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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Abstract Views: 297

PDF Views: 115




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

Abstract Views: 297  |  PDF Views: 115

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