Fatigue life of thin pre-cracked aluminum alloy panel repaired with CFRP patch at elevated temperature-Reference-Cited by-同舟云学术

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Fatigue life of thin pre-cracked aluminum alloy panel repaired with CFRP patch at elevated temperature

Published:2023 Issue: Volume:72 Page:1869-1876
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Lokhande Mayur,Shinde Prakash S.,Kumar Prashant,Shinde Hanmant P.

Publisher

Elsevier BV

Subject

General Medicine

Reference21 articles.

1. Fatigue crack propagation studies on Aluminum panels patched with Boron/Epoxy composite;Baker,1991

2. ASTM E647 15a, Standard Test Method for Measurement of Fatigue Crack Growth rates, 2015.

3. A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures;Ratwani;J. Eng. Mater. Technol.,1980

4. An FEAM based methodology for analyzing composite patch repairs of metallic structures;Nagaswamy;Struct. Integrity Aging Aircraft, ASME,1995

5. Investigation of a cracked thick aluminum panel repaired with a bonded composite patch;Schubbe;Eng. Fract. Mech.,1999

Cited by 1 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. Studying a Repair Method of LY12 Aluminum Alloy Plate;Metals;2023-10-17

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