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IssuesArchive of Issues2022-1pp.132-138

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Zarubin V.S. and Zimin V.N., "On the Cyclic Deformation of the Shell of the Combustion Chamber of a Multiple-Action Liquid-Propellant Rocket Engine," Mech. Solids. 57 (1), 132-138 (2022)
Year 2022 Volume 57 Number 1 Pages 132-138
DOI 10.3103/S0025654422010174
Title On the Cyclic Deformation of the Shell of the Combustion Chamber of a Multiple-Action Liquid-Propellant Rocket Engine
Author(s) Zarubin V.S. (Bauman Moscow State Technical University, Moscow, 105005 Russia, fn2@bmstu.ru)
Zimin V.N. (Bauman Moscow State Technical University, Moscow, 105005 Russia, zimin@bmstu.ru)
Abstract When constructing a mathematical model describing the inelastic non-isothermal deformation of the inner wall of the cylindrical shell of the combustion chamber of a liquid-propellant rocket engine (LRE), a simplified design scheme of a one-dimensional stress-strain state (SSS) of a bimetallic shell was used. The analysis of changes in stresses and deformations in the inner and outer walls of the shell during the periods of start-up, operation, shutdown and pause between starts of a multiple-action LRE is carried out. To describe the inelastic deformation of the inner wall, a mechanical analogue is used, which makes it possible to describe the non-isothermal processes of plasticity and creep. An example of calculating the stress-strain state of a shell is given, which makes it possible to estimate the accumulation of the absolute value of inelastic deformation in the material of the inner wall, which affects the damageability of its material.
Keywords bimetallic shell, non-isothermal inelastic deformation, short-term creep
Received 04 March 2021Revised 19 March 2021Accepted 15 April 2021
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