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Numerical and analytical study of fluid dynamic forces in seals and bearingsA numerical model based on a transformed, conservative form of the three dimensional Navier-Stokes equation and an analytical model based on lumped fluid parameters are presented and compared with studies of modeled rotor bearing seal systems. The rotor destabilizing factors are related to the rotative character of the flow field. It is shown that these destabilizing factors can be reduced through a decrease in the fluid average circumferential velocity. However, the rotative character of the flow field is a complex three dimensional system with bifurcated secondary flow patterns that significantly alter the fluid circumferential velocity. By transforming the Navier-Stokes equations to those for a rotating observer and using the numerical code PHOENICS-84 with a nonorthogonal body fitted grid, several numerical experiments were carried out to demonstrate the character of this complex flow field. In general, fluid injection and/or preswirl of the flow field opposing the shaft rotation significantly intensified these secondary recirculation zones and thus reduced the average circumferential velocity; injection or preswirl in the direction of rotation significantly weakened these zones.
Document ID
19880009483
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Tam, L. T.
(CHAM of North America, Inc. Huntsville, AL., United States)
Przekwas, A. J.
(CHAM of North America, Inc. Huntsville, AL., United States)
Muszynska, A.
(Bently Rotor Dynamics Research Corp. Minden, NV., United States)
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH., United States)
Braun, M. J.
(Akron Univ. OH., United States)
Mullen, R. L.
(Case Western Reserve Univ. Cleveland, Ohio., United States)
Tam, L. T.
(CHAM of North America, Inc. Huntsville, AL., United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-100268
NAS 1.15:100268
E-3903
Report Number: NASA-TM-100268
Report Number: NAS 1.15:100268
Report Number: E-3903
Accession Number
88N18867
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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