The impact of structural composite materials. Part 2: hypervelocity impact and shock

被引:20
作者
Appleby-Thomas, Gareth J. [2 ]
Hazell, Paul J. [1 ]
机构
[1] Univ New S Wales, UNSW Canberra, Sch Engn & Informat Technol, Canberra, ACT 2600, Australia
[2] Cranfield Univ, Cranfield MK43 0AL, Beds, England
关键词
Shock; impact; composites; spacecraft structures; hypervelocity; EQUATION-OF-STATE; DEBRIS IMPACT; DAMAGE PREDICTION; FIBER ORIENTATION; EPOXY COMPOSITE; WALL TARGETS; BEHAVIOR; SPACECRAFT; NASA; SHAPE;
D O I
10.1177/0309324712448299
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The combination of high strength and low density has resulted in increasing use of composite materials in structures such as aerospace systems that may be subjected to high-velocity impact during their in-service lives. In this review we focus on recent work surrounding the response of composites, primarily carbon fibre reinforced plastic and glass fibre reinforced plastic-based laminates to very high (hyper)-velocity impacts. To this end, the review is divided into two halves. In the first, hypervelocity impacts (e.g. impacts with velocities greater than ca. 2 km/s) that are likely to be encountered by aerospace systems are considered; while in the second, resultant material behaviour - in the form of shock response - is discussed. This review is designed to (1) build on previous studies which have typically largely focused on high-velocity impacts from the perspective of spacecraft protection against on-orbit impact, and; (2) complement an earlier part which focused on the lower impact velocity regime associated with ballistic-loading (Part 1).
引用
收藏
页码:406 / 418
页数:13
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