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Reynolds Stress Balance in Plane Wakes Subjected to Irrotational StrainsDirect numerical simulations of time-evolving turbulent plane wakes developing in the presence of various irrotational plane strains have been generated. A pseudospectral numerical method with up to 25 million modes is used to solve the equations in a reference frame moving with the irrotational strain. The initial condition for each simulation is taken from a previous turbulent self-similar plane wake direct numerical simulation at a velocity deficit Reynolds number, R(sub e), of about 2,000. All the terms in the equations governing the evolution of the Reynolds stresses have been calculated. The relative importance of the various terms is examined for the different strain geometries and the behavior of the individual terms is used to better assess whether the strained wakes are evolving self-similarly.
Document ID
20020049825
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Rogers, Miichael M.
(NASA Ames Research Center Moffett Field, CA United States)
Merriam, Marshal
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Aerodynamics
Meeting Information
Meeting: Fiftieth Annual Meeting of the American Physical Society, Div. of Fluid Dynamics
Location: San Francisco, CA
Country: United States
Start Date: November 23, 1997
End Date: November 25, 1997
Sponsors: American Physical Society
Funding Number(s)
PROJECT: RTOP 505-59-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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