Nowadays, the experimental modal analysis in composite materials is an important tool in the structural analysis of new designs in aircraft structures. It supplies data on the behavior of these materials and, when associated with numerical methods, it can also be used to identify elastic properties. However, lightweight composite materials demand the use of appropriate techniques and devices. This paper describes an experimental modal analysis technique where the response is measured without physical contact in a large number of points using a Laser Doopler Vibrometer (LDV), and the excitation is carried out on a single point by an electromechanical shaker.
Cite This Article
Mota, G., Sollero, P., Batista, F., Albuquerque, E. (2008). Modal Analysis Technique for Anisotropic Composite Laminates. The International Conference on Computational & Experimental Engineering and Sciences, 7(2), 95–100. https://doi.org/10.3970/icces.2008.007.095
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