Numerical Research of Intra-Chamber Transient Processes Dynamics during Starting Operation of the Solid Propellant Rocket Engine with Special Arrangement
- Authors: Egorov M.Y.1
-
Affiliations:
- Perm National Research Polytechnic University
- Issue: Vol 62, No 2 (2019)
- Pages: 234-243
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/230934
- DOI: https://doi.org/10.3103/S1068799819020090
- ID: 230934
Cite item
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
Supplementary files
