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Eulerlösungen mittels Chimeratechnik für instationäre kompressible Strömungen

Kern, V. (2000) Eulerlösungen mittels Chimeratechnik für instationäre kompressible Strömungen. Dissertation. DLR-Forschungsbericht. 2000-41, 190 S.

Full text not available from this repository.

Abstract

Relative motion of two or more bodies to each other is an unsteady problem of fluid dynamics. The area of the solution is discretised by several gridblocks which overlap. This technique is called chimeratechnique. For numerical solution of the two-dimensional Euler equations an Upwind-scheme is used. The grids, which undergo rigid-body motions, are created by Poisson mesh generator. First, basic research on shocks in the overlaping region is done. The one-block solution is the reference. The pressure-, lift- and moment-distributions are compared for both cases. Finally a separation of two bodies of a hypersonic vehicle and the passing of two bodies (NACA 0012-airfoils) in a tunnel are calculated.

Item URL in elib:https://elib.dlr.de/14263/
Document Type:Monograph (DLR-Forschungsbericht, Dissertation)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Eulerlösungen mittels Chimeratechnik für instationäre kompressible Strömungen
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kern, V.UNSPECIFIEDUNSPECIFIED
Date:2000
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:190
Status:Published
Keywords:Unsteady Aerodynamics, Eulersolutions, Chimeratechnique
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:37

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