Introducing manufacturing features into numerical modeling of hypervelocity impact damage of composite pressure vessels

被引:5
|
作者
Cherniaev, Aleksandr [1 ]
Telichev, Igor [1 ]
机构
[1] Univ Manitoba, Dept Mech Engn, E2-327 EITC,75A Chancel Lors Circle, Winnipeg, MB R3T 5V6, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Orbital debris; composite pressure vessels; filament winding; meso-scale modeling;
D O I
10.1016/j.proeng.2017.09.745
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Composite pressure vessels are extensively used in unmanned spacecraft systems due to high specific strength of composites, which provides higher mass savings as compared to metallic vessels. The most common example is their use as liquid propellant tanks. Being a part of spacecraft, composite vessels are exposed to space environment, and therefore, may be subjected to hypervelocity impacts (HVI) by orbital debris or micrometeoroids. This paper analyzes the manufacturing features such as filament winding pattern and defects of fabrication that may influence the response of composite pressure vessels to HVI, and discusses the ways to introduce those features into the numerical modeling. (C) 2017 The Authors. Published by Elsevier Ltd.
引用
收藏
页码:484 / 491
页数:8
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