DETERMINATION OF DELAMINATION SIZE IN HONEYCOMB SANDWICH PANEL USING FINITE ELEMENT METHOD

Authors

  • Ramzyzan Ramly Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia
  • Wahyu Kuntjoro Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia
  • Wirachman Wisnoe Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia
  • Rizal Effendy Mohd Nasir Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia
  • Aman Mohd Ihsan Mamat Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia
  • Firdaus Mohamad Flight Technology and Testing Centre, FTTC, Faculty of Mechanical Engineering, UiTM Shah Alam, Malaysia

DOI:

https://doi.org/10.11113/jt.v75.5220

Keywords:

Determination of delamination, size, honeycomb sandwich panel, finite element method

Abstract

This paper describes the determination of a relative delamination size of the skin to the honeycomb core of the honeycomb sandwich panel using the Finite Element Method approach. In the analysis, the honeycomb sandwich panel was modelled in the actual dimension using CATIA. The delamination of two different sizes (10 mm diameter and 30 mm diameter) were modelled to simulate the delamination cases. Using Nastran/Patran, the models underwent a three-point-bending test in order to simulate a result. The results were compared between the case of no delamination, 10 mm delamination, and 30 mm delamination. From the simulation, there was a significant difference of displacement of the skin (facing) between the 10 mm diameter delamination and the 30 mm diameter delamination.  

References

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Published

2015-08-20

Issue

Section

Science and Engineering

How to Cite

DETERMINATION OF DELAMINATION SIZE IN HONEYCOMB SANDWICH PANEL USING FINITE ELEMENT METHOD. (2015). Jurnal Teknologi, 75(8). https://doi.org/10.11113/jt.v75.5220