Mathematical model of investigating normal acoustic modes of launch vehicle modules
- Authors: Popov P.A.1, Belov A.S.1, Kryuchkov A.N.2
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Affiliations:
- Space Rocket Center «TsSKB-Progress», Samara
- Samara State Aerospace University
- Issue: Vol 11, No 4 (2012)
- Pages: 176-183
- Section: MECHANICAL ENGINEERING AND POWER ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/2270
- DOI: https://doi.org/10.18287/2541-7533-2012-0-4(35)-176-183
- ID: 2270
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Abstract
The article presents a method which considers the influence of fuel and oxidizer tanks of a launch vehicle on sound propagation in the inter-tank space. An example of finding resonant acoustic modes and frequencies of a launch vehicle module and the analysis of sound-insulation characteristics of the module are also given.
About the authors
P. A. Popov
Space Rocket Center «TsSKB-Progress», Samara
Author for correspondence.
Email: banduir@rambler.ru
Chief of Group
Russian FederationA. S. Belov
Space Rocket Center «TsSKB-Progress», Samara
Email: AnatoliyBelov@Gmail.com
Design Engineer
Russian FederationA. N. Kryuchkov
Samara State Aerospace University
Email: kan@ssau.ru
Doctor of Technical Science
Professor of the Department of Automatic Systems of Power Installations
Russian FederationReferences
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- Владимиров, В. С. Уравнения математической физики [Текст] / В. С. Владимиров - М.: Наука, 1976. - 392 с.