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Mixing processe research in 10…15 N thrusters
- Authors: Salich V.L.1, Semkin E.V.1
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Affiliations:
- Research and Development Institute of Mechanical Engineering
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 112-119
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6793
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-112-119
- ID: 6793
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Abstract
This paper presents the research of possible three numerical simulation technique applications in designed calculations of 10…15 N thruster swirl atomizer. Comparison results are given.
About the authors
V. L. Salich
Research and Development Institute of Mechanical Engineering
Author for correspondence.
Email: salich_vas@mail.ru
candidate of technical science
leading research engineer of research development department
E. V. Semkin
Research and Development Institute of Mechanical Engineering
Email: sewa20-68@rambler.ru
head of group of design-engineering department
Russian FederationReferences
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