8 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Laser equipment ASsessment for High impAct innovation in the manufactuRing European industry (LASHARE)
Date du début: 1 sept. 2013, Date de fin: 31 août 2017,
LASHARE will develop a robust assessment framework for innovative laser equipment paving the way for new manufacturing applications. It will carry out a large number of assessment experiments for a variety of laser equipment targeting strategic manufacturing areas for Europe.The Laser Equipment Assessment (LEA) will be carried out by a trio of research/supplier/user partners. Each LEA will define ...
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40
Participants partenaires
TERMINÉ
Low speed aeroacoustic test of an open rotor powered complete model (LAc-LORR OTS)
Date du début: 1 août 2015, Date de fin: 31 oct. 2016,
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 ...
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1
Participant partenaire
TERMINÉ
Advanced Measurement Techniques in a Low Speed CROR Wind Tunnel Test (LAAME-CROW)
Date du début: 1 août 2015, Date de fin: 31 oct. 2016,
"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 ...
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1
Participant partenaire
TERMINÉ
Aeroacoustic and aerodynamic wind tunnel tests at low speed for a turbofan model equipped with TPS (PLAAT)
Date du début: 1 sept. 2014, Date de fin: 31 août 2015,
"The noise shielding empennage designs for rear fuselage mounted engines are promising enough to further investigate. Significant noise reduction is one of the main goals of the Clean Sky Smart Fixed Wing Aircraft (SFWA) project.In order to determine the merits of several alternative designs, extensive wind tunnel testing with enhanced state-of-the-art measuring techniques will be performed.Tests ...
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1
Participant partenaire
TERMINÉ
European Strategic Wind Tunnels Improved Research Potential (ESWIRP)
Date du début: 1 oct. 2009, Date de fin: 30 sept. 2014,
The proposed project ESWIRP aims at enhancing the complementary research potential and service capabilities of three strategic wind tunnels in Europe both in terms of productivity and quality. The concerned wind tunnels are ONERA S1MA Modane, DNW-LLF and ETW. The main ideas leading to the proposal have been (i) the identification at European level by the aeronautical community (ACARE) of the strat ...
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3
Participants partenaires
TERMINÉ
Breakthrough Laminar Aircraft Model wind tunnel testing in Europe (BLAME)
Date du début: 16 déc. 2013, Date de fin: 15 juin 2014,
"Natural laminar flow wings will be flight tested, within a project called BLADE. A new outer laminarwing will be fitted on the legacy A340-300 wing.A large scale, low speed wind tunnel test in the DNW-LLF (Large Low speed Facility) is offered aiming at generating high quality data allowing flight clearance for the BLADE Flight Test Demonstrator providing know how for performing representative te ...
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1
Participant partenaire
TERMINÉ
Low speed aeroacoustic test of large aircraft model with open rotor engines (L-CROR OTS)
Date du début: 22 oct. 2012, Date de fin: 21 mars 2013,
"Tests will be performed on full model with installed CROR engines. The model 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 the same model as used in L-CROR-CTS (JTI-CS-2012-01-SFWA-02-028).The aim of the test is to determine the acous ...
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1
Participant partenaire
TERMINÉ
Low speed aerodynamic test of large CROR aircraft model in a closed test section (L-CROR CTS)
Date du début: 25 juin 2012, Date de fin: 24 déc. 2012,
"Tests will be performed on a full model with installed CROR engines. The model will be mounted on a ventral 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 aim of the test is to determine the aerodynamic performance and stability & control characteristics of a CROR powered ...
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