Experimental Determinations of the Damping Factor for Composite Sandwich Bars Reinforced with Two Carbon Fiber Layers

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In this paper we will build some new and original composite sandwich bars reinforced with two layers of carbon fiber, with the core made of polypropylene honeycomb. Starting from the dynamic response of these bars that are in free vibration, we will establish a procedure to determine their damping factor per unit mass and per unit length. We will also determine the bars eigenfrequencies (for the first eigenmode). The bars will have the core with 10, 15 and 20 mm and the free lengths of: 200, 230, 260, 290, 320 and 350 mm. The eigenfrequencies can be used in a future research to determine the bars stiffness. The stiffness values are important if these type of composite bars are used as frames for concrete forming, because the displacements when the concrete is molded are smaller if the stiffness has high values.

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182-187

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October 2015

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] D.F. Adams, A.K. Miller, An analysis of the impact behaviour of hybrid composite materials, Mater. Sci. Eng., (1975), 245-260.

Google Scholar

[2] S. Shi, Z. Sun, et. al., Flexural strength and energy absorption of carbon-fiber-aluminum honeycomb composite reinforced by aluminum grid, Thin-Walled Structures, 84 (2014), 416-422.

DOI: 10.1016/j.tws.2014.07.015

Google Scholar

[3] A. Salehi-Khojin, M. Mahinfalah, Temperature effects on Kevlar/hybrid and carbon fiber composite sandwiches under impact loading, Composites structures, 78 (2007), 197-206.

DOI: 10.1016/j.compstruct.2005.09.005

Google Scholar

[4] J. Gustin, A. Joneson, et. al., Low velocity impact of combination Kevlar/carbon fiber sandwich composites, Composite Structures, 69 (2005), 396-406.

DOI: 10.1016/j.compstruct.2004.07.020

Google Scholar

[5] C.O. Burada, M.C. Miriţoiu, et. al., Experimental determinations of the damping factor and stiffness for new sandwich platbands with different core and reinforcements, Romanian Journal of Materials, 44 (2014), 405-413.

Google Scholar

[6] T. Anderson, E. Mandeci, Experimental investigations of low-velocity impact characteristics of sandwich composites, Compos. Struct., 50 (2000), 239-247.

Google Scholar

[7] S.M. Lee, P. Zahuta, Instrumented impact and static indentation of composites, J Compos Mater, 25 (1991), 204-222.

DOI: 10.1177/002199839102500205

Google Scholar

[8] C.W. Ong, C.W. Boey, Advanced layered personnel armor , International Journal of Impact Engineering, 38 (2011), 369-383.

DOI: 10.1016/j.ijimpeng.2010.12.003

Google Scholar

[9] W. Nowacki, Dynamics of elastic systems, Technical Publishing House (1969).

Google Scholar

[10] C.M. Miriţoiu, D. Bolcu, ,M.M. Stănescu, Determination of Damping Coefficients for Sandwich Bars with Polypropylene Honeycomb Core and the Exterior Layers Reinforced with Metal Fabric, Materiale Plastice, 49 (2012), 118-123.

DOI: 10.4028/www.scientific.net/amm.658.255

Google Scholar

[11] D. Bolcu, M.M. Stănescu, I. Ciucă, C.M. Miriţoiu, R. Cormos, Comparative Study about the Damping Properties of the Sandwich Beams with Core by Polystyrene or Polypropylene Honeycomb, Materiale Plastice, 50 (2013), 100-106.

Google Scholar

[12] I. Manea, Experimental Modal Analysis, (2006) Universitaria Publishing House.

Google Scholar

[13] Burada, C.O., Miriţoiu, C.M., Bolcu, D., Stănescu, M.M., Experimental determinations of the damping factor and stiffness for new sandwich platbands with different reinforcement and core, Romanian Journal of Materials, 44 (2014), 405-413.

DOI: 10.4028/www.scientific.net/amm.801.182

Google Scholar

[14] S.U. Khan, C.Y. Li, N.A. Siddiqui, J. -K. Kim, Vibration damping characteristics of carbon fiber-reinforced composites containing multi-walled carbon nanotubes, Composite Science and Technology, 71 (2011), 1486-1494.

DOI: 10.1016/j.compscitech.2011.03.022

Google Scholar

[15] A. Maher, F. Ramadan, M. Ferra, Modelling of vibration damping in composite structures, Composite Structures, 46 (1999), 163-170.

DOI: 10.1016/s0263-8223(99)00051-3

Google Scholar