The Experimental and Numerical Investigation of the Flowfield Downstream the Gurney Flap
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F00%3A02034720" target="_blank" >RIV/68407700:21220/00:02034720 - 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
The Experimental and Numerical Investigation of the Flowfield Downstream the Gurney Flap
Original language description
The presented work is based on a complex investigation of the NACA 23012 airfoil equipped with the Gurney flap. The mechanism of the vortex shedding in the wake structure downstream the Gurney flap is shown. PIV tests, force measurements, and numerical computations have also been performed.
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
<a href="/en/project/LN00B073" target="_blank" >LN00B073: Josef Božek Research Center of Engine and Automotive Engineering</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2000
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Fluid Mechanics and Thermodynamics
ISBN
80-902714-4-8
ISSN
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e-ISSN
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Number of pages
22
Pages from-to
53-74
Publisher name
Gradient
Place of publication
Praha
Event location
Praha
Event date
Jun 19, 2000
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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