Aerodynamic degradation of iced airfoils ? experiments and CFD simulations
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F67985874%3A_____%2F09%3A00328340" target="_blank" >RIV/67985874:_____/09:00328340 - 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
Aerodynamic degradation of iced airfoils ? experiments and CFD simulations
Original language description
The phenomenon of in-flight icing may affect all types of aircraft. Presence of ice on wings can lead to a number of aerodynamic degradation problems. The in-house ice accretion prediction code R-ICE using 2-D panel method was developed. The CFD simulation with the software ANSYS CFX 11.0 was used to simulate flow around iced airfoils NACA 0012. These airfoils were experimentally investigated in a wind tunnel. The paper presents a comparison of lift and drag coefficients experimentally observed and numerically simulated.
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
Proceedings of the ASME 2009 Fluids Engineering Division Summer Meeting (FEDSM2009)
ISBN
978-0-7918-3855-6
ISSN
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e-ISSN
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Number of pages
7
Pages from-to
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Publisher name
ASME
Place of publication
Ashland
Event location
Vail
Event date
Aug 2, 2009
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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