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Excitation of 3D TS-waves in a swept-wing boundary layer by surface vibrations and freestream vortices

Borodulin, V. I. and Ivanov, A. V. and Kachanov, Y. S. and Mischenko, D. A. and Örlü, R. and Hanifi, Ardeshir and Hein, Stefan (2018) Excitation of 3D TS-waves in a swept-wing boundary layer by surface vibrations and freestream vortices. In: AIP Conference Proceedings, 2027 (030136). 19th International Conference on the Methods of Aerophysical Research (ICMAR), 2018-08-13 - 2018-08-19, Novosibirsk, Russia. doi: 10.1063/1.5065230.

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Official URL: https://doi.org/10.1063/1.5065230

Abstract

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.

Item URL in elib:https://elib.dlr.de/118640/
Document Type:Conference or Workshop Item (Speech)
Title:Excitation of 3D TS-waves in a swept-wing boundary layer by surface vibrations and freestream vortices
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Borodulin, V. I.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIEDUNSPECIFIED
Ivanov, A. V.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIEDUNSPECIFIED
Kachanov, Y. S.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIEDUNSPECIFIED
Mischenko, D. A.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIEDUNSPECIFIED
Örlü, R.KTH, Stockholm, SchwedenUNSPECIFIEDUNSPECIFIED
Hanifi, ArdeshirKTH StockholmUNSPECIFIEDUNSPECIFIED
Hein, StefanDLRUNSPECIFIEDUNSPECIFIED
Date:2 November 2018
Journal or Publication Title:AIP Conference Proceedings
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:2027
DOI:10.1063/1.5065230
Status:Published
Keywords:laminar-turbulent transition, three-dimensional boundary layer, EU project RECEPT
Event Title:19th International Conference on the Methods of Aerophysical Research (ICMAR)
Event Location:Novosibirsk, Russia
Event Type:international Conference
Event Start Date:13 August 2018
Event End Date:19 August 2018
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Hein, Dr.-Ing. Stefan
Deposited On:28 Sep 2018 16:44
Last Modified:24 Apr 2024 20:22

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