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Performance of a three-dimensional Navier-Stokes code on CYBER 205 for high-speed juncture flowsA vectorized 3D Navier-Stokes code has been implemented on CYBER 205 for solving the supersonic laminar flow over a swept fin/flat plate junction. The code extends MacCormack's predictor-corrector finite volume scheme to a generalized coordinate system in a locally one dimensional time split fashion. A systematic parametric study is conducted to examine the effect of fin sweep on the computed flow field. Calculated results for the pressure distribution on the flat plate and fin leading edge are compared with the experimental measurements of a right angle blunt fin/flat plate junction. The decrease in the extent of the separated flow region and peak pressure on the fin leading edge, and weakening of the two reversed supersonic zones with increase in fin sweep have been clearly observed in the numerical simulation.
Document ID
19880026881
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lakshmanan, B.
(Old Dominion Univ. Norfolk, VA, United States)
Tiwari, S. N.
(Old Dominion University Norfolk, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Meeting Information
Meeting: Applications of parallel processing in fluid mechanics
Location: Cincinnati, OH
Country: United States
Start Date: June 14, 1987
End Date: June 17, 1987
Sponsors: ASME
Accession Number
88A14108
Funding Number(s)
CONTRACT_GRANT: NAS1-53003
Distribution Limits
Public
Copyright
Other

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