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Computing high-speed flows past an oscillating cylinder near a vertical wallA computational method to simulate unsteady flows involving moving rigid boundaries and interference has been developed. The method is used to solve inviscid equations governing the fluid flow and the dynamic equations governing the motion of rigid bodies. A second-order accurate, upwind-biased, and alterating-direction-implicit method is used to solve the governing equations of the flow. A kinematic domain decomposition (KDD) procedure is extended to treat 3D problems with a high degree of accuracy and generality. The method under consideration is applied to both transonic and supertransonic flows. Both cases involve flow past a cylinder which is forced to pitch sinusoidally near a vertical wall. Benefits of the proposed approach include accurate calculation of the flow around 3D moving multiple bodies with interference; reduction of a numerical error; in particular, the dispersion error which strongly affects wave propagation; and minimization of the phase error which is accumulated according to the time advance procedure.
Document ID
19920072773
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yen, Guan-Wei
(NASA Langley Research Center Hampton, VA, United States)
Baysal, Oktay
(Old Dominion University Norfolk, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-4653
Report Number: AIAA PAPER 92-4653
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 10, 1992
End Date: August 12, 1992
Accession Number
92A55397
Funding Number(s)
CONTRACT_GRANT: NAG1-1150
Distribution Limits
Public
Copyright
Other

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