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- W2614976008 abstract "For this study, A vibration attenuation of the vibration absorber that is attached to the flight structures was carried out. Flight structures are stabilized to allow for operations in various operating environments; however, as the size and weight of the flight structures are reduced, to meet the requisite performance, the operating-environment-induced vibrations lead to a degraded operating performance; therefore, the reduction of these vibrations should lead to an increased operating performance. The vibration absorber includes a compliant energy-storage device, such as a spring, and is mass secured to the energy-storage device. In this study, the research to prepare the anti-vibration design of the flight structures was accomplished, and the vibration of the flight structures was analyzed using the finite element analysis; accordingly, a vibration experiment for the verification of the result of the finite element analysis was also conducted. Further, the design guidelines of a tuned mass damper were obtained." @default.
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- W2614976008 date "2017-05-01" @default.
- W2614976008 modified "2023-09-26" @default.
- W2614976008 title "Vibration Absorber Design and Finite Element Analysis Model Building and Experimental Ion to Prepare the Anti-Vibration Design for the Flight Structure" @default.
- W2614976008 doi "https://doi.org/10.7736/kspe.2017.34.5.331" @default.
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