Understanding the crushing behaviour of honeycombs under dynamic loading is
useful for crash simulations of vehicles and for design of impacting energ
y absorbers. Available experimental techniques, however, are not always abl
e to provide satisfactory precision for tests on honeycombs under impact lo
ading. This paper presents a new application of the Split Hopkinson Pressur
e Bar (SHPB) for testing honeycombs. Viscoelastic bars are used to improve
the accuracy of measurements, and a generalised two-strain measurement meth
od is applied to obtain a sufficient measurable maximum crush (up to 80%).
Original experimental data (especially in the in-plane crushing directions)
under impact loading are then reported. Differences between quasi-static a
nd dynamic results are discussed. (C) 1998 Elsevier Science Ltd. All rights
reserved.