LAAME-CROW

Advanced Measurement Techniques in a Low Speed CROR Wind Tunnel Test

 Coordinatore STICHTING DUITS-NEDERLANDSE WINDTUNNELS 

 Organization address address: VOORSTERWEG 31
city: Marknesse
postcode: 8316 PR

contact info
Titolo: Mr.
Nome: Oliver
Cognome: Fries
Email: send email
Telefono: +31 527248561
Fax: +31 527248582

 Nazionalità Coordinatore Netherlands [NL]
 Totale costo 947˙720 €
 EC contributo 710˙790 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-02
 Funding Scheme JTI-CS
 Anno di inizio 2015
 Periodo (anno-mese-giorno) 2015-08-01   -   2016-10-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    STICHTING DUITS-NEDERLANDSE WINDTUNNELS

 Organization address address: VOORSTERWEG 31
city: Marknesse
postcode: 8316 PR

contact info
Titolo: Mr.
Nome: Oliver
Cognome: Fries
Email: send email
Telefono: +31 527248561
Fax: +31 527248582

NL (Marknesse) coordinator 710˙790.00

Mappa


 Word cloud

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

engine       manager    cror    rotating    tunnel    configurations    model    speed    counter   

 Obiettivo del progetto (Objective)

'Tests will be performed on a full model provided with installed Counter Rotating Open Rotor (CROR) engines. The 1:7 scale model, provided by the Topic Manager, will be mounted on a dorsal sting, located at tunnel centre line. The model is provided with two powered Counter Rotating propellers which are driven by two air motors (owned by the Topic Manager). The model is basically the same as used in L-CROR CTS (JTI-CS-2012-01-SFWA-02-028). However, it will be provided with 2 new engine configurations, new model parts representative of new engine configurations, new nacelle, new pylon and new blades, airframe inflow variations. The low speed wind tunnel test is offered in the DNW-LLF (Large Low speed Facility) 8m x 6m open test section. The aim is generating high quality aerodynamic, aero-acoustic and Particle Image Velocimetry (PIV) flow field data.'

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