Computation of the Unsteady Flow Around Vibrating Structures for Aeroelastic Applications.

Carstens, V. (1997) Computation of the Unsteady Flow Around Vibrating Structures for Aeroelastic Applications. Vortrag am Laboratoire de Thermique Appliquee et de Turbomachines der EPF Lausanne, Lausanne, Schweiz, 5.5.97.

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Abstract

The determination of the aeroelastic stability of an airfoil or an assembly of turbomachinery is strongly influenced by the level of accuracy of the measured or predicted aerodynamic loads. For this reason, the unsteady lift and moment coefficients are more and more frequently computed by highly developed CFD methods which are able to take into account complex flow geometries as well as basic physical flow effects such as compressibility and viscosity.

Item URL in elib:

https://elib.dlr.de/39820/

Document Type:

Conference or Workshop Item (Speech)

Additional Information:

LIDO-Berichtsjahr=1997,

Title:

Computation of the Unsteady Flow Around Vibrating Structures for Aeroelastic Applications.

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Carstens, V.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1997

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

transonic flow, unsteady aerodynamics, oscillating cascades, deforming grids

Event Title:

Vortrag am Laboratoire de Thermique Appliquee et de Turbomachines der EPF Lausanne, Lausanne, Schweiz, 5.5.97

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:

Göttingen

Institutes and Institutions:

Institute of Aeroelasticity

Deposited By:

DLR-Beauftragter, elib

Deposited On:

02 Apr 2006

Last Modified:

27 Apr 2009 10:55

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