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Excitation of 3D TS-waves in a swept-wing boundary layer by surface vibrations and freestream vortices
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2018 (English)In: AIP Conference Proceedings, American Institute of Physics Inc. , 2018Conference paper, Published paper (Refereed)
Abstract [en]

There are several kinds of velocity disturbances, which may affect the transition to turbulence in a swept wing boundary layer. Tollmien-Schlichting (TS) waves are among most important of them. The properties of TS waves and their potential competition with cross-flow waves on a swept wing are poorly studied in theoretical works and were not studied experimentally at all. This paper presents the method of excitation of fully controlled 3D TS waves via interaction of free-stream vortices and surface vibrations. The experimental approach developed here will be used for investigation of the corresponding receptivity problem.

Place, publisher, year, edition, pages
American Institute of Physics Inc. , 2018.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-247077DOI: 10.1063/1.5065230ISI: 000481675800152Scopus ID: 2-s2.0-85056347707ISBN: 9780735417472 (print)OAI: oai:DiVA.org:kth-247077DiVA, id: diva2:1313442
Conference
19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, 13 August 2018 through 19 August 2018
Note

QC 20190503

Available from: 2019-05-03 Created: 2019-05-03 Last updated: 2019-09-05Bibliographically approved

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Örlü, RamisHanifi, Ardeshir

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