Fatigue Behavior of Fiber/Metal Laminate Panels Containing Internal Carbon Tear Straps-Reference-Cited by-同舟云学术

Fatigue Behavior of Fiber/Metal Laminate Panels Containing Internal Carbon Tear Straps

Published:2011-11 Issue:6 Volume:48 Page:2122-2129
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Rans Calvin¹,Morinière Freddy¹,Rodi Riccardo¹,Alderliesten René¹,Benedictus Rinze¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031475

Reference27 articles.

1. Rodi, R. "Residual Strength of Fibre Metal Laminates," Ph.D. Dissertation,Delft University of Technology, The Netherlands(to be published).

2. Beumler, T. "Flying GLARE, A Contribution to Aircraft Certification Issues on Strengths Properties in Non-Damaged and Fatigue Damaged GLARE Structures," Ph.D. Dissertation,Delft University of Technology, The Netherlands, 2004.

3. Fibre Metal Laminates

4. Delamination growth in Fibre Metal Laminates under variable amplitude loading

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