AE monitoring of rapid crack growth in a production-size wing fatigue test article-Reference-Cited by-同舟云学术

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AE monitoring of rapid crack growth in a production-size wing fatigue test article

Published:1976-12 Issue:6 Volume:9 Page:298-304
ISSN:0308-9126
Container-title:NDT International
language:en
Short-container-title:NDT International

Author:

Bailey C.D.,Hamilton J.M.,Pless W.M.

Publisher

Elsevier BV

Subject

General Engineering

Reference7 articles.

1. Acoustic emission, STP 505,1972

2. Monitoring structural integrity by acoustic emission, STP 571,1975

3. ASTM STP 505;Nakamura,1972

4. Acoustic emission used to non-destructively determine crack locations in aircraft structural specimens;Bailey,1973

Cited by 4 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. Acoustic emission characterization of failure modes in composites with ANN;Composite Structures;2003-08

2. Acoustic emission testing the F-111;NDT International;1989-04

3. Characterization of damage initiation and propagation in graphite/epoxy laminates by acoustic emission;Engineering Fracture Mechanics;1985-01

4. Prediction of low-cycle fatigue-life by acoustic emission—1: 2024-T3 aluminum alloy;Engineering Fracture Mechanics;1981-01

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