Compression Strength of Composite Sandwich Structures After Barely Visible Impact Damage
- 1 January 1996
- journal article
- Published by ASTM International in Journal of Composites Technology and Research
- Vol. 18 (4), 274
- https://doi.org/10.1520/ctr10113j
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- A prediction method for the compressive strength of impact damaged composite laminatesComposite Structures, 1995
- A model for predicting the behavior of impact-damaged minimum gage sandwich panels under compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Low velocity impact of composite sandwich panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Design and Analysis of Composite Structures with Manufacturing FlawsJournal of the American Helicopter Society, 1990
- Buckling, post-buckling and failure of elliptical delaminations in laminates under compressionComposite Structures, 1988
- A correlation parameter for predicting the compressive strength of composite sandwich panels after low speed impactPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Transient response of graphite/epoxy and Kevlar/epoxy laminates subjected to impactPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988