An experimental investigation into the effect of impact damage on the compressive strength of step lap joints-Reference-Cited by-同舟云学术

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An experimental investigation into the effect of impact damage on the compressive strength of step lap joints

Published:1989-01 Issue:5 Volume:32 Page:667-674
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Van Blaricum T.J.,Bates P.,Jones R.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference8 articles.

1. Damage tolerance of graphite/epoxy composites;Baker;J. Compos. Struct.,1985

2. Effect of debonding on adhesively bonded composite to metal joints;Jahardhana;Compos. Struct.,1986

3. The damage tolerance of carbon fibre composites—a workshop summary;Challenger,1986

4. In-plane compression of damaged composite laminates;Mousley,1984

5. Fatigue of impact damaged carbon fibre composite coupons; effects of loading spectrum truncation;Clark,1986

Cited by 16 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. Design considerations in the strengthening of composite lap joints using metal z-pins;Composites Part A: Applied Science and Manufacturing;2022-09

2. An experimental and numerical investigation on fatigue of composite and metal aircraft structures;STEEL COMPOS STRUCT;2022

3. Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures;Composites Part B: Engineering;2016-09

4. Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures;Composite Structures;2016-05

5. Mode I, II and Mixed Mode I/II delamination growth in composites;Composite Structures;2014-04

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