Hazizan, M.A. and Cantwell, W.J. (2003) The Low Velocity Impact Response of an Aluminium Honeycomb Sandwich Structure. Composites Part B: Engineering, 34, 679-687.
http://dx.doi.org/10.1016/S1359-8368(03)00089-1

has been cited by the following article:

• TITLE: Effect of Core Thickness and Core Density on Low Velocity Impact Behavior of Sandwich Panels with PU Foam Core

  AUTHORS: Sunith Babu Loganathan, Hanumanahally Kambada Shivanand

  KEYWORDS: Sandwich Panels, Polyurethane Foam, Specific Energy Absorption Factor, Low Velocity Impact Test

  JOURNAL NAME: Journal of Minerals and Materials Characterization and Engineering, Vol.3 No.3, May 4, 2015

  ABSTRACT: Composite sandwich structures are highly proven materials that provide high strength to weight ratio. However research works are still being carried out in the area of impact characteristics of sandwich composites. This paper provides a better understanding on the effect of core density and core thickness of sandwich panels subject to low velocity drop test. Specific energy absorption capacity of sandwich panels is obtained and factors affecting the same are explored with facings made of woven glass fiber laminates and polyurethane foam core with three different densities of 70 Kg/m3, 100 Kg/m3, 200 Kg/m3.