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Longitudinal vortices in separated turbulent flows

Schülein, Erich and Trofimov, Victor (2006) Longitudinal vortices in separated turbulent flows. DLR-Interner Bericht. DLR-IB 224-2005A17. 57 S.

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Abstract

The goal of the investigations is the study of the longitudinal vortex formation in high-speed turbulent separated flows caused by relatively small irregularities at the model leading edges or at the model surfaces. Experiments were conducted at Mach numbers 3 and 5 in the Ludwieg Tube Facility at DLR in Göttingen (RWG) with a model of a 2-D compression corner with deflection angles of 20°, 25° and 30°. The irregularities of the surface contour have been artificially simulated by very thin vortex generator strips of different shapes and thicknesses, which were located on the model surface. The dependence of the size and intensity of the observed longitudinal vortices on the introduced disturbances (thickness, shape and wavelength of the vortex generator strips) and on the flow parameters (Mach and Reynolds numbers, boundary layer thickness, compression corner angles etc.) has been shown experimentally. The possible nature of these “long-living” quasi-stationary longitudinal structures in turbulent flows is discussed.

Item URL in elib:https://elib.dlr.de/21739/
Document Type:Monograph (DLR-Interner Bericht)
Title:Longitudinal vortices in separated turbulent flows
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schülein, ErichUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Trofimov, VictorITAM NovosibirskUNSPECIFIEDUNSPECIFIED
Date:20 November 2006
Open Access:No
Number of Pages:57
Publisher:DLR Göttingen
Status:Published
Keywords:Longitudinal vortices, high-speed, turbulent, separated flows, compression corner, vortex generator, infrared thermography, oil-flow visualisation
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Schülein, Dr.rer.nat. Erich
Deposited On:05 Jan 2007
Last Modified:27 Apr 2009 04:56

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