Experimental Determinations of the Eigenmodes for Sandwich Bars with Different Core Reinforced with Metal Fabric

Article Preview

Abstract:

In this paper, starting from the theoretical background of modal identification, it is established an experimental method used to determine the eigenmodes of some composite bars with the core made of polypropylene honeycomb and polystyrene reinforced with metal fabric. The single-point excitation method is used. This method has been widely used in modal tests and it consists in applying a force in a given point and recording the vibratory structure response in all interest points, including the excitation point. Although the single-point excitation requires a minimum of equipment, it needs a laborious analysis to perform extensive result processing in order to interpret the dynamic behaviour of the structure under test.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

255-260

Citation:

Online since:

October 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] P.C. Yang, C.H. Norris, Y. Stavsky, Elastic Wave Propagation in Heterogeneous Plates, Int. Jour. Solids. Struct., 2 (1965), 664-684.

Google Scholar

[2] J.M. Whitney, N.Y. Pagano, Shear Deformation in Heterogeneous Anisotropic Plates, Jour. Appl. Mech., 37 (1970), 1031-1036.

DOI: 10.1115/1.3408654

Google Scholar

[3] J.N. Reddy, A Review of Refined Theories of Laminated Composites Plates, Shock and Vibration, 22 (1990), 3-17.

Google Scholar

[4] A. Noiser, R.K. Kapania, J.N. Reddy, Free vibration analysis of laminated plates using a Lay-Wise Theory, American Institute of Aeronautic and Astronautics Journal, 31 (1993), 2335-2346.

DOI: 10.2514/3.11933

Google Scholar

[5] V.N. Paimushin, I.M. Zakirov, et. al., Average Elastic and Strength Characteristics of a Honeycomb Core and a Theoretical-Experimental Method of their Determination, Mechanics of Composite Materials, 48 (2012), 511-524.

DOI: 10.1007/s11029-012-9296-0

Google Scholar

[6] N.I. Akishev, I.I. Zakirov, et. al., Theoretical-Experimental Method for Determining the Averaged Elastic and Strength Characteristics of a Honeycomb Core of Sandwich Designs, Mechanics of Composite Materials, 47 (2011), 377-386.

DOI: 10.1007/s11029-011-9216-8

Google Scholar

[7] M.S. Konsta-Gdoutos, E.E. Gdoutos, The Effect of Load and Geometry of the Failure Modes of Sandwich Beams, Applied Composite Materials, 12 (2005), 165-176.

DOI: 10.1007/s10443-005-1120-8

Google Scholar

[8] V.E. Kryutchenko, Elastic Properties of Honeycomb Sandwich Plates with Non-traditional Cell Forms, Mechanics of Composite Materials, 33 (1997), 132-135.

DOI: 10.1007/bf02269599

Google Scholar

[9] D.J. Edwins, Modal Testing. Theory and Practice, Bruel&Kjaer (1987).

Google Scholar

[10] M.M. Stanescu, D. Bolcu, I. Manea, et. Al., Experimental Researches Concerning the Properties of Composite Materials with Random Distribution of Reinforcement, Materiale Plastice, 46: 1 (2009), 73-78.

Google Scholar

[11] I. Manea, D. Bolcu, C. Miritoiu, Software for mechanical systems modal identification, Annals of the University of Craiova. Mechanical Series, 1 (2007), 191-199.

Google Scholar

[12] C. Miritoiu, D. Ilincioiu, et. al., A Comparison Between the Modal Parameters Obtained by two Different Accelerometers, The 5TH International Conference on Manufacturing Science and Education – MSE 2011, 1 (2011), 39-43.

Google Scholar