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Peculiarities of solving three-dimensional problems of flow about a launch vehicle with large nose fairings using the ANSYS FLUENT software
- Authors: Kharitonova A.N.1, Shakhov V.G.2
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Affiliations:
- Samara Space Rocket Center “TsSKB-Progress”, Samara
- Samara State Aerospace University
- Issue: Vol 11, No 4 (2012)
- Pages: 116-123
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/2262
- DOI: https://doi.org/10.18287/2541-7533-2012-0-4(35)-116-123
- ID: 2262
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Abstract
The basic modes of flow about a launch vehicle with large nose fairings are discussed, some actual trajectories taken as an example. The Reynolds and Mach numbers are calculated on the basis of the parameters of the given trajectories, the modes of flow about the launch vehicles are determined. The possibility of using the ANSYS FLUENT software for the simulation of the flow about a launch vehicle on the actual trajectory is dealt with.
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About the authors
A. N. Kharitonova
Samara Space Rocket Center “TsSKB-Progress”, Samara
Author for correspondence.
Email: annqwer@mail.ru
Head of Group
Russian FederationV. G. Shakhov
Samara State Aerospace University
Email: shakhov@ssau.ru
Candidate of Technical Science, Professor
Head of the Department of Aerohydrodynamics
Russian FederationReferences
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