The interaction between mistiming and friction in the forced response of bladed disk assemblies

J. H. Griffin, Alok Sinha

    Research output: Contribution to journalArticle

    78 Citations (Scopus)

    Abstract

    This paper summarizes the results of an investigation to establish the impact of mistuning on the performance and design of blade-to-blade friction dampers of the type used to control the resonant response of turbine blades in gas turbine engines. In addition, it discusses the importance of friction slip force variations on the dynamic response of shrouded fan blades.

    Original languageEnglish (US)
    Pages (from-to)205-211
    Number of pages7
    JournalJournal of Engineering for Gas Turbines and Power
    Volume107
    Issue number1
    DOIs
    StatePublished - Jan 1 1985

    Fingerprint

    Turbines
    Friction
    Turbomachine blades
    Fans
    Dynamic response
    Gas turbines

    All Science Journal Classification (ASJC) codes

    • Nuclear Energy and Engineering
    • Fuel Technology
    • Aerospace Engineering
    • Energy Engineering and Power Technology
    • Mechanical Engineering

    Cite this

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    The interaction between mistiming and friction in the forced response of bladed disk assemblies. / Griffin, J. H.; Sinha, Alok.

    In: Journal of Engineering for Gas Turbines and Power, Vol. 107, No. 1, 01.01.1985, p. 205-211.

    Research output: Contribution to journalArticle

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