Stress Distribution Around a Semi-Circular Edge-Notch in a Finite Size Laminated Composite Plate Under Uniaxial Tension-Reference-Cited by-同舟云学术

Stress Distribution Around a Semi-Circular Edge-Notch in a Finite Size Laminated Composite Plate Under Uniaxial Tension

Published:1983-07 Issue:4 Volume:17 Page:357-367
ISSN:0021-9983
Container-title:Journal of Composite Materials
language:en
Short-container-title:Journal of Composite Materials

Author:

Lakshminarayana H.V.¹

Affiliation:

1. Materials Laboratory Air Force Wright Aeronautical Laboratories Wright-Patterson Air Force Base Ohio 45433

Abstract

A computationally efficient finite element model that can provide accurate numerical solutions to the problem of a semi-circular edge-notch in a finite size laminated composite plate under uniaxial tension is presented. Numerical results showing the effect of composite material proper ties and laminate designs on the stress field are also presented and discussed.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

http://journals.sagepub.com/doi/pdf/10.1177/002199838301700406

Reference7 articles.

1. On Solution of a Semicircular Edge Notch

2. R.J. Nuismer, "Continuum Modeling of Damage Accumulation and Ultimate Failure in Fiber Reinforced Laminated Composite Materials", Research workshop on Mechanics of Composite Materials, Duke University, Durham, North Carolina, Oct. 17-18, 1978.

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