Size Effects in Scaled Fiber Composites Under Four-Point Flexure Loading-Reference-Cited by-同舟云学术

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Size Effects in Scaled Fiber Composites Under Four-Point Flexure Loading

Published:2000-06 Issue:6 Volume:38 Page:1047-1054
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Johnson David P.¹,Morton John²,Kellas Sotiris³,Jackson Karen E.⁴

Affiliation:

1. Mississippi State University, Mississippi State, Mississippi 39762

2. Royal Aerospace Establishment, Farborough, Hampshire, England GU14 6TD, United Kingdom

3. Lockheed Engineering and Sciences Company, Inc., Hampton, Virginia 23681-0001

4. U.S. Army Research Laboratory, Hampton, Virginia 23681-0001

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1066

Reference15 articles.

1. The Effect of Stress Nonuniformity and Size on the Strength of Composite Materials

2. Note on Composite Size Effect

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Review of Similitude Methods for Structural Engineering;Applied Mechanics Reviews;2019-05-01

2. Scale Effect on Impact Performance of Unidirectional Glass Fiber Reinforced Epoxy Composite Laminates;Materials;2019-04-23

3. 7.4 Size Effects in Composites;Comprehensive Composite Materials II;2018

4. An experimental study of scaling effects in the perforation resistance of woven CFRP laminates;Composite Structures;2017-12

5. Methodology for exciting dynamic shear and moment failure in composite sandwich beams;Journal of Sandwich Structures & Materials;2012-06-18

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