CFD Based Aerodynamic Optimization of the Wind Tunnel Primary Nozzle

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F11%3A%230002373" target="_blank" >RIV/46747885:24210/11:#0002373 - 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
CFD Based Aerodynamic Optimization of the Wind Tunnel Primary Nozzle
Original language description
Abstract. The aerodynamic shape optimization of the supersonic flat nozzle is the aim of proposed paper. The nozzle discussed, is applied as a primary nozzle of the inlet part of supersonic wind tunnel. Supersonic nozzles of the measure area inlet partsneed to guarantee several requirements of flow properties and quality. Mach number and minimal differences between real and required velocity and turbulence profiles at the nozzle exit are the most important parameters to meet. The aerodynamic shape optimization of the flat 2D nozzle in CFD is employed to reach as uniform exit velocity profile as possible, with the mean Mach number 1.4.
Czech name
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Czech description
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Project
<a href="/en/project/GAP101%2F10%2F1709" target="_blank" >GAP101/10/1709: Nozzles and diffusers for ejectors</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
The 4th International Meeting of Advances in Thermofluids
ISBN
978-967-0194-07-3
ISSN
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e-ISSN
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Number of pages
8
Pages from-to
193-200
Publisher name
Universiti Teknologi Malaysia
Place of publication
Malaysia
Event location
Melaka, Malaysia
Event date
Oct 3, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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