Design of the Low Turbulence Wind Tunnel for Investigation of Three Dimensional Unsteady Flow

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F01%3A02098837" target="_blank" >RIV/68407700:21220/01:02098837 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Design of the Low Turbulence Wind Tunnel for Investigation of Three Dimensional Unsteady Flow
Original language description
To investigate the unsteady three-dimensional flow within cylindrical curved Channels a new special low turbulence wind tunnel has been designed and manufactured. The wind tunnel was designed to provide exact aerodynamic experiments by changing and adjusting the flow variables at the inlet section of measured channels. The purpose of the investigation is to clarify the effect of inlet flow structure (average profile of the flow field) and its turbulence parameters on the value of energy loss, caused bysecondary flow containing the pair of vortex tubes flowing out from the curved channel.
Czech name
Není k dispozici
Czech description
Není k dispozici

Project
<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2001
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Proceedings of International Conference on Advanced Engineering Design
ISBN
0-85261-731-3
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
93-98
Publisher name
University of Glasgow
Place of publication
Glasgow
Event location
Glasgow
Event date
Jun 24, 2001
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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