Control of Boundary Layer Separation on Flapped Airfoil with Low-Profile Vortex Generator
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F09%3A00332938" target="_blank" >RIV/61388998:_____/09:00332938 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Control of Boundary Layer Separation on Flapped Airfoil with Low-Profile Vortex Generator
Original language description
The paper focuses on reducing eventually removing flow separation, which is occurred on deflected flap, with vortex generators. Airfoil NACA 63A421 with simple flap and low profile vane-type vortex generators were used. The investigation was carried outusing experimental and numerical method. The flow over the airfoil was visualized by tuft filaments technique in closed circuit wind tunnel for two flap deflections and four angles of attack. Two size and two different shapes of vortex generators were tested. The data from numerical simulation of flapped airfoil without VG's control were used for vortex generator designing.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2009
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Experimental Fluid Mechanics 2009
ISBN
978-80-7372-538-9
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
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Publisher name
Technical University of Liberec
Place of publication
Liberec
Event location
Liberec
Event date
Nov 25, 2009
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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