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국내 최대 기계 및 로봇 연구정보
통합검색 화살표
  • NX CAE(Nastran)
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Vibration and Acoustic Fatigue
    Volume No Loading actions (near-field jet, buzz-saw noise due to fan, turbulent boundary layer) and Damping (estimation in laminated plates, use of damping treatments).
    DATA Title Damping in acoustically excited structures.
    DATA Item 73011
    KEYWORD acoustic, curved, damping, flat, honeycomb, integral, loading, panel, skin, stiffener, stringer
    ISBN 0 85679 036 2
    ABSTRACT ESDU 73011 presents the results of over 500 tests to obtain damping ratio for flat skin-stringer panels with and without viscoelastic jointing compound, for curved skin-stringer panels with viscoelastic jointing compound, for curved and flat integrally-machined skin-stringer panels, and for honeycomb structures. The data are presented as a function of frequency so that the user can readily estimate a damping ratio appropriate to the construction used. Methods of increasing damping are discussed.

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