Numerical Research of Intra-Chamber Processes Dynamics during Startup of a Special Solid Propellant Engine
- Authors: Egorov M.Y.1
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Affiliations:
- Perm National Research Polytechnical University
- Issue: Vol 60, No 4 (2017)
- Pages: 591-599
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230310
- DOI: https://doi.org/10.3103/S106879981704016X
- ID: 230310
Cite item
Abstract
In this paper an attempt is made to conduct a direct numerical study of intra-chamber processes in a solid propellant rocket engine. An adjoin problem is formulated. To solve this problem, a set of computer applications was developed using the standard of multithreaded processing OpenCL. The results of calculations are presented.
About the authors
M. Yu. Egorov
Perm National Research Polytechnical University
Author for correspondence.
Email: egorov-m-j@yandex.ru
Russian Federation, pr. Komsomol’skii 29, Perm, 614990
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