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Article type: Research Article
Authors: Woo, Sung-Hyun | Han, Jae-Hung
Affiliations: KOMPSAT-5 System Engineering and Integration Team, Korea Aerospace Research Institute, Daejeon, Korea | Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, Korea
Note: [] Corresponding author: Jae-Hung Han, Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Korea. Tel.: +82 42 350 3723; Fax: +82 42 350 3710; E-mail: [email protected]
Abstract: Shock induced vibration can be more crucial in the mid frequency range where the dynamic couplings with structural parts and components play important roles. To estimate the behavior of structures in this frequency range where conventional analytical schemes, such as statistical energy analysis (SEA) and finite element analysis (FEA) methods may become inaccurate, many alternative methodologies have been tried up to date. This study presents an effective and practical method to accurately predict transient responses in the mid frequency range without having to resort to the large computational efforts. Specifically, the present study employs the more realistic frequency response functions (FRFs) from the energy flow method (EFM) which is a hybrid method combining the pseudo SEA equation (or SEA-Like equation) and modal information obtained by the finite element analysis (FEA). Furthermore, to obtain the time responses synthesized with modal characteristics, a time domain correction is practiced with the input force signal and the reference FRF on a position of the response subsystem. A numerical simulation is performed for a simple five plate model to show its suitability and effectiveness over the standard analytical schemes.
Keywords: Vibro-acoustic, mid frequency, shock response, finite element analysis (FEA), shock response spectrum (SRS), statistical energy analysis (SEA), energy flow method (EFM), virtual modal synthesis and simulation (VMSS), time domain correction
DOI: 10.3233/SAV-130789
Journal: Shock and Vibration, vol. 20, no. 5, pp. 847-861, 2013
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