Vortex Wake of an A/C in High-Lift Configuration

Stumpf, E. (2000) Vortex Wake of an A/C in High-Lift Configuration. In: Geophysical Research Abstracts (CD-Rom). EGS, Nizza (fr), 25.-28.04.2000.

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Abstract

By means of Euler computations and Direct Numerical Simulations the vortex wake of a narrow-body wind-tunnel-model in different flight configurations has been investigated. The simulation domain covers in total 45 spans, aircraft configurations are landing, take-off and two configurations with differential flap setting. Special emphasis was put on the influence of atmospheric turbulence on the evolving wake. For the nearfield calculation up to half a span behind the model the DLR-Euler code Tau was used, the downstream flowfield was simulated with the DLR-Direct Numerical Simulation code Mesoscop.

Item URL in elib:

https://elib.dlr.de/13340/

Document Type:

Conference or Workshop Item (Paper)

Additional Information:

LIDO-Berichtsjahr=2001,

Title:

Vortex Wake of an A/C in High-Lift Configuration

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Stumpf, E.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2000

Journal or Publication Title:

Geophysical Research Abstracts (CD-Rom)

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Series Name:

Vol. 2

Status:

Published

Event Title:

EGS, Nizza (fr), 25.-28.04.2000

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):

L - Low-Emission Air Traffic (old)

Location:

Köln-Porz , Braunschweig , Göttingen

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik

Deposited By:

Grant, Claudia

Deposited On:

16 Sep 2005

Last Modified:

14 Jan 2010 20:18

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