AFRODITE

Advanced Fluid Research On Drag reduction In Turbulence Experiments

 Coordinatore KUNGLIGA TEKNISKA HOEGSKOLAN 

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 Nazionalità Coordinatore Sweden [SE]
 Totale costo 1˙418˙399 €
 EC contributo 1˙418˙399 €
 Programma FP7-IDEAS-ERC
Specific programme: "Ideas" implementing the Seventh Framework Programme of the European Community for research, technological development and demonstration activities (2007 to 2013)
 Code Call ERC-2010-StG_20091028
 Funding Scheme ERC-SG
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-11-01   -   2015-10-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    KUNGLIGA TEKNISKA HOEGSKOLAN

 Organization address address: Valhallavaegen 79
city: STOCKHOLM
postcode: 10044

contact info
Titolo: Dr.
Nome: Jens Henrik Mikael
Cognome: Fransson
Email: send email
Telefono: 46702822553
Fax: 4687907654

SE (STOCKHOLM) hostInstitution 1˙418˙399.00
2    KUNGLIGA TEKNISKA HOEGSKOLAN

 Organization address address: Valhallavaegen 79
city: STOCKHOLM
postcode: 10044

contact info
Titolo: Ms.
Nome: Heide
Cognome: Hornk
Email: send email
Telefono: +46 8790 7128

SE (STOCKHOLM) hostInstitution 1˙418˙399.00

Mappa


 Word cloud

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

passive    transition    delay    afrodite    turbulence    energy    flow    roughness    offs    drag   

 Obiettivo del progetto (Objective)

'A hot topic in today's debate on global warming is drag reduction in aeronautics. The most beneficial concept for drag reduction is to maintain the major portion of the airfoil laminar. Estimations show that the potential drag reduction can be as much as 15%, which would give a significant reduction of NOx and CO emissions in the atmosphere considering that the number of aircraft take offs, only in the EU, is over 19 million per year. An important element for successful flow control, which can lead to a reduced aerodynamic drag, is enhanced physical understanding of the transition to turbulence process.

In previous wind tunnel measurements we have shown that roughness elements can be used to sensibly delay transition to turbulence. The result is revolutionary, since the common belief has been that surface roughness causes earlier transition and in turn increases the drag, and is a proof of concept of the passive control method per se. The beauty with a passive control technique is that no external energy has to be added to the flow system in order to perform the control, instead one uses the existing energy in the flow.

In this project proposal, AFRODITE, we will take this passive control method to the next level by making it twofold, more persistent and more robust. Transition prevention is the goal rather than transition delay and the method will be extended to simultaneously control separation, which is another unwanted flow phenomenon especially during airplane take offs. AFRODITE will be a catalyst for innovative research, which will lead to a cleaner sky.'

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