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

J. H. Griffin, Alok Sinha

    Research output: Contribution to journalArticle

    1 Citation (Scopus)

    Abstract

    This article summarizes the results of an investigation to establish the impact of mistuning on the perfomance 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. (A)

    Original languageEnglish (US)
    Journal[No source information available]
    StatePublished - Jan 1 1984

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    Turbines
    Friction
    Turbomachine blades
    Fans
    Dynamic response
    Gas turbines

    All Science Journal Classification (ASJC) codes

    • Mechanical Engineering

    Cite this

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    title = "The interaction between mistuning and friction in the forced response of bladed disk assemblies.",
    abstract = "This article summarizes the results of an investigation to establish the impact of mistuning on the perfomance 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. (A)",
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    AU - Sinha, Alok

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    N2 - This article summarizes the results of an investigation to establish the impact of mistuning on the perfomance 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. (A)

    AB - This article summarizes the results of an investigation to establish the impact of mistuning on the perfomance 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. (A)

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