MAWS

Modelling of Adaptive Wing Structures

 Coordinatore UNIVERSITY OF BRISTOL 

 Organization address address: TYNDALL AVENUE SENATE HOUSE
city: BRISTOL
postcode: BS8 1TH

contact info
Titolo: Mrs.
Nome: Julie
Cognome: Coombs
Email: send email
Telefono: +44 117 3315535

 Nazionalità Coordinatore United Kingdom [UK]
 Totale costo 199˙999 €
 EC contributo 149˙999 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-01
 Funding Scheme JTI-CS
 Anno di inizio 2012
 Periodo (anno-mese-giorno) 2012-01-01   -   2014-07-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITY OF BRISTOL

 Organization address address: TYNDALL AVENUE SENATE HOUSE
city: BRISTOL
postcode: BS8 1TH

contact info
Titolo: Mrs.
Nome: Julie
Cognome: Coombs
Email: send email
Telefono: +44 117 3315535

UK (BRISTOL) coordinator 149˙999.55
2    THE UNIVERSITY OF LIVERPOOL

 Organization address address: Brownlow Hill, Foundation Building 765
city: LIVERPOOL
postcode: L69 7ZX

contact info
Titolo: Ms.
Nome: Cherie
Cognome: Judge
Email: send email
Telefono: +44 151 794 8260
Fax: +44 151 794 8728

UK (LIVERPOOL) participant 0.00

Mappa


 Word cloud

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

inverse    wing    aircraft    wash    sizing    structural    structure    adaptive   

 Obiettivo del progetto (Objective)

'An adaptive wing tip concept will be developed to enable controlled wash-in and wash-out throughout the entire flight envelope. The concept, based upon adaptive stiffness structures enables control of the aeroelastic deflections, and also facilitates gust load alleviation. Furthermore, a mathematically based design tool will be developed making use of Reduced Order Models (ROMs) of the wing structure and aerodynamics such that an inverse approach can be employed to determine the required sizing of the internal aircraft structure, and also the position and sizing of any adaptive structural components and actuators. The adaptive structural concept and the inverse ROM approach will be demonstrated and evaluated on two real-size aircraft test cases.'

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