Wing airfoil ice accretion model
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F67985874%3A_____%2F05%3A00028068" target="_blank" >RIV/67985874:_____/05:00028068 - 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
Wing airfoil ice accretion model
Original language description
The paper reviews the first period of a wing airfoil ice accretion theoretical solution. The ice accretion model includes the calculation of a velocity distribution round a wing airfoil. The resulting flow field is used to the aerodynamic forces acting on water droplets determination. The set of differential eyuations describing particle trajectories through the local flow field is derived from the spherical shape droplet motion equations. Results of the droplet trajectories solution are used for the water mass flux impacting on the wing airfoil surface.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
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
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2005
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
The 31st Internationally attended scientific conference of the military technical academy. Modern technologies in the 21st century
ISBN
973-640-074-3
ISSN
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e-ISSN
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Number of pages
7
Pages from-to
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Publisher name
Military technical academy
Place of publication
Bucharest
Event location
Bucharest
Event date
Nov 3, 2005
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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