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Numerical study of gasdynamic characteristics counterflow burner with use of anisotropic models of turbulence
- Authors: Piralishvily S.A.1, Guryanov A.I.1, Badernikov A.V.1
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Affiliations:
- Rybinsk State Academy of Aviation Technology named P.A. Solovjov
- Issue: Vol 10, No 3-1 (2011): Special Issue
- Pages: 123-130
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1738
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-1(27)-123-130
- ID: 1738
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Abstract
Results of numerical simulation of viscous compressible gas in counterflow burner unit, taking into account characteristic features of flow in bounded swirling flow diaphragm walls. The calculations are performed using models of turbulence: SST, ke, RNG ke, EARSM, RSM BSL. It is shown that in the case of the Reynolds stress transport model structure of the flow has the features do not appear when using the standard two-parameter models of turbulence, but observed during the experiments.
About the authors
S. A. Piralishvily
Rybinsk State Academy of Aviation Technology named P.A. Solovjov
Author for correspondence.
Email: root@rsatu.ru
Doctor of Engineering Science
Professor
Head of the Department «General and Technical Physics»
Russian FederationA. I. Guryanov
Rybinsk State Academy of Aviation Technology named P.A. Solovjov
Email: root@rsatu.ru
Candidate of Engineering Science
Senior Lecturer of the Department «General and Technical Physics»
Russian FederationA. V. Badernikov
Rybinsk State Academy of Aviation Technology named P.A. Solovjov
Email: root@rsatu.ru
Postgraduate of the Department «General and Technical Physics»
Russian FederationReferences
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