Dynamic behavior of staggered triangular honeycomb cores under in-plane crushing loadings
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Deqiang Sun
, Weihong Zhang and Jiang Yu
Abstract
A reliable finite element model was employed to investigate the effects of configuration parameters and impact velocity on the in-plane deformation mode and dynamic plateau stress of staggered triangular honeycomb cores at impact velocities 3–300 m s–1 under in-plane crushing loadings. At different impact velocities, ‘>’-, ‘<’-shaped, and ‘I’-shaped deformation modes appear in turn. The effects of configuration parameters on the deformation modes are discussed qualitatively. When all configuration parameters are kept constant, the mean in-plane dynamic plateau stress is proportional to the square of impact velocity; for a given impact velocity, the mean in-plane dynamic plateau stress is related to the ratio of cell-wall thickness to edge length by power laws and to the expanding angle by complicated curves. Mean in-plane dynamic plateau stresses are expressed by empirical equations in terms of configuration parameters and impact velocity based on our simulation results.
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© 2012, Carl Hanser Verlag, München
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- Contents
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- Award/Preisverleihung
- The Werner-Köster-Preis 2011
- Original Contributions
- Ostwald ripening in Al–Li alloys: A test of theory
- The Mg–C phase equilibria and their thermodynamic basis
- Experimental and thermodynamic study of nickel (30 wt.%Cr) – based alloys containing between 2.5 and 5.0 wt.% carbon
- Thermodynamic description of the system Cu–Sn–P experimental and numerical investigation
- Severe tempering of bainite generated at low transformation temperatures
- A comparative study of microstructure, compressive, and fracture properties of Ti3Al-based intermetallics produced via powder metallurgy, and melting and casting processes
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