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Published in: Technical Physics 3/2019

01-03-2019 | ATOMIC AND MOLECULAR PHYSICS

Flow Structure and Thrust Change at Gas Jet Injection into the Supersonic Part of a Nozzle

Authors: K. N. Volkov, V. N. Emelyanov, M. S. Yakovchuk

Published in: Technical Physics | Issue 3/2019

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Abstract

The numerical simulation of gas-dynamic processes accompanying the transverse injection of a gas jet into the supersonic part of a nozzle is considered in the context of creating steering forces in rocket engines. Numerical calculations are conducted based on various turbulence models at different mass flow rates of the injected gas. The calculation results obtained for the non-viscous, laminar, and turbulent formulation of the problem are compared with each other and with the physical experiment data. The formation of a shock wave and vortex flow pattern is discussed. Conclusions about the effect of problem input parameters on the thrust gain coefficient are made.

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Metadata
Title
Flow Structure and Thrust Change at Gas Jet Injection into the Supersonic Part of a Nozzle
Authors
K. N. Volkov
V. N. Emelyanov
M. S. Yakovchuk
Publication date
01-03-2019
Publisher
Pleiades Publishing
Published in
Technical Physics / Issue 3/2019
Print ISSN: 1063-7842
Electronic ISSN: 1090-6525
DOI
https://doi.org/10.1134/S1063784219030265

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