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    <meta content="Sargison, Jane E." name="eprints.creators_name" />
<meta content="Walker, Greg J." name="eprints.creators_name" />
<meta content="Bond, V." name="eprints.creators_name" />
<meta content="Chevalier, G." name="eprints.creators_name" />
<meta content="Jane.Sargison@utas.edu.au" name="eprints.creators_id" />
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<meta content="Three devices that artificially increase the thickness of the boundary layer in a wind tunnel working section have been tested. These included a serrated fence to disturb the flow, and the use of various secondary jet arrays injected into the boundary layer through the bounding surface. Momentum and turbulence profiles in the boundary layer downstream from the thickening devices were measured. The greatest boundary layer thickness was achieved using an array of varying diameter crossflow jets with the jet diameter reducing with distance downstream.However, the fence thickener and a plate with varying jets
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with momentum and turbulence profiles more typical of a natural equilibrium boundary layer." name="eprints.abstract" />
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<meta content="Roberts, J.L., The influence of hull boundary layers on
waterjet intake performance, PhD thesis, University of
Tasmania, 1998.
Roberts, J.L. and Walker, G.J., Artificial thickening of wind tunnel boundary layers via an array of cross-flow jets,
Experimental Thermal and Fluid Science, 27, 2003, 583-
588.
Patel, V.C., Calibration of the Preston tube and limitations on its use in pressure gradients., Journal of Fluid Mechanics, 23, 1965, 185-208.
Schlichting, H., 1979, “Boundary-Layer Theory”,
Seventh Edition, McGraw-Hill Book Company, New
York.
Klebanoff, P.S., Characteristics of turbulence in a boundary
layer with zero pressure gradient, NACA Rep. No. 1247,
1955.
Standen, N.M., A spire array for generating thick turbulent
shear layers for natural wind simulation in wind tunnels,
LTR-LA-94, National Aeronautical Establishment, NRC
Canada, May 1972." name="eprints.referencetext" />
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increasing in diameter downstream produce a boundary layer
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    <h1 class="ep_tm_pagetitle">Experimental review of devices to artificially thicken wind tunnel boundary layers</h1>
    <p style="margin-bottom: 1em" class="not_ep_block"><span class="person_name">Sargison, Jane E.</span> and <span class="person_name">Walker, Greg J.</span> and <span class="person_name">Bond, V.</span> and <span class="person_name">Chevalier, G.</span> (2004) <xhtml:em>Experimental review of devices to artificially thicken wind tunnel boundary layers.</xhtml:em> In: Fifteenth Australasian Fluid Mechanics Conference, 13 - 17 December 2004, Sydney.</p><p style="margin-bottom: 1em" class="not_ep_block"></p><table style="margin-bottom: 1em" class="not_ep_block"><tr><td valign="top" style="text-align:center"><a onmouseover="EPJS_ShowPreview( event, 'doc_preview_2957' );" href="http://eprints.utas.edu.au/2307/1/Sargison00091.pdf" onmouseout="EPJS_HidePreview( event, 'doc_preview_2957' );"><img alt="[img]" src="http://eprints.utas.edu.au/style/images/fileicons/application_pdf.png" class="ep_doc_icon" border="0" /></a><div class="ep_preview" id="doc_preview_2957"><table><tr><td><img alt="" src="http://eprints.utas.edu.au/2307/thumbnails/1/preview.png" class="ep_preview_image" border="0" /><div class="ep_preview_title">Preview</div></td></tr></table></div></td><td valign="top"><a href="http://eprints.utas.edu.au/2307/1/Sargison00091.pdf"><span class="ep_document_citation">PDF</span></a> - Requires a PDF viewer<br />381Kb</td></tr></table><p style="margin-bottom: 1em" class="not_ep_block">Official URL: <a href="http://www.aeromech.usyd.edu.au/15afmc/">http://www.aeromech.usyd.edu.au/15afmc/</a></p><div class="not_ep_block"><h2>Abstract</h2><p style="padding-bottom: 16px; text-align: left; margin: 1em auto 0em auto">Three devices that artificially increase the thickness of the boundary layer in a wind tunnel working section have been tested. These included a serrated fence to disturb the flow, and the use of various secondary jet arrays injected into the boundary layer through the bounding surface. Momentum and turbulence profiles in the boundary layer downstream from the thickening devices were measured. The greatest boundary layer thickness was achieved using an array of varying diameter crossflow jets with the jet diameter reducing with distance downstream.However, the fence thickener and a plate with varying jets&#13;
increasing in diameter downstream produce a boundary layer&#13;
with momentum and turbulence profiles more typical of a natural equilibrium boundary layer.</p></div><table style="margin-bottom: 1em" cellpadding="3" class="not_ep_block" border="0"><tr><th valign="top" class="ep_row">Item Type:</th><td valign="top" class="ep_row">Conference or Workshop Item (Paper)</td></tr><tr><th valign="top" class="ep_row">Subjects:</th><td valign="top" class="ep_row"><a href="http://eprints.utas.edu.au/view/subjects/291202.html">290000 Engineering and Technology &gt; 291200 Maritime Engineering &gt; 291202 Ship and Platform Hydrodynamics</a><br /><a href="http://eprints.utas.edu.au/view/subjects/290201.html">290000 Engineering and Technology &gt; 290200 Aerospace Engineering &gt; 290201 Aerodynamics</a></td></tr><tr><th valign="top" class="ep_row">ID Code:</th><td valign="top" class="ep_row">2307</td></tr><tr><th valign="top" class="ep_row">Deposited By:</th><td valign="top" class="ep_row"><span class="ep_name_citation"><span class="person_name">Dr Jane Sargison</span></span></td></tr><tr><th valign="top" class="ep_row">Deposited On:</th><td valign="top" class="ep_row">24 Oct 2007 10:28</td></tr><tr><th valign="top" class="ep_row">Last Modified:</th><td valign="top" class="ep_row">09 Jan 2008 02:30</td></tr><tr><th valign="top" class="ep_row">ePrint Statistics:</th><td valign="top" class="ep_row"><a target="ePrintStats" href="/es/index.php?action=show_detail_eprint;id=2307;">View statistics for this ePrint</a></td></tr></table><p align="right">Repository Staff Only: <a href="http://eprints.utas.edu.au/cgi/users/home?screen=EPrint::View&amp;eprintid=2307">item control page</a></p>
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