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Gas turbine rotor/case structural response to rotating stall: Experimental documentation and analytical approachThe forcing functions and structural responses characterizing gas turbine rotor/case system vibration due to rotating stall in an axial flow compressor are described. Two data sets with fundamentally different response characteristics are presented; one is supersynchronous and the other subsynchronous. Conventional beam element rotor dynamics analysis is shown to be severely limited in its ability to predict these responses. A new analytical approach, which significantly increases structural response predictive capability for these phenomena, is briefly discussed.
Document ID
19830007383
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haley, P. J.
(Detroit Diesel Allison Indianapolis, IN, United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Turbomachinery
Subject Category
Mechanical Engineering
Accession Number
83N15654
Funding Number(s)
CONTRACT_GRANT: F33615-79-C-2089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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