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.
Keywords
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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- ANSYS CFX Version 14.0 Documentation, 2011.
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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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