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A computational study of saddle point separation and horseshoe vortex systemIncompressible flow around a cylinder-end wall junction has been simulated by solving the incompressible Navier-Stokes equations in three dimensions. The equations, cast in generalized curvilinear coordinates, are solved in time as a hyperbolic system by adding a pressure term in the continuity equation and are marched to a steady state. Various physical quantities associated with the saddle point of separation and the horseshoe vortex system are calculated. Computational and experimental results are generally consistent. The skin friction and the pressure distribution on the end wall are consistent with the physics of the problem. Secondary flows both in front of the cylinder and behind it are predicted that are in qualitative agreement with flow visualization results. The calculations also indicate a strongly nonuniform pressure loading along the length of the cylinder. A new mechanism for the existence of the recirculation bubbles behind the cylinder-end wall with relatively low ratio of cylinder height to the approaching boundary layer thickness is observed which is markedly different from its two-dimensional counterpart.
Document ID
19850038710
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaul, U. K.
(NASA Ames Research Center Moffett Field; Informatics General Corp., Palo Alto, CA, United States)
Kwak, D.
(NASA Ames Research Center Moffett Field, CA, United States)
Wagner, C.
(U.S. Naval Underwater Systems Center New London, CT, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 85-0182
Accession Number
85A20861
Distribution Limits
Public
Copyright
Other

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