Fully Coupled Micro/Macro Deformation, Damage, and Failure Prediction for SiC/Ti-15-3 Laminates-Reference-Cited by-同舟云学术

Fully Coupled Micro/Macro Deformation, Damage, and Failure Prediction for SiC/Ti-15-3 Laminates

Published:2002-07 Issue:3 Volume:15 Page:74-83
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Bednarcyk Brett A.¹,Arnold Steven M.²

Affiliation:

1. Senior Research Associate, OAI, and Visiting Senior Research Scientist, Dept. of Civil Engineering, Univ. of Virginia, Thornton Hall, Charlottesville, VA 22903-2442.

2. Senior Research Engineer, NASA Glenn Research Center MS 49-7, 21000 Brookpark Rd., Cleveland, OH 44135.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282002%2915%3A3%2874%29

Reference29 articles.

1. Micromechanical analysis of thermo-inelastic multiphase short-fiber composites

2. Arnold S. M. and Castelli M. G. (1995). “What constitutes a model material?” Proc. HITEMP Review 1995 Vol. II NASA CP 10178 paper 35A NASA Glenn Research Center Cleveland.

3. A Differential CDM Model for Fatigue of Unidirectional Metal Matrix Composites

4. Micromechanics-based deformation and failure prediction for longitudinally reinforced titanium composites

5. Transverse tensile and creep modeling of continuously reinforced titanium composites with local debonding

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