TY - JOUR T1 - Free Vibration Analysis of Foam-Core Sandwich Structures TT - Free Vibration Analysis of Foam-Core Sandwich Structures AU - Kösedağ, Ertan AU - Ekici, Recep PY - 2021 DA - March DO - 10.2339/politeknik.571396 JF - Politeknik Dergisi PB - Gazi University WT - DergiPark SN - 2147-9429 SP - 69 EP - 74 VL - 24 IS - 1 LA - en AB - In thispaper, the free vibration analyses of aluminum-foam sandwich structures werecompleted numerically. Foam and aluminum (Al) were used for the core andsurface layers of the sandwich structure, respectively. In addition, anadhesive was used as a thin film. Natural frequencies and mode shapes of thesandwich structure were obtained for different thickness core and surfacematerials. For this, three different sandwich structures, different thicknessof the core with same surface layers and the same core thickness with differentsurface layers thickness, were modeled as SS1, SS2 and SS3. Analyses were performed by ABAQUS/Standardfinite element software. The increase in the thickness of the Al layergenerally caused a decrease in the frequency, but this decrease is not verydramatic. The increase in the thickness of the core has caused a seriousincrease in the frequency of the sandwich structure. KW - Foam-core KW - free vibration KW - natural frequencies KW - numeric analysis KW - sandwich structures N2 - 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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [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. CR - [11] Lai, L. “Study of Free Vibration of Aluminum Honeycomb Panels.” MSc. Thesis, Toronto University, 2002. UR - https://doi.org/10.2339/politeknik.571396 L1 - https://dergipark.org.tr/en/download/article-file/973828 ER -