Mechanical design and performance of composite multifunctional materials

被引：138

作者：

Thomas, JP

Qidwai, MA

机构：

[1] USN, Res Lab, Multifunct Mat Branch, Washington, DC 20375 USA

[2] Geocenters Inc, Washington Operat, Washington, MD 20749 USA

来源：

ACTA MATERIALIA | 2004年 / 52卷 / 08期

关键词：

composites; modeling; mechanical properties; electrical properties; multifunctional;

D O I：

10.1016/j.actamat.2004.01.007

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Combining, functions in a single material entity permits improvements in system performance not possible through independent subsystem optimizations. The design of composite multifunctional materials for optimal system performance involves selection of constituents, cross-section architecture, and interface connections. We describe a methodology for deriving indices that quantitatively relate system-level performance of discrete composite components to their constituent properties and geometry. These material-architecture indices provide a useful metric for ranking composite design configurations. The methodology is demonstrated by the analysis and ranking of several notional multifunctional structure-battery laminate designs. (C) 2004 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.

引用

页码：2155 / 2164

页数：10

共 13 条

[1]

Allen D.H., 1985, INTRO AEROSPACE STRU

[2]

Anderson JD., 2012, AIRCRAFT PERFORMANCE

[3] CRITERIA FOR SELECTING THE COMPONENTS OF COMPOSITES [J].

ASHBY, MF .

ACTA METALLURGICA ET MATERIALIA, 1993, 41 (05) :1313-1335

[4] OVERVIEW NO 92 - MATERIALS AND SHAPE [J].

ASHBY, MF .

ACTA METALLURGICA ET MATERIALIA, 1991, 39 (06) :1025-1039

[5]

ASHBY MF, 1999, MAT SELECTION MECH

[6]

Ehrlich G.M., 2002, HDB BATTERIES

[7]

GOZDZ AS, 1998, Patent No. 5840087

[8]

GOZDZ AS, 2000, P 198 M EL SOC PHOEN

[9]

NIU MCY, 1992, COMPOSITE AIRFRAME S, P89

[10]

Roark R.J., 1975, FORMULAS STRESS STRA, DOI DOI 10.1016/j.vaccine.2008.10.077

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