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Mach number effect on 3D-wave packets in subsonic flat plate boundary layer

Delfs, J. (1996) Mach number effect on 3D-wave packets in subsonic flat plate boundary layer. In: Proc. EUROMECH Colloquium 353 "Dynamics of localized disturbances in engineering flows", Karlsruhe, 1.-3.4.1996., pp. 57-58.

Full text not available from this repository.

Abstract

The effect of Mach number on the characteristics of unstable three-dimensional wave-packets is studied in the subsonic regime. Pronounced three-dimensionality starts to occur at M>0.7 for the adiabatic flat plate flow.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Mach number effect on 3D-wave packets in subsonic flat plate boundary layer
Authors:
AuthorsInstitution or Email of Authors
Delfs, J.UNSPECIFIED
Date:1996
Journal or Publication Title:Proc. EUROMECH Colloquium 353 "Dynamics of localized disturbances in engineering flows", Karlsruhe, 1.-3.4.1996.
Page Range:pp. 57-58
Status:Published
Keywords:convective instability, unstable wave packets, localized disturbances, transition in compressible boundary layer
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):L - Human Factors and Safety in Aeronautics
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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