A Mode I cohesive law characterization procedure for through-the-thickness crack propagation in composite laminates-Reference-Cited by-同舟云学术

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A Mode I cohesive law characterization procedure for through-the-thickness crack propagation in composite laminates

Published:2016-06 Issue: Volume:94 Page:338-349
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Bergan Andrew^ORCID,Dávila Carlos,Leone Frank,Awerbuch Jonathan,Tan Tein-Min

Funder

Boeing Company Research and Technology

Federal Aviation Administration Technical Center

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference59 articles.

1. “Airworthiness standards: transport category airplanes,” Title 14 code of federal regulations,2011

2. Fracture mechanics: fundamentals and applications;Anderson,2005

3. Materials usage, design and analysis;CMH-17,2011

4. Advanced structural concept development using stitched composites;Velicki,2008

5. Assessment of damage containment features of a full-scale PRSEUS fuselage panel;Bergan;J Compos Struct,2014

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