Crashworthiness Simulation Research of Fuselage Section with Composite Skin-Reference-Cited by-同舟云学术

Crashworthiness Simulation Research of Fuselage Section with Composite Skin

Published:2014 Issue: Volume:80 Page:59-65
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Mou Haolei,Zou Tianchun,Feng Zhenyu,Ren Jian

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference14 articles.

1. Design and Evaluation of Composite Fuselage Panels Subjected to Combined Loading Conditions;Damodar;Journal of Aircraft,2005

2. Research on effects of oblique struts on crashworthiness of composite fuselage sections;Zou;Journal of Aircraft,2012

3. A comparative study of the crashworthiness of civil aircraft with different strut configurations;Ren;International Journal of Crashworthiness,2010

4. Wiggenraad JFM, Michielsen ALPJ, Santoro D, and et al. Development of a crashworthy composite fuselage structure for a commuter aircraft, NLR-TP-99532, National Aerospace Laboratory NLR, 1999: 3-14.

5. Development of a scale model composite fuselage concept for improved crashworthiness;Jackson;Journal of Aircraft,2001

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