Failure and damage characterization of (±30°) biaxial braided composites under multiaxial stress states-Reference-Cited by-同舟云学术

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Failure and damage characterization of (±30°) biaxial braided composites under multiaxial stress states

Published:2016-11 Issue: Volume:90 Page:748-759
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Cichosz Jörg,Wehrkamp-Richter Tobias,Koerber Hannes,Hinterhölzl Roland,Camanho Pedro P.

Funder

Federal Ministry for Transport, Innovation and Technology

Federal Ministry for Economy, Family and Youth

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference38 articles.

1. CFRP using braided preforms/RTM process for aircraft applications;Uozumi;Adv Compos Mater,2005

2. Development of a composite trailing arm for a helicopter main landing gear;de Haan,2010

3. The influence of braiding configuration on damage tolerance of drive shafts;Erber,2009

4. FVK-anwendungen bei Daimler - lessons learned;Dölle,2010

5. Rüger O. Preforming: Stand der Technik & Ausblick; 2009. [acessed 24/02/2014].

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