elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Characteristics of 3D Instability of a 35-Degree Swept Wing to CF and TS Modes. Experiment and Theory

Borodulin, V. I. and Ivanov, A. V. and Kachanov, Y. S. and Örlü, R. and Hanifi, A. and Hein, Stefan (2016) Characteristics of 3D Instability of a 35-Degree Swept Wing to CF and TS Modes. Experiment and Theory. 18th INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH, 27. Jun. - 03. Jul. 2016, Perm, Russland. DOI: 10.1063/1.4963996

Full text not available from this repository.

Official URL: http://conf.nsc.ru/icmar2016

Abstract

An extensive experimental investigation of linear evolution of Cross-Flow (CF) and Tollmien-Schlichting (TS) modes of boundary layer oscillations on swept wing has been carried out. Stability characteristics of TS waves on swept wing were studied experimentally for the first time. The development of both modes was compared with calculations and showed to be in good agreement. The whole dataset may be used for promotion of theoretical methods of investigation of transition to turbulence on swept wings.

Item URL in elib:https://elib.dlr.de/104858/
Document Type:Conference or Workshop Item (Speech)
Additional Information:(http://scitation.aip.org/content/aip/proceeding/aipcp/1770) AIP Conference Proceedings 1770, 030054, 2016
Title:Characteristics of 3D Instability of a 35-Degree Swept Wing to CF and TS Modes. Experiment and Theory
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Borodulin, V. I.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIED
Ivanov, A. V.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIED
Kachanov, Y. S.Institute of Theoretical and Applied Mechanics, Novosibirsk, 630090, RussiaUNSPECIFIED
Örlü, R.KTH, Stockholm, SchwedenUNSPECIFIED
Hanifi, A.Aeronautical Research Institute of Sweden, Bromma, SwedenUNSPECIFIED
Hein, Stefanstefan.hein (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.1063/1.4963996
Status:Published
Keywords:laminar-turbulent transition, receptivity
Event Title:18th INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH
Event Location:Perm, Russland
Event Type:international Conference
Event Dates:27. Jun. - 03. Jul. 2016
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 - Military Technologies
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Hein, Dr.-Ing. Stefan
Deposited On:04 Jan 2017 10:38
Last Modified:27 Feb 2019 12:26

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.