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An investigation of the vibration characteristics of shrouded-bladed-disk rotor stagesCoupled differential equations of motion are given for application to a rotating, pretwisted and heated beam under the effects of thermal stresses and gas bending loads. The circumferential modes of the multi-blade vibration of a bladed-disk rotor stage were studied. A finite element method was developed for the dynamic and static deformation analysis of the blade. The deformations of a bladed disk and a shrouded-bladed disk were studied by introducing a special bladed-disk element and a special shrouded-blade element. Some features of the vibration of part-span-shrouded, bladed-disk rotor stages are discussed. The static deformation, thermal stress and gas bending effects on the blade vibration were presented previously.
Document ID
19790044995
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Chen, L.-T.
(McDonnell Douglas Research Laboratories St. Louis, Mo., United States)
Dugundji, J.
(MIT Cambridge, Mass., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 79-0734
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials Conference
Location: St. Louis, MO
Start Date: April 4, 1979
End Date: April 6, 1979
Accession Number
79A29008
Funding Number(s)
CONTRACT_GRANT: NSG-3079
Distribution Limits
Public
Copyright
Other

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