Finite Element Modeling of Fatigue in Fiber–Metal Laminates-Reference-Cited by-同舟云学术

Finite Element Modeling of Fatigue in Fiber–Metal Laminates

Published:2015-08 Issue:8 Volume:53 Page:2228-2236
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Woelke Pawel B.,Rutner Marcus P.,Shields Michael D.,Rans Calvin,Alderliesten René

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053600

Reference29 articles.

1. MarissenR. “Fatigue Crack Growth in ARALL, A Hybrid Aluminium-Aramid Composite Material, Crack Growth Mechanisms and Quantitative Predictions of the Crack Growth Rate,” Ph.D. Thesis, Delft Univ. of Technology, Delft, The Netherlands, 1988.

2. Fibre-metal laminatesRecent developments and applications

3. Fibre Metal Laminates

4. VlotA. “Glare, History of the Development of a New Aircraft Material,” Kluwer Academic, Dordrecht, The Netherlands, 2001.

5. LDA's Applicability for Predicting Fatigue Crack Growth in FML's Under VA Loading

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