Skip to main content
Log in

Investigation of low velocity impact behaviors of honeycomb sandwich composites

  • Published:
Journal of Mechanical Science and Technology Aims and scope Submit manuscript

Abstract

Honeycomb sandwich composites are used as significant structural members in advanced engineering applications. Thus, it is critical to determine how they behave under impact loading, in addition to other loads. In this study, low velocity impact loading behaviors of honeycomb sandwich composites were experimentally investigated. Almost all of the design parameters of honeycomb sandwich composites were investigated. The results indicated that the core thickness of honeycomb had no effect on the strength of the composite, and the parameter influencing the impact behavior of the specimen the most was the face sheet thickness. When the face sheet thickness of the specimen was increased, the most apparent strength increase was observed in the models using carbon fiber-reinforced composite face sheets. For all face sheet types subject to impact energy of 10 Joules, the upper face sheets of 0.5 mm-thick specimens were perforated.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. S. Belouettar, A. Abbadi, Z. Azari, R. Belouettar and P. Freres, Experimental investigation of static and fatigue behaviour of composites honeycomb materials using four point bending tests, Compos. Struct., 87 (3) (2009) 265–273.

    Article  Google Scholar 

  2. S. H. Yoon, Y. W. Kwon and L. A. Clawson, Experimental investigation on low energy impact behavior of foam cored sandwich composites, J. Mech. Sci. Technol., 11 (2) (1997) 136–142.

    Google Scholar 

  3. Q. He, W. Tang, J. Zhang and X. Wang, Effects of concentrated rigid inclusions defects on the in-plane impact behavior of hexagonal honeycombs, J. Mech. Sci. Technol., 31 (10) (2017) 4691–4701.

    Article  Google Scholar 

  4. H. Yin, G. Wen, S. Hou and Q. Qing, Multiobjective crashworthiness optimization of functionally lateral graded foamfilled tubes, Mater. Des., 44 (2013) 414–428.

    Article  Google Scholar 

  5. E. J. Herup and A. N. Palazotto, Low-velocity impact damage initiation in graphite/epoxy/Nomex honeycombsandwich plates, Compos. Sci. Technol., 57 (12) (1998) 1581–1598.

    Article  Google Scholar 

  6. C. Y. Tan and H. M. Akil, Impact response of fiber metal laminate sandwich composite structure with polypropylene honeycomb core, Compos Part B-Eng., 43 (3) (2012) 1433–1438.

    Article  Google Scholar 

  7. A. Akatay, M. Ö. Bora, O. Çoban, S. Fidan and V. Tuna, The influence of low velocity repeated impacts on residual compressive properties of honeycomb sandwich structures, Compos Struct., 125 (2015) 425–433.

    Article  Google Scholar 

  8. P. M. Schubel, J. J. Luo and I. M. Daniel, Impact and post impact behavior of composite sandwich panels, Compos Part A-Appl S, 38 (3) (2007) 1051–1057.

    Article  Google Scholar 

  9. S. A. Galehdari, M. Kadkhodayan and S. Hadidi-Moud, Low velocity impact and quasi-static in-plane loading on a graded honeycomb structure; experimental, analytical and numerical study, Aerosp. Sci. Technol., 47 (2015) 425–433.

    Article  Google Scholar 

  10. B. O. Baba, Curved sandwich composites with layer-wise graded cores under impact loads, Compos. Struct., 159 (2017) 1–11.

    Article  Google Scholar 

  11. Y. M. Jen, C. W. Ko and H. B. Lin, Effect of the amount of adhesive on the bending fatigue strength of adhesively bonded aluminum honeycomb sandwich beams, Int. J. Fatigue, 31 (3) (2009) 455–462.

    Article  Google Scholar 

  12. R. Gunes and K. Arslan, Development of numerical realis-tic model for predicting low-velocity impact response of aluminium honeycomb sandwich structures, J. Sandw. Struct. Mater., 18 (1) (2016) 95–112.

    Article  Google Scholar 

  13. R. S. Sharma, V. P. Raghupathy and G. M. Priyamvada, Investigation of low velocity impact response of aluminium honeycomb sandwich panels, APRN J. Eng. Appl. Sci., 6 (2011) 7–14.

    Google Scholar 

  14. J. K. Paik, A. K. Thayamballi and G. S. Kim, The strength characteristics of aluminum honeycomb sandwich panels, Thin Wall Struct., 35 (3) (1999) 205–231.

    Article  Google Scholar 

  15. O. Mohammadiha and H. Beheshti, Optimization of functionally graded foam filled conical tubes under axial impact loading, J. Mech. Sci. Technol., 28 (5) (2014) 1741–1752.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Murat Yavuz Solmaz.

Additional information

Recommended by Editor Chongdu Cho

Tolga Topkaya graduated from Department of Mechanical Engineering at Fırat University at 2007. He gained his Ph.D. degree at the same university at 2017. He is working as Research Assistant at University of Batman, Department of Mechanical Engineering since 2010. His main research fields are composites, biomechanics and adhesion and adhesives.

Murat Yavuz Solmaz received his Ph.D. degree in Mechanical Enginering from Fırat University, Turkey, in 2008. He is currently an Associate Professor at Faculty of Engineering, Department of Mechanical Engineering, Firat Univeristy in Turkey. His research interests include composite materials, sandwich composites and adhesive joints.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Topkaya, T., Solmaz, M.Y. Investigation of low velocity impact behaviors of honeycomb sandwich composites. J Mech Sci Technol 32, 3161–3167 (2018). https://doi.org/10.1007/s12206-018-0619-5

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12206-018-0619-5

Keywords

Navigation