Compressive strength of aluminum honeycomb core sandwich panels with thick carbon–epoxy facesheets subjected to barely visible indentation damage
Author:
Affiliation:
1. Sibley School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY, USA
2. Department of Mechanical and Aerospace Engineering, Syracuse University, Syracuse, NY, USA
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/0021998315575748
Reference22 articles.
1. Compressive Strength of Composite Sandwich Panels After Impact Damage: An Experimental and Analytical Study
2. Localized Impact on Sandwich Structures With Laminated Facings
3. Interfacial fracture in sandwich laminates
4. Compression after impact strength of composite sandwich panels
5. On Residual Compressive Strength Prediction of Composite Sandwich Panels after Low-Velocity Impact Damage
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1. The impact response of a Nomex® honeycomb core/E-glass/epoxy composite sandwich structure to increasing velocities: Experimental and numerical analysis;Composite Structures;2023-09
2. Review of carbon fiber-reinforced sandwich structures;Polymers and Polymer Composites;2022-01
3. Evaluation of test methods and face-sheet thickness effects in damage tolerance assessment of composite sandwich plates;Journal of Sandwich Structures & Materials;2021-08-05
4. Residual compressive strength of aluminum alloy honeycomb sandwich panel in the presence of multiple impact dents;Journal of Sandwich Structures & Materials;2021-08-01
5. Effects of honeycomb core damage on the performance of composite sandwich structures;Journal of Composite Materials;2019-12-06
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