Model of pneumohydraulic launch system-Reference-Cited by-同舟云学术

Model of pneumohydraulic launch system

Published:2020-09-30 Issue:3(162), Volume: Page:6-12
ISSN:2518-1696
Container-title:Системи обробки інформації
language:
Short-container-title:soi

Author:

Амброжевич М.В.^ORCID,Середа В.О.^ORCID

Abstract

A reactive pneumohydraulic displacement system is proposed as an inclined launch system for an aircraft. The advantages of the proposed transport system in relation to the known analogs of comparable energy are stated. A complex non-stationary spatial model of the system is presented. The mathematical apparatus for constructing a model is considered. The calculation results are presented in the form of continual mappings of physical fields and integral characteristics of the launch system. The analysis of the starting characteristics for different proportions of equipment – the ratio of water and air. The conclusion is made about the effectiveness of the proposed launch system and the best equipment conditions.

Publisher

Ivan Kozhedub Kharkiv National Air Force University KNAFU

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