Spectral Stiffness Microplane Model for Quasibrittle Composite Laminates—Part I: Theory-Reference-Cited by-同舟云学术

Spectral Stiffness Microplane Model for Quasibrittle Composite Laminates—Part I: Theory

Published:2008 Issue:2 Volume:75 Page:021009
ISSN:0021-8936
Container-title:Journal of Applied Mechanics
language:en
Short-container-title:J. Appl. Mech.

Author:

Cusatis Gianluca,Beghini Alessandro,Bažant Zdeněk P.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Link

http://appliedmechanics.asmedigitalcollection.asme.org/data/Journals/JAMCAV/26682/021009_1.pdf

Reference47 articles.

1. Tensile failure of fibrous composites

2. Rosen, B. W. , 1965, “Mechanics of Composite Strengthening,”Fiber Composite Materials, ASM, Metals Park, Ohio, Chap. 3.

3. Transverse Normal Loading of a Unidirectional Composite

4. Longitudinal Shear Loading of a Unidirectional Composite

5. Bažant, Z. P., and Cedolin, L. , 2003,Stability of Structures: Elastic, Inelastic, Fracture and Damage Theories, 2nd ed., Dover Publications, New York.

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