Aeroacoustical Investigation of NACA 0012 Airfoil Using CFD
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F19%3A00336560" target="_blank" >RIV/68407700:21220/19:00336560 - 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
Aeroacoustical Investigation of NACA 0012 Airfoil Using CFD
Original language description
This paper presents an investigation of a two-dimensional approach to numerical prediction of aerodynamical noise generated by NACA 0012 airfoil. The aim of this paper is to investigate this approach as a simple prediction method for aerodynamical noise generated by two-dimensional bodies. The numerical simulation was performed by the commercial software (Ansys Fluent) using unsteady Reynolds-averaged Navier-Stokes (URANS) equations for a flow solution and Ffowcs-Williams and Hawkings (FW-H) analogy for an acoustic solution. The obtained results were compared to available published experimental results
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20302 - Applied mechanics
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Studentská tvůrčí činnost 2019
ISBN
978-80-01-06564-8
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
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Publisher name
České vysoké učení technické v Praze, Fakulta strojní
Place of publication
Praha
Event location
Technická 4, Praha 6
Event date
Apr 9, 2019
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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