HomeChoose your langage
Breaking the ice !
titr_bullet.gif Aircraft icing

 VIDEO  Graph
Ice accretion on a small scale airfoil
in French Propulsion Test Center's (CEPr)
Small Icing Loop (PAG)
VIDEO
Comparison between calculated
and experimental ice shapes


When an aircraft flies through a supercooled LEXIQUEdroplets cloud, ice accretion occurs on the front parts of structure, (i.e. wing, tail plane, air intake), what can conduct to fatal accidents. In order to avoid icing, de-icing LEXIQUE or anti-icing LEXIQUE protection system are supplied by the pilot when he encounters icing conditions.

New generation of airplanes will be more sensitive to icing because airfoils will be thinner and engines will be less powerful. Consequently, improvement of protection systems are necessary. Based on icing wind tunnel test, numerical codes which can predict ice accretion are developed.



Scientific Experts :

Guffond - Direction de la Physique (DMPH) - ONERA Meudon

R - Henry - Direction de la Physique (DMPH) - ONERA Meudon



Similar activities
filet

Subsonic Aircrafts

Ground experimentation

Aerodynamics

filet


Back


| Home | Applications | Methods | Topics | Glossary | Credits |


ONERA's web site
http://www.onera.fr


Copyright ONERA - 1996-1999