Analytical statistics of forced response of a mistuned bladed disk assembly in subsonic flow

S. Chen, A. Sinha

Research output: Contribution to journalConference article

Abstract

The statistics of the forced response of a structurally and aerodynamically coupled bladed disk assembly have been computed efficiently by the analytical technique. The validity of the analytical technique has been corroborated by comparison with the results from numerical simulations. Lastly, the effects of the following parameters on the statistics of the maximum amplitude have been studied: aerodynamic coupling, fluid density, and stagger angle.

Original languageEnglish (US)
Pages (from-to)GT205 6p
JournalAmerican Society of Mechanical Engineers (Paper)
StatePublished - Jan 1 1990
EventInternational Gas Turbine and Aeroengine Congress and Exposition - Brussels, Belg
Duration: Jun 11 1990Jun 14 1990

All Science Journal Classification (ASJC) codes

  • Mechanical Engineering

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