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变深度水下发射系统内弹道实验研究

吕翔 李江 陈剑 何国强 梁材 靳成学

固体火箭技术2012,Vol.35Issue(1):24-28,5.
固体火箭技术2012,Vol.35Issue(1):24-28,5.

变深度水下发射系统内弹道实验研究

Experimental investigation on interior ballistics of variable depth underwater launch system

吕翔 1李江 1陈剑 1何国强 1梁材 2靳成学2

作者信息

  • 1. 西北工业大学燃烧、热结构与内流场重点实验室,西安710072
  • 2. 中国船舶重工集团713所,郑州450015
  • 折叠

摘要

Abstract

Experiments for interior ballistics investigation of underwater launch system are carried out under different launching depths and velocities,utilizing the variable depth underwater launch simulation facility. Simplified motion equations for modeling the subscale missile' s movement in the launcher are established, and a procedure for solving the motion equations based on the experiment results are proposed. Friction coefficients and launching velocities for each experiment are obtained after a thorough analysis of experiment results,with the launching velocities verified by digital image processing results. Numerical relationship between friction coefficient and launching velocity is established based on the curve fitting. Results show that the launching velocity increment causes an opposite changing of friction coefficient. A critical launching velocity dominating the friction coefficient's slop is proposed, below which the friction coefficient presents a steep slop. It shows that the critical value of launching velocity is about 18~20 m/s.

关键词

变深度/水下发射/实验/内弹道

Key words

variable depth/underwater launch experiment/interior ballistics

分类

航空航天

引用本文复制引用

吕翔,李江,陈剑,何国强,梁材,靳成学..变深度水下发射系统内弹道实验研究[J].固体火箭技术,2012,35(1):24-28,5.

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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