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Numerische Untersuchungen einer Adaptiven Wand am Transsonischen Windkanal Göttingen

Weiand, Peter (2015) Numerische Untersuchungen einer Adaptiven Wand am Transsonischen Windkanal Göttingen. Master's, FH Aachen University of Applied Sciences.

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Abstract

The subject of this investigation is a simulation of the adaptive wall section of the transonic wind tunnel in Gottingen by computational fluid dynamics. A method for wall adaption of closed tunnel sections for 2D-measurements by Amecke is applied. This investigation uses an existing process chain in the numerical environment of the DLR TAU-code. The measurement series which was examined was taken in the Transonic Wind Tunnel Gottingen at Mach numbers between 0.75 and 0.85. In the process the wall boundary layer of the empty tunnel as well as the pressure distribution of a NACA0010 airfoil had been investigated. The wall adaption method is used iteratively. The results of the simulations at transonic speeds give information about the convergence behavior of the wall adaption which is based on the potential theory. It was observed, that at Mach numbers higher than 0.75 a greater number of adaption steps is required in order to minimize the interference. The measured and calculated pressure distributions show a very good agreement. Fluid phenomena at Mach numbers of 0.85 require the use of a diffusor which was not implemented for the fully subsonic computations. Further investigations show influences due to a gap between the sidewall and the airfoil on the pressure distribution and the adaption. The possibility to perform a numerical simulation of a static experiment in the Transonic Wind Tunnel by taking into account the full geometry of the measuring section could be proven for this procedure.

Item URL in elib:https://elib.dlr.de/96375/
Document Type:Thesis (Master's)
Additional Information:Erstprüfer: Prof. Dipl.-Ing. J.-Michael Bauschat Zweitprüfer: Dr. Anthony D. Gardner
Title:Numerische Untersuchungen einer Adaptiven Wand am Transsonischen Windkanal Göttingen
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Weiand, PeterDLR, AS-HELUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:91
Status:Published
Keywords:Wind tunnel, wall adaptation, wall interference, numerical simulation, DLR-TAU
Institution:FH Aachen University of Applied Sciences
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Micknaus, Ilka
Deposited On:04 Jun 2015 16:18
Last Modified:31 Jul 2019 19:53

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