The 31st Internationally attended scientific conference of the military technical academy. Modern technologies in the 21st century. - Bucharest : Military technical academy, 2005
- ISBN 973-640-074-3
Rozsah stran
3.56-3.62
Poč.str.
7 s.
Akce
Internationally attended scientific conference /31./ : modern technologies in the XXI century
Datum konání
03.11.2005-04.11.2005
Místo konání
Bucharest
Země
RO - Rumunsko
Typ akce
WRD
Jazyk dok.
eng - angličtina
Země vyd.
RO - Rumunsko
Klíč. slova
aircraft icing ; ice accretion ; icing modell
Vědní obor RIV
JU - Aeronautika, aerodynamika, letadla
CEP
KSK2076106 GA AV ČR - Akademie věd
GA103/04/0970 GA ČR - Grantová agentura ČR
FT-TA/026 GA MPO - Ministerstvo průmyslu a obchodu
CEZ
AV0Z2060917 - UH-J
Anotace
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.
