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Wall Correction Methods for Dynamic Tests

Voß, R. (1998) Wall Correction Methods for Dynamic Tests. In: AGARDograph 336 Wind Tunnel Wall Corrections AGARD-AG, 336. Canada Communication Group Inc.. 9-1-9-29. ISBN 92-836-1076-8.

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Abstract

Wind tunnel wall interference in unsteady flow has not been as thoroughly investigated as it has been in steady flow. In the case of unsteady flow, the problem of wind tunnel wall interference is complicated even more by additional parameters describing the time dependent variation of the unsteady flow field. Moreover, other sources of interference such as tunnel wall reflections in the form of acoustic waves, and, as a consequence, wind tunnel resonance, play an important role as well.

Document Type:Book Section
Additional Information: LIDO-Berichtsjahr=1999,
Title:Wall Correction Methods for Dynamic Tests
Authors:
AuthorsInstitution or Email of Authors
Voß, R.UNSPECIFIED
Date:1998
Journal or Publication Title:AGARDograph 336 Wind Tunnel Wall Corrections
Refereed publication:Yes
In ISI Web of Science:No
Volume:336
Page Range:9-1-9-29
Editors:
EditorsEmail
North Atlantic Treaty Organization, UNSPECIFIED
Publisher:Canada Communication Group Inc.
Series Name:AGARD-AG
ISBN:92-836-1076-8
Status:Published
Keywords:unsteady aerodynamics, wind tunnel interface, wind tunnel wall corrections, panel methods, tunnel resonance, wind tunnel wall adaption
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 - Flexible Aircraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:25

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