• Experimental modal analysis was used to validate the model.
INTRODUCTIONIn order to reduce Eddy currents and consequently heat losses, the magnetic cores in electrical devices are usually made of large number of thin metal sheets. These sheets are stacked together and are often line welded in order to preserve shape. The magnetostriction and magetic forces are a phenomena accompanying the magnetisation process and present a problem in terms of vibrations. The intensity of vibrations depends on the dynamic properties of the structure and the magnitude of the excitation phenomena. By optimizing the design of the laminated structure, the resonant frequencies can be avoided.In order to predict the dynamic response of such structures a valid structural model must be developed, including an effective and reliable model of a contact-dependent structure, with friction between the laminae.Laminated structures are usually substantially more flexible than the equivalent homogeneous structures [1] and [2], and exhibit orthotropic behavior and high levels of internal damping due to the interlaminar friction forces [3] and [4]. The numerical model of a laminated structure has to account for the pressure distribution between laminae, as it influences the stiffness distribution within the structure [4] to [6]. The authors of [6] observed a significant increase of the eigenfrequencies even for small increases of the pressure between the laminae. Some analytical models also exist for the estimation of modal parameters of a stator packet [7] and [8]; however, they fail to take the frictional contact between the laminae into account. An efficient contact model in the field of multibody dynamics was presented in [9], which separates between the normal and tangential influences of contact parameters on a highly flexible body. Laminated structures are also commonly modelled using orthotropic material properties [10], [11] and [12] that are obtained experimentally, by measuring a real structure and consequently updating the numerical model. Simplified models are used in order to reduce the complexity, number of components in the analysis, number of details and number of degrees of freedom. Many of these models were developed for the modelling of composite structures. These methods are commonly referred to as homogenisation methods [12].Some of the methods employ "template" -2018/2/19 -9:53 -page 2 -#2 Modelling of the structure using the orthotropic material properties is performed by modifying the shear and elastic moduli of the equivalent homogeneous structure.The obtained material parameters are applicable to the specific laminated structure and assume a uniform pressure distribution and friction forces between the lamina.Thus, each modification regarding the geometry, number of laminae, number and position of welds, etc. has to be evaluated experimentally and then the valid numerical model can be created. Moreover, the introduction of orthotropic material properties can also lead to the occurrence of additional unrealistic mod...