Influence of friction dampers on torsional blade flutter

Alok Sinha, J. H. Griffin, R. E. Kielb

    Research output: Contribution to journalArticlepeer-review

    15 Scopus citations

    Abstract

    This paper deals with the stabilizing effects of dry friction on torsional blade flutter. A lumped parameter model with single degree of freedom per blade has been used to represent the rotor stage. The well-known cascade theories for incompressible and supersonic flows have been used to determine the allowable increase in fluid velocity relative to the blade. It has been found that the effectiveness of friction dampers in controlling flutter can be substantial.

    Original languageEnglish (US)
    Pages (from-to)313-318
    Number of pages6
    JournalJournal of Engineering for Gas Turbines and Power
    Volume108
    Issue number2
    DOIs
    StatePublished - Jan 1 1986

    All Science Journal Classification (ASJC) codes

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

    Fingerprint Dive into the research topics of 'Influence of friction dampers on torsional blade flutter'. Together they form a unique fingerprint.

    Cite this