Damage model for metal-matrix composite under high intensity loading

被引:6
|
作者
Naboulsi, SK [1 ]
Palazotto, AN [1 ]
机构
[1] USAF, Inst Technol, Dept Aeronaut & Astronaut, Wright Patterson AFB, OH 45433 USA
关键词
D O I
10.1016/S0749-6419(01)00043-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A damage model for a composite structure under high intensity dynamic loading is presented. The model is based on a thermodynamic micromechanic approach, which is formulated using the conservation laws and the energy balance equations (the first and second laws of thermodynamics). A homogenization or averaging technique is implemented in the development to simplify the representation of the non-homogeneous material. The metal-matrix composite's inelastic response is modeled using elastic-plastic constitutive relations considering finite plastic strain and damage effect. The damage model is validated with experimental data available in the literatures, and it shows fairly good agreement. A parametric study demonstrating the characteristics of the damage model is also presented. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:435 / 468
页数:34
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