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Experimental study of transient dynamics of a flexible rotorThe results of an experimental program to investigate the transient response of a flexible rotor are presented. The program consisted of a series of tests conducted on a rig with a rotor designed to operate above its first bending critical speed. The purpose of the tests was to obtain experimental data on the transient behavior of a flexible rotor under conditions simulating those which might occur in a jet aircraft engine. The scope of the program included tests to measure the response of both balanced and unbalanced rotors during steady-state operation, acceleration, deceleration, and simulated blade loss.
Document ID
19760019426
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hibner, D. H.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Buono, D. F.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Mechanical Engineering
Report/Patent Number
PWA-5333
NASA-CR-2703
Accession Number
76N26514
Funding Number(s)
CONTRACT_GRANT: NAS3-18523
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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