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.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/39075/

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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Meijering, A.(1)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Dietz, G.(2)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Hein, S.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Dallmann, U.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1996

Open Access:

Number of Pages:

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:

DLR-Beauftragter, elib

Deposited On:

03 Apr 2006

Last Modified:

27 Apr 2009 10:36

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