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Examination of the Influence of Flow Speed on the Coherence Lengths in Turbulent Boundary Layers at High Subsonic Mach Numbers

Haxter, Stefan and Ehrenfried, Klaus and Kröber, Stefan (2014) Examination of the Influence of Flow Speed on the Coherence Lengths in Turbulent Boundary Layers at High Subsonic Mach Numbers. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag, Cham Heidelberg New York Dordrecht London. pp. 619-627. doi: 10.1007/978-3-319-03158-3_63. ISBN 978-3-319-03157-6. ISSN 1612-2909.

Full text not available from this repository.

Official URL: http://link.springer.com/chapter/10.1007/978-3-319-03158-3_63

Abstract

Wind tunnel measurements of wall pressure fluctuation were conducted at high subsonic Mach number. The data was analyzed in order to calculate the spatial decay of coherence of turbulent structures in the turbulent boundary layer as a function of the Strouhal number. The decay parameter determined from the measurements was compared with the predictions from the coherence length model of Efimtsov. The Mach number was varied in order to investigate the influence of a change in flow speed on the decay parameter for various Strouhal numbers.

Item URL in elib:https://elib.dlr.de/78724/
Document Type:Contribution to a Collection
Additional Information:DOI: 10.1007/978-3-319-03158-3_63, Online ISBN: 978-3-319-03158-3, ISSN 1860-0824 (electronic), Library of Congress Control Number: 2013957123
Title:Examination of the Influence of Flow Speed on the Coherence Lengths in Turbulent Boundary Layers at High Subsonic Mach Numbers
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Haxter, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ehrenfried, KlausUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kröber, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2014
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics IX
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:124
DOI:10.1007/978-3-319-03158-3_63
Page Range:pp. 619-627
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasDLRUNSPECIFIEDUNSPECIFIED
Heller, GerdAirbus DeutschlandUNSPECIFIEDUNSPECIFIED
Kreplin, Hans-PeterDLRUNSPECIFIEDUNSPECIFIED
Nitsche, WolfgangTU-BerlinUNSPECIFIEDUNSPECIFIED
Krämer, EwaldUni StuttgartUNSPECIFIEDUNSPECIFIED
Rist, UlrichUni StuttgartUNSPECIFIEDUNSPECIFIED
Publisher:Springer Verlag, Cham Heidelberg New York Dordrecht London
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-03157-6
Status:Published
Keywords:wind tunnel test, coherence length, corcos model, efimtsov model, variation of speed number, coherent structure decay
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Institute of Aerodynamics and Flow Technology > Fluid Systems
Deposited By: Micknaus, Ilka
Deposited On:31 Mar 2014 14:53
Last Modified:18 Mar 2024 12:03

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