Evaluation of mode II fatigue disbonding using Central Cut Plies specimen and distributed strain sensing technology-Reference-Cited by-同舟云学术

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Evaluation of mode II fatigue disbonding using Central Cut Plies specimen and distributed strain sensing technology

Published:2018-02-16 Issue:4 Volume:95 Page:259-285
ISSN:0021-8464
Container-title:The Journal of Adhesion
language:en
Short-container-title:The Journal of Adhesion

Author:

Ribeiro Fabricio N.¹²^ORCID,Martinez Marcias¹³^ORCID,Rans Calvin¹^ORCID

Affiliation:

1. Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherlands

2. Divisão de Sistemas Aeronáuticos, Instituto de Aeronáutica e Espaço, São José dos Campos, Brazil

3. Department of Mechanical and Aeronautical Engineering, Clarkson University, Potsdam, NY, USA

Funder

FP7 People: Marie-Curie Actions

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/10.1080/00218464.2018.1433039

Reference50 articles.

1. Flinn, R. A.; Trojan, P. K. Engineering Materials and Their Applications, 4th ed. Wiley: New York, 1995; pp 608.

2. Bonded composite repair of fatigue-cracked primary aircraft structure

3. Marissen, R. Doctoral thesis, Technische Universiteit Delft, The Netherlands, 1988.

4. Damage Tolerance Philosophy for Bonded Aircraft Structures

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