Fatigue behavior in thick aluminum panels with a composite repair-Reference-Cited by-同舟云学术

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Fatigue behavior in thick aluminum panels with a composite repair

Published:1998-04-20 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
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Author:

Schubbe Joel¹,Mall Shankar²

Affiliation:

1. USAF, Research Lab., Wright-Patterson AFB, OH

2. USAF, Inst. of Technology, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1997

Reference22 articles.

1. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch

2. REPAIR EFFICIENCY IN FATIGUE-CRACKED ALUMINIUM COMPONENTS REINFORCED WITH BORON/EPOXY PATCHES

3. Repair of mirage III aircraft using the BFRP crack-patching technique

4. 5R. Fredell. PhD thesis, Department of Mechanical Engineering, University of Deleware, 1992.

Cited by 3 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. Effect of Patch Thickness on the Repair Performance of Bonded Composite Repair in Cracked Aluminum Plate;Materials Today: Proceedings;2017

2. Progressive failure analysis of bonded composite repairs;Composite Structures;2007-12

3. Investigation of a cracked thick aluminum panel repaired with a bonded composite patch;Engineering Fracture Mechanics;1999-06

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