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Numerical Study of the Interaction between Shock Wave and Free Shear Layer

Tomaselli, L. (1997) Numerical Study of the Interaction between Shock Wave and Free Shear Layer. DLR-Interner Bericht. 223-97 A 17, 53 S.

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Abstract

The general purpose of this study is the development of a numerical simulation model of the reflection of shock waves at compressible shear layers and ist verification by comparison with experiment and analytical results of approximate theories. The need for such a simulation model arose from problems with the experimental investigation of plane cascades, which are usually investigated in a laterally confined free jet such that shock reflections at the jet boundary can significantly influence the aerodynamic measurements in the cascade's wake.

Item URL in elib:https://elib.dlr.de/37607/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1997,
Title:Numerical Study of the Interaction between Shock Wave and Free Shear Layer
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Tomaselli, L.UNSPECIFIEDUNSPECIFIED
Date:1997
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:53
Status:Published
Keywords:Shock wave, shear layer, supersonic flow, Navier-Stokes code
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:09

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