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Numerical Investigation of the Boundary Layer Instabilities Over a Blunt Flat Plate at Angle of Attack in Supersonic Flow

Meijering, A.(1) and Dietz, G.(2) and Hein, S. and Dallmann, U. (1996) Numerical Investigation of the Boundary Layer Instabilities Over a Blunt Flat Plate at Angle of Attack in Supersonic Flow. DLR-Interner Bericht. 223-96 A 44, 80 S.

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Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Numerical Investigation of the Boundary Layer Instabilities Over a Blunt Flat Plate at Angle of Attack in Supersonic Flow
Authors:
AuthorsInstitution or Email of Authors
Meijering, A.(1)UNSPECIFIED
Dietz, G.(2)UNSPECIFIED
Hein, S.UNSPECIFIED
Dallmann, U.UNSPECIFIED
Date:1996
Number of Pages:80
Status:Published
Keywords:Nonlocal Instability Analysis, Flat Plate in Supersonic Flow, Full Navier-Stokes Solver, Advection Upstream Splitting Method (AUSM), Bluntness Effect, Effect of Angle of Attack, Similarity Solution for Compressible Flows
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:27 Apr 2009 10:36

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