Adhesively Bonded Joint Modeling using Finite Element Method for Failure Mode Prediction-Reference-Cited by-同舟云学术

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Adhesively Bonded Joint Modeling using Finite Element Method for Failure Mode Prediction

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Stoumbos Tom G.¹,Setoodeh Shahriar¹,Francis Justin¹,Curtis Daniel¹

Affiliation:

1. Orbital Sciences Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1531

Reference6 articles.

1. Modeling Progressive Failure of Bonded Joints Using a Single Joint Finite Element

2. A Macroscopic Finite Element for a Symmetric Double Lap Joint Subjected to Mechanical and Thermal Loading

3. Failure mode maps for honeycomb sandwich panels

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. Honeycomb Core Failure Prediction in Joint using Nonlinear Finite Element Analysis;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

2. Adhesively Bonded Joint Modeling Approaches using Linear Finite Element Analysis;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02

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