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Wing airfoil rime ice accretion prediction

Result description

The paper presents the rime ice accretion prediction code. Model includes the calculation of a velocity distribution, droplet motion equations and detetrmination of a water mass flux impacting on the wing airfoil surface. Changing the airfoil shape is illustrated in compare of experimental results.

Keywords

rime ice accretionnumerical methods

The result's identifiers

Alternative languages

  • Result language

    angličtina

  • Original language name

    Wing airfoil rime ice accretion prediction

  • Original language description

    The paper presents the rime ice accretion prediction code. Model includes the calculation of a velocity distribution, droplet motion equations and detetrmination of a water mass flux impacting on the wing airfoil surface. Changing the airfoil shape is illustrated in compare of experimental results.

  • Czech name

    Modelování klasické námrazy na profilu křídla

  • Czech description

    Příspěvek popisuje modelovéní klasické námrazy. Model zahrnuje výpočet rychlostního pole, rovnice pohybu kapek a stanovení toku vody dopadající na profil křídla. Změna tvaru profilu křídla je srovnána s výsledky experimentu

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Others

  • Publication year

    2006

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Engineering mechenics 2006

  • ISBN

    80-86246-27-2

  • ISSN

  • e-ISSN

  • Number of pages

    8

  • Pages from-to

    313

  • Publisher name

    Institute of Theoretical and Applied Mechanics

  • Place of publication

    Praha

  • Event location

    Svratka

  • Event date

    May 15, 2006

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article

Basic information

Result type

D - Article in proceedings

D

CEP

JU - Aeronautics, aerodynamics, aeroplanes

Year of implementation

2006