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Modal Analysis and Testing of Honeycomb Sandwich Composites

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Abstract

In the present work, the modal parameters such as fundamental natural frequency, mode shapes and damping are estimated for honeycomb sandwich composites by varying cell size and its effect on parameters have been studied. Experimental Modal tests were conducted on hexagonal cell honeycombs of sizes 6 and 12 mm maintaining the facing thickness constant at around 1 mm with three different boundary conditions viz C-F-F-F, C-F-C-F and C-C-C-C. The traditional “strike method” has been used to measure the vibration properties. The modal characteristics of the specimens have been obtained by studying its impulse response. Each specimen has been subjected to impulses through a hard tipped hammer which is provided with a force transducer and the response has been measured through the accelerometer.

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References

  1. Yu SD, Cleghorn WL (2005) Free flexural vibration analysis of symmetric honeycomb panels. J Sound Vib 284(1–2):189–204

    Article  Google Scholar 

  2. Saitoa T, Parberyb RD, Kawnoa S (1997) Parameter identification for aluminium honeycomb sandwich panels based on orthotropic Timoshenko beam theory. J Sound Vib 208(2):271–287

    Article  Google Scholar 

  3. Boudjemai A, Bouanane MH, Mankour RA, Salem H, Chouchaoui B (2012) MDA of hexagonal honeycomb plates used for space application. World Acad Sci Eng Technol 66:221–229

    Google Scholar 

  4. Luo H, Liu G, Ma S, Liu W (2011) Dynamic analysis of the spacecraft structure on orbit made up of honeycomb sandwich plates. In: 2011 IEEE international conference on computer science and automation engineering, vol 1, pp 83–87

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  5. Liu QL, Zhao Y (2002) Role of anisotropic core in vibration properties of honeycomb sandwich panels. J Thermoplast Compos Mater 15(1): 944–952

    Article  Google Scholar 

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Acknowledgments

Authors gratefully acknowledge the Management, Principal, Head of the Department of Mechanical Engineering, and Dean, PG Studies for their constant encouragement and support in carrying out this work.

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Correspondence to Adarsh Kumar .

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© 2015 The Society for Experimental Mechanics, Inc.

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Kumar, A., Sharma, R.S. (2015). Modal Analysis and Testing of Honeycomb Sandwich Composites. In: Mains, M. (eds) Topics in Modal Analysis, Volume 10. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-319-15251-6_22

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  • DOI: https://doi.org/10.1007/978-3-319-15251-6_22

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-15250-9

  • Online ISBN: 978-3-319-15251-6

  • eBook Packages: EngineeringEngineering (R0)

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