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Roughness-induced transition of compressible laminar boundary layers

Roughness-induced transition of compressible laminar boundary layers
Roughness-induced transition of compressible laminar boundary layers
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.
9789048137220
337-342
Springer
Redford, J.R
deaf7483-f90d-408c-b473-830ef9f439f0
Sandham, N.D.
0024d8cd-c788-4811-a470-57934fbdcf97
Roberts, G.T.
deaf59ac-e4ee-4fc2-accf-df0639d39368
Schlatter, Philipp
Henningson, Dan S.
Redford, J.R
deaf7483-f90d-408c-b473-830ef9f439f0
Sandham, N.D.
0024d8cd-c788-4811-a470-57934fbdcf97
Roberts, G.T.
deaf59ac-e4ee-4fc2-accf-df0639d39368
Schlatter, Philipp
Henningson, Dan S.

Redford, J.R, Sandham, N.D. and Roberts, G.T. (2010) Roughness-induced transition of compressible laminar boundary layers. Schlatter, Philipp and Henningson, Dan S. (eds.) In Seventh IUTAM Symposium on Lamier-Turbulent Transition: Proceedings of the Seventh IUTAM Symposium on Laminar-Turbulent Transition, Stockholm, Sweden, 2009. vol. 18, Springer. pp. 337-342 . (doi:10.1007/978-90-481-3723-7).

Record type: Conference or Workshop Item (Paper)

Abstract

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.

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More information

Published date: 11 March 2010
Venue - Dates: conference; se; 2010-03-11, Stockholm, Sweden, 2010-03-11
Organisations: Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 155293
URI: http://eprints.soton.ac.uk/id/eprint/155293
ISBN: 9789048137220
PURE UUID: a6d0d1c0-fde1-447c-bb94-4efc456bbd7e
ORCID for N.D. Sandham: ORCID iD orcid.org/0000-0002-5107-0944

Catalogue record

Date deposited: 01 Jun 2010 10:52
Last modified: 14 Mar 2024 02:42

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Contributors

Author: J.R Redford
Author: N.D. Sandham ORCID iD
Author: G.T. Roberts
Editor: Philipp Schlatter
Editor: Dan S. Henningson

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