A correlation parameter for predicting the compressive strength of composite sandwich panels after low speed impact
- 18 April 1988
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- One dimensional modelling of failure in laminated plates by delamination bucklingInternational Journal of Solids and Structures, 1981
- Hard Object Impact Damage of Metal Matrix CompositesJournal of Composite Materials, 1976
- Impact Damage Tolerance of Graphite/Epoxy Sandwich PanelsPublished by ASTM International ,1975