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Analysis of the impact of structural and gas-dynamic parameters of missiles on shock-wave processes in silos
Author(s) -
Р. А. Пешков,
Р. В. Сидельников
Publication year - 2015
Publication title -
vestnik koncerna vko «almaz - antej»
Language(s) - English
Resource type - Journals
ISSN - 2542-0542
DOI - 10.38013/2542-0542-2015-2-55-60
Subject(s) - container (type theory) , rocket (weapon) , shock (circulatory) , aerospace engineering , fluent , software , shock wave , computer science , aeronautics , engineering , mechanical engineering , computational fluid dynamics , medicine , programming language
The analysis capabilities of software ANSYS FLUENT and verification algorithm research, used to solve the problems of disclosure under rocket container space under the influence of the value of the loading of the launch canister and missiles of various factors: the speed of the rocket from the container, the different approaches to solving problems with moving boundaries, the length of the container.

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