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Gasdynamic Analysis of a High Speed Pneumatic Missile Launching System.

机译：高速气动导弹发射系统的气动分析。

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摘要

This paper presents an analysis of a high speed compressed air missile launching system, consisting of a reservoir, valve, and launch tube. Simplifying assumptions are discussed and made, a model is determined, and its numerical solution using FORTRAN is presented. (Author)

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作者
Schneider, S. P.;
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年度 1982
页码 1-56
总页数 56
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Guided missile launchers; Gas dynamics; Mathematical models; High velocity; Compressed air; Valves; Numerical analysis; Equations; Fortran; Mathematical analysis;

机译：导弹发射器;气体动力学;数学模型;高速;压缩空气;阀门;数值分析;方程式; Fortran;数学分析;

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3. New ramjet engine to enhance range, speed of China's air-launched missiles [J] . Gabriel Dominguez Jane's Defence Weekly . 2017,第24期

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6. Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle [O] . Kui Li, Lei Wang, Yanhong Lv, 2015

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Gasdynamic Analysis of a High Speed Pneumatic Missile Launching System.

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