Application of Shape based Similarity Query for Aerodynamic Optimization of Wind Tunnel Primary Nozzle

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F10%3A%230001634" target="_blank" >RIV/46747885:24210/10:#0001634 - 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
Application of Shape based Similarity Query for Aerodynamic Optimization of Wind Tunnel Primary Nozzle
Original language description
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 parts need 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)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
International Conference Experimental Fluid Mechanics 2010 Conference Proceedings
ISBN
9788073726706
ISSN
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e-ISSN
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Number of pages
852
Pages from-to
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Publisher name
Technická univerzita v Liberci
Place of publication
Technická univerzita v Liberci
Event location
Ještěd, Liberec
Event date
Jan 1, 2010
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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