Compression after impact strength of thin laminates with various percentage of 0° plies
Author:
Affiliation:
1. NASA-MSFC, Building 4610, Marshall Space Flight Center, USA
2. Department of Composite Material Engineering, Winona State University, USA
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/0021998312472219
Reference6 articles.
1. Compression After Impact Testing of Sandwich Composites for Usage on Expendable Launch Vehicles
2. Damage growth analysis of low velocity impacted composite panels
3. The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite
4. Compressive failure of notched carbon fibre composites
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