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Free Vibration Analysis of Foam-Core Sandwich Structures

Year 2021, Volume: 24 Issue: 1, 69 - 74, 01.03.2021
https://doi.org/10.2339/politeknik.571396

Abstract

In this
paper, the free vibration analyses of aluminum-foam sandwich structures were
completed numerically. Foam and aluminum (Al) were used for the core and
surface layers of the sandwich structure, respectively. In addition, an
adhesive was used as a thin film. Natural frequencies and mode shapes of the
sandwich structure were obtained for different thickness core and surface
materials. For this, three different sandwich structures, different thickness
of the core with same surface layers and the same core thickness with different
surface layers thickness, were modeled as SS1, SS2 and SS3.
Analyses were performed by ABAQUS/Standard
finite element software. The increase in the thickness of the Al layer
generally caused a decrease in the frequency, but this decrease is not very
dramatic. The increase in the thickness of the core has caused a serious
increase in the frequency of the sandwich structure
.

References

  • [1] Burlayenko, V. N. and Sadowski, T. “Influence Of Skin/Core Debonding On Free Vibration Behavior Of Foam And Honeycomb Cored Sandwich Plates” Internatıonal Journal Of Non-Lınear Mechanıcs 45 (10): 959–968, 2010.
  • [2] Goh, C. S., Gupta, M. J., Wei, L. and Lee, C. “Characterization Of High Performance Mg/MgO Nanocomposites.” Journal of Composite Materials 41(19): 2325–2335,2007.
  • [3] Petrone, G., Alessandro, V. D., Franco, F. Mace, B. and De Rosa, S. “Modal Characterisation Of Recyclable Foam Sandwich Panels.” Composite Structures 113(1): 362–368, 2014.
  • [4] Apalak, Z. G., Ekici, R., Yildirim, M., Apalak, M. K. “Free Vibration Analysis Of An Adhesively Bonded Functionally Graded Double Containment Cantilever Joint.” Journal of Adhesion Science and Technology 28(12): 1117–1139, 2014.
  • [5] Chen, J. E., Zhang, W., Sun, M., Yao, M. H., Liu, J. “Free Vibration Analysis Of Composite Sandwich Plates With Different Truss Cores.” Mechanics of Advanced Materials and Structures, 24(1): 1–13, 2017.
  • [6] Sakar, G., and Bolat, C. “The Free Vibration Analysis of Honeycomb Sandwich Beam Using 3D and Continuum Model” International Journal of Mechanical and Mechatronics Engineering 9 (6): 1077-1081, 2015.
  • [7] Lashin, M. M. A, and Nady, A. O. E. “The Free Vibration Analysis of Sandwich Beam Stracture Using Finite Element Approach” Journal of Mechanical and Civil Engineering 12 (1): 34-42, 2015.
  • [8] Khare, R. K., Kant, T., and Garg, A. A. “Free Vibration of Composite and Sandwich Laminates With a Higher-Order Facet Shell Element.” Composite Structures 65: 405–418, 2004.
  • [9] Nilsson, E., and Nilsson, A. C. “Prediction and Measurement of Some Dynamic Properties of Sandwich Structures with Honeycomb and Foam Cores.” Journal of Sound and Vibration, 251: 409-430, 2002.
  • [10] Li, Z., and Crocker, M. J. “Effects of Thickness and Delamination on the Damping in Honeycomb–Foam Sandwich Beams.” Journal of Sound and Vibration 294: 473-485, 2006.
  • [11] Lai, L. “Study of Free Vibration of Aluminum Honeycomb Panels.” MSc. Thesis, Toronto University, 2002.

Free Vibration Analysis of Foam-Core Sandwich Structures

Year 2021, Volume: 24 Issue: 1, 69 - 74, 01.03.2021
https://doi.org/10.2339/politeknik.571396

Abstract

In this paper, the free vibration analyses of aluminum-foam sandwich structures were completed numerically. Foam and aluminum (Al) were used for the core and surface layers of the sandwich structure, respectively. In addition, an adhesive was used as a thin film. Natural frequencies and mode shapes of the sandwich structure were obtained for different thickness core and surface materials. For this, three different sandwich structures, different thickness of the core with same surface layers and the same core thickness with different surface layers thickness, were modeled as SS1, SS2 and SS3. Analyses were performed by ABAQUS/Standard finite element software. The increase in the thickness of the Al layer generally caused a decrease in the frequency, but this decrease is not very dramatic. The increase in the thickness of the core has caused a serious increase in the frequency of the sandwich structure.

