International Journal of Vehicle Structures and Systems

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Flexural Behavior of Sandwich Structure with AA 8011 Honeycomb Core and Al 1100 Face Skins


Affiliations
1 Dept. of Production Engg., Sri Sairam Engg., College, Chennai, India
2 Dept. of Mech., Engg., Bannari Amman Institute of Tech., Sathyamangalam, India
 

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This paper details the fabrication and flexural testing of sandwich structure with Aluminium honeycomb core with Aluminium face skins. The material for the face skin is aluminium 1100 and for the core is Aluminium AA8011. The cell size obtained by fabrication is 7mm. The specimen is prepared and tested as per the ASTM standard C393/C393M-11 on a three-point bending test to obtain the ultimate core shear strength and the face skin strength. Finite element analysis is also carried out to validate the experimental test.

Keywords

Sandwich Panels, Aluminium Honeycomb Core, Core Shear Strength, Finite Element Analysis.
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  • T. Bitzer. 1997. Honeycomb Technology – Materials, Design, Manufacturing, Applications and Testing, Chapman and Hall.

  • V. Crupi, G. Epasto and E. Guglielmino. 2012. Collapse modes in Aluminum honeycomb sandwich panels under bending and impact loading, Int. J. Impact Engineering, 43, 6-15.

  • K. Mohan, Y.T. Hon, S. Idapalapati and H.P. Seow. 2005. Failure of sandwich beams consisting of alumina face sheet and Aluminum foam core in bending, Materials Science and Engineering (A), 409, 292-301.

  • Hot curing epoxy system based on Araldite LY 556 / Hardener HY 917 / Accelerator DY 070, Data Sheet, Publ. No. 98010/e, February 1998, Ciba Specialty Chemicals, Switzerland.

  • ASTM C393/C393M-11. 2011. Standard Test Method for Core Shear Properties of Sandwich Constructions by Beam Flexure.

  • Quick Start Guide to Midas NFX, Version 2018, MIDAS Information Technology, Korea.

  • A. Abbadi, Y. Koutsawa, A. Carmasol, S. Belouettar and Z. Azari. 2009. Experimental and numerical characterization of honeycomb sandwich composite panels, Simulation Modelling Practice and Theory, 17, 1533-1547.


Abstract Views: 315

PDF Views: 125




  • Flexural Behavior of Sandwich Structure with AA 8011 Honeycomb Core and Al 1100 Face Skins

Abstract Views: 315  |  PDF Views: 125

Authors

M. R. Ashok
Dept. of Production Engg., Sri Sairam Engg., College, Chennai, India
M. Manojkumar
Dept. of Production Engg., Sri Sairam Engg., College, Chennai, India
P. V. Inbanaathan
Dept. of Production Engg., Sri Sairam Engg., College, Chennai, India
R. Shanmuga Prakash
Dept. of Mech., Engg., Bannari Amman Institute of Tech., Sathyamangalam, India

Abstract


This paper details the fabrication and flexural testing of sandwich structure with Aluminium honeycomb core with Aluminium face skins. The material for the face skin is aluminium 1100 and for the core is Aluminium AA8011. The cell size obtained by fabrication is 7mm. The specimen is prepared and tested as per the ASTM standard C393/C393M-11 on a three-point bending test to obtain the ultimate core shear strength and the face skin strength. Finite element analysis is also carried out to validate the experimental test.

Keywords


Sandwich Panels, Aluminium Honeycomb Core, Core Shear Strength, Finite Element Analysis.

References





DOI: https://doi.org/10.4273/ijvss.10.6.05