pr. Komsomol’skii 29, Perm, 614990

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