The Guidelines of Material Design and Process Control on Hybrid Fiber Metal Laminate for Aircraft Structures-Reference-Cited by-同舟云学术

The Guidelines of Material Design and Process Control on Hybrid Fiber Metal Laminate for Aircraft Structures

Published:2019-01-30 Issue: Volume: Page:
ISSN:
Container-title:Optimum Composite Structures
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Author:

Yoon Park Sang,Jong Choi Won

Publisher

IntechOpen

Link

http://www.intechopen.com/download/pdf/62669

Reference64 articles.

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2. Alderliesten RC, Homan J. Fatigue and damage tolerance issues of GLARE in aircraft structures. International Journal of Fatigue. 2006;28:1116-1123. DOI: 10.1016/j.ijfatigue.2006.02.015

3. Fontain L. NDT on A380. In: 48th Annual Non–Destructive Testing (NDT) Forum; 20–22 September 2005; Orlando, Florida

4. Beumler T. Fiber metal laminate structures–From laboratory to application. In: Invitation to an RAeS Lecture in Cooperation with the DGLR and VDI (Presented to the Royal Aerospace Society Hamburg Branch at Hamburg University of Applied Science); 29th October 2009; Hamburg, Germany

5. Roebroeks GHJJ. Glare features. In: Vlot A, Gunnink JW, editors. Fibre Metal Laminates: An Introduction. The Netherlands: Kluwer Academic Publishers; 2001. pp. 23-37. DOI: 10.1007/978-94-010-0995-9_2

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