In-Flight Ice Accretion Prediction Code
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F10%3A00428641" target="_blank" >RIV/60162694:G43__/10:00428641 - 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
In-Flight Ice Accretion Prediction Code
Original language description
The phenomenon of in-flight icing may affect all types of aircraft. The paper deals with the development of the computational wing airfoil ice accretion prediction code Ice. Presented code versions enable computational rime ice and glaze ice accretion prediction on single and multi-element airfoils in acceptable time of solution. There are presented results of rime ice and glaze ice accretion predictions and compared with current ice accretion prediction codes. Various cases of predicted ice shapes areshown in dependence of air temperature. The latest Ice code version enables to solve system of several airfoils. The example of ice prediction on the wing airfoil with a slotted flap is shown for two angles of deflection.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
<a href="/en/project/GAP101%2F10%2F0257" target="_blank" >GAP101/10/0257: Influence of Heat Transfer on Laminar-Turbulent Transition</a><br>
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
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
INCAS BOULETIN
ISSN
2066-8201
e-ISSN
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Volume of the periodical
2
Issue of the periodical within the volume
4
Country of publishing house
RO - ROMANIA
Number of pages
8
Pages from-to
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UT code for WoS article
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EID of the result in the Scopus database
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