Damage tolerance of CFRP airframe bolted joints in bearing, following bolt pull-through failure-Reference-Cited by-同舟云学术

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Damage tolerance of CFRP airframe bolted joints in bearing, following bolt pull-through failure

Published:2020-03 Issue: Volume:185 Page:107766
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Giannopoulos Ioannis K.,Grafton Kaelan,Guo Shijun,Smith Howard

Publisher

Elsevier BV

Subject

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

Reference19 articles.

1. Composite airframe structures;Niu,1995

2. Airframe stress analysis and sizing;Niu,1997

3. Composite joints and connections;Camanho,2011

4. Composite materials for aircraft structures;Baker,2016

5. Certification specifications and acceptable means of compliance for large aeroplanes CS-25;EASA;Amend,2017

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1. Experimental and numerical studies on filled-hole compression of FRP laminates considering different countersunk hole configurations;Construction and Building Materials;2024-02

2. A progressive damage model for carbon fiber-reinforced polymer laminates subjected to fastener pull-through failure;Composite Structures;2023-12

3. Study on Tensile Performance of Double-Bolted Joints between Carbon Fiber Reinforced Polymer Plate and Aluminum Plate;Journal of Physics: Conference Series;2023-06-01

4. Damage tolerance in engineering components: Implementation to anchor heads;Engineering Fracture Mechanics;2022-06

5. Three-dimensional progressive damage and failure analysis of double-lap composite bolted joints under quasi-static tensile loading;Composite Structures;2022-04

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