Small-Scale Forcing of a Turbulent Boundary Layer

In order to understand the effect of small scale forcing on turbulent flows and its implications on control, an experimental investigation is made into the forcing of the inertial scales in the wall region of a turbulent boundary layer. A wall-mounted resonant actuator is used to produce a local vor...

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Main Author: Lorkowski, Thomas
Format: Technical Report
Language:en_US
Published: Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology 2010
Online Access:http://hdl.handle.net/1721.1/57605
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author Lorkowski, Thomas
author_facet Lorkowski, Thomas
author_sort Lorkowski, Thomas
collection MIT
description In order to understand the effect of small scale forcing on turbulent flows and its implications on control, an experimental investigation is made into the forcing of the inertial scales in the wall region of a turbulent boundary layer. A wall-mounted resonant actuator is used to produce a local vortical structure in the streamwise direction which is convected downstream by the boundary layer flow. The frequency associated with this structure is governed by the resonant frequency of the device and falls in the range of the inertial scales at the Reynolds number of the experiment (Re[theta] [is approximately equal to] 1200). Single and multiple point measurements have been made to determine mean and fluctuating statistics as well as dual-point correlations. These data can be used to infer changes in the structure of the near wall region of the boundary layer that are due to the actuator forcing and subsequently, to construct transfer functions between the actuator and the fluid necessary for active control.
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spelling mit-1721.1/576052019-04-10T10:25:05Z Small-Scale Forcing of a Turbulent Boundary Layer Lorkowski, Thomas In order to understand the effect of small scale forcing on turbulent flows and its implications on control, an experimental investigation is made into the forcing of the inertial scales in the wall region of a turbulent boundary layer. A wall-mounted resonant actuator is used to produce a local vortical structure in the streamwise direction which is convected downstream by the boundary layer flow. The frequency associated with this structure is governed by the resonant frequency of the device and falls in the range of the inertial scales at the Reynolds number of the experiment (Re[theta] [is approximately equal to] 1200). Single and multiple point measurements have been made to determine mean and fluctuating statistics as well as dual-point correlations. These data can be used to infer changes in the structure of the near wall region of the boundary layer that are due to the actuator forcing and subsequently, to construct transfer functions between the actuator and the fluid necessary for active control. 2010-08-27T20:02:50Z 2010-08-27T20:02:50Z 1997-01 Technical Report http://hdl.handle.net/1721.1/57605 en_US ACDL Technical Reports;FDRL TR-97-2 application/pdf Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology
spellingShingle Lorkowski, Thomas
Small-Scale Forcing of a Turbulent Boundary Layer
title Small-Scale Forcing of a Turbulent Boundary Layer
title_full Small-Scale Forcing of a Turbulent Boundary Layer
title_fullStr Small-Scale Forcing of a Turbulent Boundary Layer
title_full_unstemmed Small-Scale Forcing of a Turbulent Boundary Layer
title_short Small-Scale Forcing of a Turbulent Boundary Layer
title_sort small scale forcing of a turbulent boundary layer
url http://hdl.handle.net/1721.1/57605
work_keys_str_mv AT lorkowskithomas smallscaleforcingofaturbulentboundarylayer