The F111C Wing Pivot Fitting Repair and its Implications for the Design/Assessment of Bonded Joints and Composite Repairs-Reference-Cited by-同舟云学术

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The F111C Wing Pivot Fitting Repair and its Implications for the Design/Assessment of Bonded Joints and Composite Repairs

Published:2018 Issue: Volume: Page:511-543
ISSN:
Container-title:Aircraft Sustainment and Repair
language:
Short-container-title:

Author:

Molent Lorrie,Jones Rhys

Publisher

Elsevier

Reference41 articles.

1. Concept and conduct of proof test of F-111 production aircraft;Buntin,1971

2. Final Engineering Report: A8-112 Wing Pivot Fitting Failure Investigation (Manufacturing processes), FZM-12-5130A;Bland,1982

3. 40 years of F-111 aircraft structural integrity support by the defence science and technology organisation;Swanton,2009

4. Design of an all boron epoxy doubler for the F-111C wing pivot fitting: Structural aspects;Molent;J. Compos. Struct.,1989

5. Stress Analysis of a Boron/Epoxy Reinforcement for the F-111C Wing Pivot Fitting, Aero. Res. Labs., ARL-STRUC-REP-426, DSTO, Melbourne, Australia;Molent,1987

Cited by 2 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. Thoughts on the durability and damage tolerance assessment of adhesively-bonded joints;Theoretical and Applied Fracture Mechanics;2022-06

2. Static and cyclic strength properties of brittle adhesives with porosity;International Journal of Fatigue;2018-12

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