Obiettivo It is proposed in this research programme to optimize the pylon shape of a Counter Rotating Open Rotor (CROR) propeller and its embedded flow control system, in order to reduce the noise emission through pylon wake attenuation, by means of advanced experimental methodology, such as 3CHD-PIV, adapted to in-flight tests.It is proposed to decompose the project into subtasks of increasing complexity. Each task falls within the scope of either ISAE or AAE. Thus, ISAE and AAE offer to join their different skills to elaborate a work-plan based on well-defined responsibilities.The subtasks are summarized below:1.Optimization of the flow control device for the 2D pylon. 2.Detailed design and manufacturing of the 2D type pylon wind tunnel model and its instrumentation.3.Low speed wind tunnel tests of the 2D pylon without open rotor, in a non vibrating environment, including parametric studies on the advanced flow control devices parameters and boundary layer transition effects.4.Comparison between experimental results and numerical prediction. Analysis of the results, physical understanding and recommendation for further improvement of the concept.5.Definition of vibration environment simulators (VES), in compliance with Airbus inputs from in flight tests.6.Detailed definition and manufacturing of VES applicable to the different PIV subsystems (cameras, laser, laser sheet generation devices) as implemented in the wind tunnel.7.Characterization of the limits of the vibration spectrum supported by the PIV subsystems, beyond which vibration-induced errors on PIV measurements impose corrections on raw data or on PIV subsystems attitude.8.Definition of correction methodology to correct PIV measurements, through raw data manipulation or PIV subsystems vibration attenuation, in order to recover a non disturbed PIV measurement.9.Validation of the correctiion methodology in wind tunnel by replicating subtask 3. Campo scientifico engineering and technologyelectrical engineering, electronic engineering, information engineeringelectronic engineeringcontrol systemsengineering and technologyelectrical engineering, electronic engineering, information engineeringelectronic engineeringsensorsoptical sensorsengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftnatural sciencesphysical sciencesclassical mechanicsfluid mechanicsfluid dynamicsnatural sciencesphysical sciencesopticslaser physics Programma(i) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Argomento(i) JTI-CS-2011-2-SFWA-02-017 - Advanced Pylon Noise Reduction Design and characterisation through flight worthy PIV Invito a presentare proposte SP1-JTI-CS-2011-02 Vedi altri progetti per questo bando Meccanismo di finanziamento JTI-CS - Joint Technology Initiatives - Clean Sky Coordinatore INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE Contributo UE € 361 860,00 Indirizzo AVENUE EDOUARD BELIN 10 31055 Toulouse Francia Mostra sulla mappa Regione Occitanie Midi-Pyrénées Haute-Garonne Tipo di attività Higher or Secondary Education Establishments Contatto amministrativo Michel Tello (Mr.) Collegamenti Contatta l’organizzazione Opens in new window Sito web Opens in new window Costo totale Nessun dato Partecipanti (1) Classifica in ordine alfabetico Classifica per Contributo UE Espandi tutto Riduci tutto AEROCONSEIL SAS Francia Contributo UE € 29 000,00 Indirizzo 7 BOULEVARD HENRI ZIEGLER 31700 Blagnac Mostra sulla mappa Regione Occitanie Midi-Pyrénées Haute-Garonne Tipo di attività Private for-profit entities (excluding Higher or Secondary Education Establishments) Contatto amministrativo David Corceiro (Mr.) Collegamenti Contatta l’organizzazione Opens in new window Costo totale Nessun dato