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Numerical investigation of phisical processes in cooling jacket of thrust chamber of LOx – LH2 LRE using 3D computer simulation methods
- Authors: Yakub P.A.1, Gumennyy A.V.1
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Affiliations:
- OSC KBKhA, Voronezh
- Issue: Vol 11, No 3-1 (2012): Special Issue
- Pages: 93-98
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2100
- DOI: https://doi.org/10.18287/2541-7533-2012-0-3-1(34)-93-98
- ID: 2100
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Abstract
The problem solution of conjugate heat transfer in thrust chamber cooling jacket of liquid rocket engine is considered. Finding design data is compared with experiment.
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About the authors
P. A. Yakub
OSC KBKhA, Voronezh
Author for correspondence.
Email: pavel-vrn@list.ru
Design-engineer
Russian FederationA. V. Gumennyy
OSC KBKhA, Voronezh
Email: gav126@mail.ru
Chief of Gas Dynamics, Fluid Dynamics and Thermal Design Department
Russian FederationReferences
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- Шлихтинг, Г. Теория пограничного слоя [Текст] / Г. Шлихтинг. - М.: Наука, 1974. – 713 c.
- Kuhl, D. Thermomechanical analysis and optimization of cryogenic liquid rocket engines [Теxt] / D. Kuhl, J. Riccius // Journal of Propulsion and Power – 2002. - V.18. - №4.
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