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Numerical Simulation of Fundamental Breakdown of a Laminar Boundary Layer at Mach 4.5

Adams, N.A. and Kleiser, L. (1993) Numerical Simulation of Fundamental Breakdown of a Laminar Boundary Layer at Mach 4.5. In: AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, Nov. 30 - Dec. 3, 1993. AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference, Nov. 30 - Dec. 3, 1993, Munich, Germany.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1993, pages=11,
Title:Numerical Simulation of Fundamental Breakdown of a Laminar Boundary Layer at Mach 4.5
Authors:
AuthorsInstitution or Email of Authors
Adams, N.A.UNSPECIFIED
Kleiser, L.UNSPECIFIED
Date:1993
Journal or Publication Title:AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, Nov. 30 - Dec. 3, 1993
Series Name:AIAA Paper 93-5027
Status:Published
Keywords:Boundary Layer, Compressible, Supersonic Transition, Instability, Breakdown, Oblique Waves, Fundamental, Lambda Vortices, High-Shear Layers, Y-Shear Layer, Direct Numerical Simulation
Event Title:AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference
Event Location:Munich, Germany
Event Type:international Conference
Event Dates:Nov. 30 - Dec. 3, 1993
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L TG - Querschnittstechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Theoretische Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:22 Feb 2010 14:24

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