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Characterization of High-Frequency Excitation of a Wake by SimulationInsights into the effects of high-frequency forcing on free shear layer evolution are gained through analysis of several direct numerical simulations. High-frequency forcing of a fully turbulent plane wake results in only a weak transient effect. On the other hand, significant changes in the developed turbulent state may result when high-frequency forcing is applied to a transitional wake. The impacts of varying the characteristics of the high-frequency forcing are examined, particularly, the streamwise wavenumber band in which forcing is applied and the initial amplitude of the forcing. The high-frequency excitation is found to increase the dissipation rate of turbulent kinetic energy, to reduce the turbulent kinetic energy production rate, and to reduce the turbulent kinetic energy suppression increases with forcing amplitude once a threshold level has been reached. For a given initial forcing energy, the largest reduction in turbulent kinetic energy density was achieved by forcing wavenumbers that are about two to three times the neutral wavenumber determined from linear stability theory.
Document ID
20030017833
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cain, Alan B.
(Innovative Technology Applications Co. Chesterfield, MO United States)
Rogers, Michael M.
(NASA Ames Research Center Moffett Field, CA United States)
Kibens, Valdis
(Boeing Co. Saint Louis, MO United States)
Mansour, Nagi
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Physics (General)
Report/Patent Number
AIAA Paper 2003-0179
Report Number: AIAA Paper 2003-0179
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 6, 2003
End Date: January 9, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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