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.
Publisher
Trans Tech Publications, Ltd.
Reference12 articles.
1. P.C. Yang, C.H. Norris, Y. Stavsky, Elastic Wave Propagation in Heterogeneous Plates, Int. Jour. Solids. Struct., 2 (1965), 664-684.
2. J.M. Whitney, N.Y. Pagano, Shear Deformation in Heterogeneous Anisotropic Plates, Jour. Appl. Mech., 37 (1970), 1031-1036.
3. J.N. Reddy, A Review of Refined Theories of Laminated Composites Plates, Shock and Vibration, 22 (1990), 3-17.
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.
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.
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献