A comparative study of failure features in aerospace grade unidirectional and bidirectional woven CFRP composite laminates under four-point bend fatigue loads-Reference-Cited by-同舟云学术

A comparative study of failure features in aerospace grade unidirectional and bidirectional woven CFRP composite laminates under four-point bend fatigue loads

Published:2015-02-11 Issue:6 Volume:46 Page:644-651
ISSN:0933-5137
Container-title:Materialwissenschaft und Werkstofftechnik
language:en
Short-container-title:Mat.-wiss. u. Werkstofftech

Author:

Suresh Kumar M.¹,Ambresha M.¹,Panbarasu K.¹,Kishore I.²,Ranganath V. R.¹

Affiliation:

1. CSIR-National Aerospace Laboratories; Bangalore 560017 India

2. Department of Materials Engineering; Indian Institute of Science; Bangalore 560 012 India

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/mawe.201400278/fullpdf

Reference13 articles.

1. D.R. Tenney J.G. Davis R.B. Pipes N. Johnston NASA composite materials development: lessons learned and future challenges. Technical Report 2009

2. C.W. Kensche Fatigue of composites for wind turbines institute of structures and design, 3rd international conference on fatigue of composites 13-15 September 2004 Kyoto, Japan

3. U.K. Vaidya B. Mathew J.M. Sands Flexural fatigue response of repaired. S2-glass/vinyl ester composites. Army Research Laboratory Report TR 4912, 2009

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