Roughness-induced transition of compressible laminar boundary layers
Redford, J.R, Sandham, N.D. and Roberts, G.T. (2010) Roughness-induced transition of compressible laminar boundary layers. In, Schlatter, Philipp and Henningson, Dan S. (eds.) Seventh IUTAM Symposium on Lamier-Turbulent Transition: Proceedings of the Seventh IUTAM Symposium on Laminar-Turbulent Transition, Stockholm, Sweden, 2009. Dordrecht, Netherlands, Springer, 337-342. (IUTAM Bookseries, 18). (doi:10.1007/978-90-481-3723-7).
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Direct numerical simulation is used to study flow over a roughness element in a flat plate boundary layer at high speed. The roughness element is modeled as a continuous bump with a height that is approximately half the boundary-layer thickness. Simulations with a variety of Mach numbers and wall temperatures have been run over a range of Reynolds numbers, and the results are used to establish a criterion for turbulent breakdown.
|Item Type:||Book Section|
|Subjects:||T Technology > TL Motor vehicles. Aeronautics. Astronautics|
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences > Aerodynamics & Flight Mechanics
|Date Deposited:||01 Jun 2010 10:52|
|Last Modified:||02 Mar 2012 11:35|
|Contributors:||Redford, J.R (Author)
Sandham, N.D. (Author)
Roberts, G.T. (Author)
Schlatter, Philipp (Editor)
Henningson, Dan S. (Editor)
|Date:||11 March 2010|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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