Surface Irregularity Factor as a Parameter to Evaluate the Fatigue Damage State of CFRP
Author:
Publisher
MDPI AG
Subject
General Materials Science
Link
http://www.mdpi.com/1996-1944/8/11/5407/pdf
Reference24 articles.
1. Aircraft Structural Health and Usage Monitoring;Boller,2004
2. Modeling the variable amplitude fatigue of composite materials: A review and evaluation of the state of the art for spectrum loading
3. A study on estimation of damage accumulation of glass fibre reinforce plastic (GFRP) composites under a block loading situation
4. Evaluation of the Fatigue Linear Damage Accumulation Rule for Aeronautical CFRP Using Artificial Neural Networks
5. Stiffness Reduction Mechanisms in Composite Laminates;Highsmith,1982
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