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Elasticity effects on cavitation in a squeeze film damper undergoing noncentered circular whirlElasticity of the liner and its effects on cavitation were numerically determined for a squeeze film damper subjected to dynamic loading. The loading was manifested as a prescribed motion of the rotor undergoing noncentered circular whirl. The boundary conditions were implemented using Elrod's algorithm which conserves lineal mass flux through the moving cavitation bubble as well as the oil film region of the damper. Computational movies were used to analyze the rapidly changing pressures and vapor bubble dynamics throughout the dynamic cycle for various flexibilities in the damper liner. The effects of liner elasticity on cavitation were only noticeable for the intermediate and high values of viscosity used in this study.
Document ID
19900004470
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brewe, David E.
(Army Aviation Research and Development Command Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:102392
E-4224
AD-A217846
NASA-TM-102392
AVSCOM-TM-89-C-012
Report Number: NAS 1.15:102392
Report Number: E-4224
Report Number: AD-A217846
Report Number: NASA-TM-102392
Report Number: AVSCOM-TM-89-C-012
Meeting Information
Meeting: Nordic Symposium on Tribology
Location: Trondheim
Country: Norway
Start Date: June 26, 1988
End Date: June 29, 1988
Sponsors: Wear Magazine
Accession Number
90N13786
Funding Number(s)
PROJECT: RTOP 505-63-1A
PROJECT: DA PROJ. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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