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A numeric far field model for support interference studies in a slotted wall wind tunnel (European Transonic Windtunnel)

Heidebrecht, Alexander (2006) A numeric far field model for support interference studies in a slotted wall wind tunnel (European Transonic Windtunnel). Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 6 / 20 (220), pp. 581-587. Professional Engineering Publishing. DOI: 10.1243/09544100JAERO92

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Official URL: http://pep.metapress.com/content/1202407811711jwm/?p=bc9cd6b11f484813becc41f67c047f4f&pi=4

Abstract

This article presents a simplified computational fluid dynamics (CFD) model of the European Transonic Windtunnel test section that represents the model support in a far field and is specifically designed for the investigation of model support effects in the transonic regime. Two parametric studies were carried out in order to determine geometric parameters of the adapted support geometry and in order to enable the simulation of actual wind tunnel experiments, by correlating the wind tunnel reference Mach number with that at the far field in the CFD computation and the effective Mach number at the model location. A comparison was done using measured calibration data from the wind tunnel.

Item URL in elib:https://elib.dlr.de/47166/
Document Type:Article
Title:A numeric far field model for support interference studies in a slotted wall wind tunnel (European Transonic Windtunnel)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Heidebrecht, AlexanderUNSPECIFIEDUNSPECIFIED
Date:December 2006
Journal or Publication Title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:6 / 20
DOI :10.1243/09544100JAERO92
Page Range:pp. 581-587
Editors:
EditorsEmail
Institution of Mechanical Engineers, UNSPECIFIED
Publisher:Professional Engineering Publishing
Series Name:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aeospace Engineering
Status:Published
Keywords:transonic wind tunnel, ETW, model support, support correction, Transsonischer Windkanal, ETW, Modellaufhängung, Windkanalkorrektur
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Configuration Design
Deposited By: Heidebrecht, Alexander
Deposited On:24 Feb 2009
Last Modified:31 Jul 2019 19:18

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