The torsional stability of a compressor cascade

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Abstract

This paper includes new experimental data on the torsional stability of a compressor or fan type of blade row. This data is linked in with published material to form a three dimensional figure describing the stability of such rows. The data is then discussed by considering relative values of influence coefficients and some of the trends in the stability figure are explained. New data is also included on the relative magnitudes and phases of the influence coefficients.

Original languageEnglish
Title of host publicationManufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791879023
DOIs
Publication statusPublished - 1991
EventASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991 - Orlando, United States
Duration: 3 Jun 19916 Jun 1991

Publication series

NameProceedings of the ASME Turbo Expo
Volume5

Conference

ConferenceASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991
Country/TerritoryUnited States
CityOrlando
Period3/06/916/06/91

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