ACOC-TH

"Acoustic and thermal instrumentation, tests and modelling of engine surface coolers in representative aerodynamic conditions"

 Coordinatore INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES 

 Organization address address: CHAUSSEE DE WATERLOO 72
city: RHODE SAINT GENESE
postcode: 1640

contact info
Titolo: Mr.
Nome: Dirk
Cognome: De Vleeschauwer
Email: send email
Telefono: 3223599610
Fax: 3223599600

 Nazionalità Coordinatore Belgium [BE]
 Totale costo 299˙284 €
 EC contributo 224˙463 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2009-01
 Funding Scheme JTI-CS
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-01-01   -   2013-02-28

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES

 Organization address address: CHAUSSEE DE WATERLOO 72
city: RHODE SAINT GENESE
postcode: 1640

contact info
Titolo: Mr.
Nome: Dirk
Cognome: De Vleeschauwer
Email: send email
Telefono: 3223599610
Fax: 3223599600

BE (RHODE SAINT GENESE) coordinator 183˙138.00
2    UNIVERSITE LIBRE DE BRUXELLES

 Organization address address: Avenue Franklin Roosevelt 50
city: BRUXELLES
postcode: 1050

contact info
Titolo: Dr.
Nome: Patrick
Cognome: Hendrick
Email: send email
Telefono: 3226502658
Fax: 3226502710

BE (BRUXELLES) participant 41˙325.00

Mappa


 Word cloud

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

tests    thermal    aerodynamic    heat    engine    performed    surface    coolers    oil    acoustic   

 Obiettivo del progetto (Objective)

'The present proposal addresses the acoustic and thermal instrumentation, tests and modelling of engine surface coolers in representative aerodynamic conditions. In addition to aerodynamic tests already performed on surface coolers in a regional funded project, complementary tests have to be conducted to characterize these equipments from a thermal and acoustic point of view. The concerned Air Cooled Oil Cooler thermal characterization will be performed in a high speed wind tunnel, especially adapted in order to host this device and to retrieve take-off engine-like conditions. The main expected results are the quantification of heat extraction and the surface temperature maps of the heat exchanger. The contribution to the acoustic investigation is principally focused a detailed analysis of the measurements.'

Introduzione (Teaser)

Optimising heat management of aircraft turbofan oil is a complex problem both mathematically and experimentally. An EU-funded project has, however, provided solutions that will aid in the evaluation of promising technologies for the future.

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