ICE-TRACK

Support of Icing Tests (Runback-Ice behaviour of surfaces) and Icing Mechanisms

 Coordinatore GROUPE D'INVESTISSEMENT FINANCIER SA - GIF 

 Organization address address: AVENUE MERCATOR 3A
city: WAVRE
postcode: 1300

contact info
Titolo: Mr.
Nome: Victor
Cognome: Labin
Email: send email
Telefono: +32 10 451 457
Fax: +32 10 842 491

 Nazionalità Coordinatore Belgium [BE]
 Totale costo 229˙467 €
 EC contributo 172˙100 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-01
 Funding Scheme JTI-CS
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-11-01   -   2012-04-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    GROUPE D'INVESTISSEMENT FINANCIER SA - GIF

 Organization address address: AVENUE MERCATOR 3A
city: WAVRE
postcode: 1300

contact info
Titolo: Mr.
Nome: Victor
Cognome: Labin
Email: send email
Telefono: +32 10 451 457
Fax: +32 10 842 491

BE (WAVRE) coordinator 172˙100.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

choice    icing       water    runback    surfaces    recommendations    aircraft    intakes    air    ice   

 Obiettivo del progetto (Objective)

'The role of the project is to make an advance towards a better understanding of the runback ice formation mechanisms on aircraft wings, empennage and engine air intakes through experimental and theoretical research and to provide recommendations on the choice of efficient ice protection coatings for flying vehicles. This will help to increase safety of air flights in icing conditions. Thus, the project is aimed at collaborating its effort towards achieving the double and five-fold reduction of aircraft accident rate in the short and long terms respectively, which is one of the goals set for the year 2020 by the Strategic Research Agenda provided by the Advisory Council for Aeronautics Research in Europe (ACARE). In order to solve the abovementioned problems related to runback ice formation on the aero-dynamic surfaces and aeroengine air intakes, the team of experienced scientists will perform the following work within the frames of the ICE-TRACK project: • conduct tests of the 30 surface profile samples provided by the relevant SFWA mem-ber in artificial icing conditions in the range of outside temperatures between 0С and -30С, liquid water content 0,2-2,5 g/m3, air flow speed up to 100 m/s and with given water droplets sizes; • investigate runback ice formation processes; • measure forces of ice adhesion to the surfaces; • provide recommendations concerning the choice ofthe most promising surfaces.'

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