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Computation of saddle point of attachmentLow-speed flows over a cylinder mounted on a flat plate are studied numerically in order to confirm the existence of a saddle point of attachment in the flow before an obstacle, to analyze the flow characteristics near the saddle point theoretically, and to address the significance of the saddle point of attachment to the construction of external flow structures, the interpretation of experimental surface oil-flow patterns, and the theoretical definition of three-dimensional flow separation. Two numerical codes, one for an incompressible flow and another for a compressible flow, are used for various Mach numbers, Reynolds numbers, grid sizes, and numbers of grid points. It is pointed out that the potential presence of a saddle point of attachment means that a line of 'oil accumulation' from both sides of a skin-friction line emanating outward from a saddle point can be either a line of separation or a line of attachment.
Document ID
19910058985
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hung, Ching-Mao
(NASA Ames Research Center Moffett Field, CA, United States)
Sung, Chao-Ho
(U.S. Navy, David W. Taylor Naval Ship Research and Development Center Bethesda, MD, United States)
Chen, Chung-Lung
(Rockwell International Science Center Thousand Oaks, CA, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-1713
Accession Number
91A43608
Distribution Limits
Public
Copyright
Other

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