Buckling detection of an omega-stiffened aircraft composite panel using distributed fibre optic sensors-Reference-Cited by-同舟云学术

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Buckling detection of an omega-stiffened aircraft composite panel using distributed fibre optic sensors

Published:2018-11 Issue: Volume:132 Page:375-384
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Díaz-Maroto Patricia F.,Fernández-López Antonio,García-Alonso Jaime,Iglesias Manuel,Güemes Alfredo

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference36 articles.

1. Composite Materials for Aircraft Structures;Dutton,2004

2. R. Boyer, N. Padmapriya, Aircraft Materials, in: Ref. Modul. Mater. Sci. Mater. Eng., Elsevier. doi:10.1016/B978-0-12-803581-8.01934-2, 2016.

3. Numerical and experimental study of dynamic buckling behavior of a J-stiffened composite panel under in-plane shear;Bai;Compos. Struct.,2017

4. Composite Materials: Design and Applications;Gay,2015

5. Future structural stability design for composite space and airframe structures;Degenhardt;Thin-Walled Struct.,2014

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