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Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings.

Gardner, Anthony Donald (2006) Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings. DLR-Interner Bericht. IB 2006 A 32, 234 S.

Full text not available from this repository.

Abstract

This report details a series of numerical experiments designed to provide an assessment of the acceptable sting length between the model and the sting holder required to minimise sting interference for the TWG 15-degree, 25-degree and 45-degree rolling stings. Calculations were undertaken for Mach numbers of 0.50, 0.90, 1.05 and 1.63, and for model attitudes between 0 and 55 degrees. These calculations indicated that the minimum spacing varied with the Mach number and angle of attack between 1 cm and 20 cm.

Item URL in elib:https://elib.dlr.de/44435/
Document Type:Monograph (DLR-Interner Bericht)
Title:Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gardner, Anthony DonaldUNSPECIFIEDUNSPECIFIED
Date:2006
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:234
Status:Published
Keywords:CFD, TAU, support interference, TWG
HGF - Research field:Aeronautics, Space and Transport (old)
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: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Gardner, Dr.habil. Anthony
Deposited On:20 Jun 2007
Last Modified:27 Apr 2009 13:01

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