References

  • [1] Burlayenko, V. N. and Sadowski, T. “Influence Of Skin/Core Debonding On Free Vibration Behavior Of Foam And Honeycomb Cored Sandwich Plates” Internatıonal Journal Of Non-Lınear Mechanıcs 45 (10): 959–968, 2010.
  • [2] Goh, C. S., Gupta, M. J., Wei, L. and Lee, C. “Characterization Of High Performance Mg/MgO Nanocomposites.” Journal of Composite Materials 41(19): 2325–2335,2007.
  • [3] Petrone, G., Alessandro, V. D., Franco, F. Mace, B. and De Rosa, S. “Modal Characterisation Of Recyclable Foam Sandwich Panels.” Composite Structures 113(1): 362–368, 2014.
  • [4] Apalak, Z. G., Ekici, R., Yildirim, M., Apalak, M. K. “Free Vibration Analysis Of An Adhesively Bonded Functionally Graded Double Containment Cantilever Joint.” Journal of Adhesion Science and Technology 28(12): 1117–1139, 2014.
  • [5] Chen, J. E., Zhang, W., Sun, M., Yao, M. H., Liu, J. “Free Vibration Analysis Of Composite Sandwich Plates With Different Truss Cores.” Mechanics of Advanced Materials and Structures, 24(1): 1–13, 2017.
  • [6] Sakar, G., and Bolat, C. “The Free Vibration Analysis of Honeycomb Sandwich Beam Using 3D and Continuum Model” International Journal of Mechanical and Mechatronics Engineering 9 (6): 1077-1081, 2015.
  • [7] Lashin, M. M. A, and Nady, A. O. E. “The Free Vibration Analysis of Sandwich Beam Stracture Using Finite Element Approach” Journal of Mechanical and Civil Engineering 12 (1): 34-42, 2015.
  • [8] Khare, R. K., Kant, T., and Garg, A. A. “Free Vibration of Composite and Sandwich Laminates With a Higher-Order Facet Shell Element.” Composite Structures 65: 405–418, 2004.
  • [9] Nilsson, E., and Nilsson, A. C. “Prediction and Measurement of Some Dynamic Properties of Sandwich Structures with Honeycomb and Foam Cores.” Journal of Sound and Vibration, 251: 409-430, 2002.
  • [10] Li, Z., and Crocker, M. J. “Effects of Thickness and Delamination on the Damping in Honeycomb–Foam Sandwich Beams.” Journal of Sound and Vibration 294: 473-485, 2006.
  • [11] Lai, L. “Study of Free Vibration of Aluminum Honeycomb Panels.” MSc. Thesis, Toronto University, 2002.
There are 11 citations in total.

Details

Primary Language English
Subjects Engineering
Journal Section Research Article
Authors

Ertan Kösedağ 0000-0002-5580-0414

Recep Ekici 0000-0002-4420-8431

Publication Date March 1, 2021
Submission Date May 29, 2019
Published in Issue Year 2021 Volume: 24 Issue: 1

Cite

APA Kösedağ, E., & Ekici, R. (2021). Free Vibration Analysis of Foam-Core Sandwich Structures. Politeknik Dergisi, 24(1), 69-74. https://doi.org/10.2339/politeknik.571396
AMA Kösedağ E, Ekici R. Free Vibration Analysis of Foam-Core Sandwich Structures. Politeknik Dergisi. March 2021;24(1):69-74. doi:10.2339/politeknik.571396
Chicago Kösedağ, Ertan, and Recep Ekici. “Free Vibration Analysis of Foam-Core Sandwich Structures”. Politeknik Dergisi 24, no. 1 (March 2021): 69-74. https://doi.org/10.2339/politeknik.571396.
EndNote Kösedağ E, Ekici R (March 1, 2021) Free Vibration Analysis of Foam-Core Sandwich Structures. Politeknik Dergisi 24 1 69–74.
IEEE E. Kösedağ and R. Ekici, “Free Vibration Analysis of Foam-Core Sandwich Structures”, Politeknik Dergisi, vol. 24, no. 1, pp. 69–74, 2021, doi: 10.2339/politeknik.571396.
ISNAD Kösedağ, Ertan - Ekici, Recep. “Free Vibration Analysis of Foam-Core Sandwich Structures”. Politeknik Dergisi 24/1 (March 2021), 69-74. https://doi.org/10.2339/politeknik.571396.
JAMA Kösedağ E, Ekici R. Free Vibration Analysis of Foam-Core Sandwich Structures. Politeknik Dergisi. 2021;24:69–74.
MLA Kösedağ, Ertan and Recep Ekici. “Free Vibration Analysis of Foam-Core Sandwich Structures”. Politeknik Dergisi, vol. 24, no. 1, 2021, pp. 69-74, doi:10.2339/politeknik.571396.
Vancouver Kösedağ E, Ekici R. Free Vibration Analysis of Foam-Core Sandwich Structures. Politeknik Dergisi. 2021;24(1):69-74.