Computational Advances in Reliability Assessment of Aircraft Structures Under Corrosion-Fatigue Damage-Reference-Cited by-同舟云学术

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Computational Advances in Reliability Assessment of Aircraft Structures Under Corrosion-Fatigue Damage

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
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Author:

Ghiocel Dan¹,Wang Letian¹

Affiliation:

1. Ghiocel Predictive Technologies Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2148

Reference15 articles.

1. PAPER AIAA-2005-2148

2. L3 Hole 1 70.779 -13.5% 1.234 159.6% 35.39 3.6% 0.617 64.7%

3. Exclude Interference L7 Hole 3 57.187 -63.0% 1.433 149.4% 28.593 46.8% 0.717 973.5%

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. Fatigue Life Analysis of Un-repaired and Repaired Metallic Substrate Using FRANC2D;Proceedings of the 7th International Conference on Fracture Fatigue and Wear;2018-07-15

2. DFR based fatigue reliability assessment of riveted lap joint accounting for correlations;International Journal of Fatigue;2013-02

3. Fatigue reliability assessment of riveted lap joint of aircraft structures;International Journal of Fatigue;2012-10

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