Acoustic-induced random vibration analysis for spacecraft using wavenumber expression of joint acceptance

The on-board components mounted on the structural panel of spacecraft are exposed to a severe random vibration environment, mainly induced by the acoustic excitation of the panel structure due to the large acoustic noise from the launch vehicle. To verify the components' resistance against...

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Bibliographic Details
Main Authors: Koki SATO, Tomoya NIWA, Qinzhong SHI, Daichi TODAKA, Shigemasa ANDO
Format: Article
Language:Japanese
Published: The Japan Society of Mechanical Engineers 2023-08-01
Series:Nihon Kikai Gakkai ronbunshu
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/transjsme/89/924/89_23-00110/_pdf/-char/en