Post-Failure Behavior of Laminates: II — Stress Concentration-Reference-Cited by-同舟云学术

Post-Failure Behavior of Laminates: II — Stress Concentration

Published:1977-01 Issue:1 Volume:11 Page:71-78
ISSN:0021-9983
Container-title:Journal of Composite Materials
language:en
Short-container-title:Journal of Composite Materials

Author:

Chou Shun-Chin¹,Orringer O.²,Rainey J.H.¹

Affiliation:

1. U.S. Army Materials and Mechanics Research Center Watertown, Massachusetts 02172

2. Aeroelastic and Structures Research Laboratory Massachusetts Institute of Technology Cambridge, Massachusetts 02139

Abstract

Experimental and analytical results are presented for the post-failure behavior of quasi-isotropic glass-epoxy laminates with a central circular hole. Load-strain response is predicted by combining a failure model developed from tests of unnotched laminates with a tangent-modulus finite-element analysis of the notched laminate. The prediction is shown to agree both qualitatively and quantitatively with experimental results.

Publisher

SAGE Publications

Subject

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

Link

http://journals.sagepub.com/doi/pdf/10.1177/002199837701100108

Reference5 articles.

1. On the Behavior of Composite Laminates After Initial Failures

2. Post-Failure Behavior of Laminates I — No Stress Concentration

3. Alternate Hybrid-Stress Elements for Analysis of Multilayer Composite Plates

4. Deformation and Failure of Boron-Epoxy Plate with Circular Hole

Cited by 21 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical methodologies for simulating bird-strike on composite wings;Composite Structures;2018-10

2. Finite Element Simulation of Interlaminar and Intralaminar Damage in Laminated Composite Plates Subjected to Impact;Latin American Journal of Solids and Structures;2018-07-02

3. Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression;Composites Part B: Engineering;2016-06

4. Progressive Failure Analysis of Composite Structures Using a Constitutive Material Model (USERMAT) Developed and Implemented in ANSYS ©;Applied Composite Materials;2011-08-11

5. A Global/Local Finite Element Approach for Predicting Interlaminar and Intralaminar Damage Evolution in Composite Stiffened Panels Under Compressive Load;Applied Composite Materials;2010-04-15