On the Feasibility of Using Thermal Gradients for Active Control of Interlaminar Stresses in Laminated Composites
Author:
Affiliation:
1. Boeing Commercial Airplane Group, PO. Box 3707 MS 67-HM, Seattle, WA 98124-2207
2. FAA Center of Excellence for Computational Modeling of Aircraft Structures, Georgia Institute of Technology, Atlanta, GA 30332-0356
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/002199839703101601
Reference12 articles.
1. Some observations on the interlaminar strength of composite laminates
2. Prevention of Delamination of Composite Laminates
3. Improvement of Edge Delamination Strength of Composite Laminates Using Adhesive Layers
4. On thermal edge effects in composite laminates
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