Formulation of cohesive failure load for bonded single lap joints using coupled elasto-plastic stress-diffusion model-Reference-Cited by-同舟云学术

Formulation of cohesive failure load for bonded single lap joints using coupled elasto-plastic stress-diffusion model

Published:2019-11-06 Issue:4 Volume:34 Page:427-442
ISSN:0169-4243
Container-title:Journal of Adhesion Science and Technology
language:en
Short-container-title:Journal of Adhesion Science and Technology

Author:

Mazhari Emad¹,Nassar Sayed A.¹,Belingardi Giovanni²,Gerini-Romagnoli Marco¹

Affiliation:

1. Fastening and Joining Research Institute (FAJRI), Department of Mechanical Engineering, Oakland University, Rochester, MI, USA;

2. Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin, Italy

Publisher

Informa UK Limited

Subject

Materials Chemistry,Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanics of Materials,General Chemistry

Link

https://www.tandfonline.com/doi/pdf/10.1080/01694243.2019.1670594

Reference29 articles.

1. United States Department of Transportation. Handbook-Airframe AMT. Oklahoma City (OK): Federal Aviation Administration; 2012. p. 13–22.

2. Dickson JN, Hsu T-M, McKinney JM. Development of an understanding of the fatigue phenomena of bonded and bolted joints in advanced filamentary composite materials. Vol. 1. Analysis methods. Marietta: Lockheed-Georgia Co; 1972.

3. Grimes GC, Greimann L, Wah T, et al. The development of nonlinear analysis methods for bonded joints in advanced filamentary composite structures San Antonio (TX): Southwest Research Inst; 1972.

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