journal article·2018-05

Low-Velocity Impact Behavior of Sandwich Structures with Additively Manufactured Polymer Lattice Cores

Andrew J. Turner, Mohammed Al Rifaie, Ahsan Mian, Raghavan Srinivasan

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Abstract

Sandwich panel structures are widely used in aerospace, marine, and automotive applications because of their high flexural stiffness, strength-to-weight ratio, good vibration damping, and low through-thickness thermal conductivity. These structures consist of solid face sheets and low-density cellular core structures, which are traditionally based upon honeycomb folded-sheet topologies. The recent advances in additive manufacturing (AM) or 3D printing process allow lattice core configurations to be designed with improved mechanical properties. In this work, the sandwich core is comprised of lattice truss structures (LTS). Two different LTS designs are 3D-printed using acrylonitrile butadiene styrene (ABS) and are tested under low-velocity impact loads. The absorption energy and the failure mechanisms of lattice cells under such loads are investigated. The differences in energy-absorption capabilities are captured by integrating the load–displacement curve found from the impact response. It is observed that selective placement of vertical support struts in the unit-cell results in an increase in the absorption energy of the sandwich panels.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Cellular and Composite Structures · Polymer composites and self-healing · Polymer Foaming and Composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (14)

Show source-provided references
1. J.M. Hundley, E.C. Clough, and A.J. Jacobsen, The Low Velocity Impact Response of Sandwich Panels with Lattice Core Reinforcements, Int. J. Impact Eng., 2015, 84, p 64–7710.1016/j.ijimpeng.2015.05.009 ↗
2. G.S. Dhaliwal and G.M. Newaz, Modeling Low Velocity Impact Response of Carbon Fiber Reinforced Aluminum Laminates (CARALL), J. Dyn. Behav. Mater, 2016, 2, p 181–19310.1007/s40870-016-0057-3 ↗
3. J. Ju, J. Summers, J. Ziegert, and G. Fadel, Design of Honeycombs for Modulus and Yield Strain in Shear, J. Eng. Mater. Technol., 2012, 134, p 01100210.1115/1.4004488 ↗
4. M.F. Ashby, A.G. Evans, N.A. Fleck, L.J. Gibson, J.W. Hutchinson, and H.N.G. Wadley, Metal Foams: A Design Guide, Woburn, Butterworth-Heinemann, MA, 2000
5. R.A.W. Mines, S. Tsopanos, Y. Shen, R. Hasan, and S.T. McKown, Drop Weight Impact Behaviour of Sandwich Panels with Metallic Micro Lattice Cores, Int. J. Impact Eng., 2013, 60, p 120–13210.1016/j.ijimpeng.2013.04.007 ↗
6. D.J. Sypeck and N.G. Wadley, Cellular Metal Truss Core Sandwich Structures, Adv. Eng. Mater., 2002, 4(10), p 759–76410.1002/1527-2648(20021014)4:10<759::AID-ADEM759>3.0.CO;2-A ↗
7. J. Wang, A.G. Evans, K. Dharmasena, and H.N.G. Wadley, On the Performance of Truss Panels with Kagome Cores, Int. J. Solids Struct., 2003, 40, p 2981–2988
8. S. Chiras, D.R. Mumm, A.G. Evans, N. Wicks, J.W. Hutchinson, K. Dharmasena, H.N.G. Wadley, and S. Fichter, The Structural Performance of Near-Optimized Truss Core Panels, Int. J. Solids Struct., 2002, 39, p 4093–411510.1016/S0020-7683(02)00241-X ↗
9. D.T. Queheillalt and H.N.G. Wadley, Titanium Alloy Lattice Truss Structures, Mater. Des., 2009, 30, p 1966–197510.1016/j.matdes.2008.09.015 ↗
10. C. Williams, Design and Development of a Layer-Based Additive Manufacturing Process for the Realization of Metal Parts of Designed Mesostructures, Georgia Institute of Technology, Atlanta, 2008
11. Y. Shen, W. Cantwell, R. Mines, and Y. Li, Low-Velocity Impact Performance of Lattice Structure Core Based Sandwich Panels, J. Compos. Mater., 2014, 48(25), p 3153–316710.1177/0021998313507616 ↗
12. “uPrint SE Plus,” Stratasys (2017). http://www.stratasys.com/3d-printers/idea-series/uprint-se-plus . Accessed 14 Jan 2017.
13. ABSplus-P430 Material Specification Sheet, Stratasys Inc., 2015.
14. Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event, American Society of Testing and Materials, Standard D7136/D7136M − 15.