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Flow past a plate with elliptic leading edge: layer response to free-stream vorticity
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW.
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Mechanics.ORCID iD: 0000-0002-4346-4732
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Mechanics, Stability, Transition and Control.ORCID iD: 0000-0001-7864-3071
2010 (English)In: SEVENTH IUTAM SYMPOSIUM ON LAMINAR-TURBULENT TRANSITION / [ed] Schlatter P; Henningson DS, 2010, Vol. 18, 565-568 p.Conference paper, Published paper (Refereed)
Abstract [en]

We show the response of the boundary-layer flow past a wing to free-stream disturbances with axial, vertical and spanwise vorticity and explain the associated receptivity mechanisms. A flat plate with elliptic leading edge serves as wing model. and the vortical free-stream disturbances are modeled by space and time periodic Fourier modes. The results are extracted from solutions to the incompressible Navier-Stokes equations computed with the Spectral Element Method.

Place, publisher, year, edition, pages
2010. Vol. 18, 565-568 p.
Series
IUTAM Bookseries, 18
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:kth:diva-29875DOI: 10.1007/978-90-481-3723-7_101ISI: 000277097200101Scopus ID: 2-s2.0-84862272579ISBN: 978-90-481-3722-0 (print)OAI: oai:DiVA.org:kth-29875DiVA: diva2:399124
Conference
7th IUTAM Symposium on Laminar-Turbulent Transition, Royal Inst Technol, Stockholm, SWEDEN, JUN 23-26, 2009
Note
QC 20110221Available from: 2011-02-21 Created: 2011-02-17 Last updated: 2011-02-21Bibliographically approved

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Brandt, LucaHenningson, Dan S.

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