Aerodynamic and acouStic for high-by-Pass ratIo tuRbofan intEgration

Información del proyecto

ASPIRE

Identificador del acuerdo de subvención: 681856

DOI 10.3030/681856

Proyecto cerrado

Fecha de la firma de la CE 4 Diciembre 2015

Fecha de inicio 1 Enero 2016

Fecha de finalización 30 Septiembre 2018

Financiado con arreglo a

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coste total € 3 406 735,00

Aportación de la UE € 2 908 234,00

Coordinado por

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
France

Publicaciones

Conference proceedings (14)

Development of experimental method for azimuthal mode measurement for jet-wing interaction noise.

Autores: V.F. Kopiev, G.A. Faranosov, I.V. Belyaev, M.Yu. Zaytsev, O.P. Bychkov.
Publicado en: Proceedings of the 24th International Congress on Sound and Vibration, Edición 596, 23-27 July 2017, once a year, 2017, ISBN 978-1-906913-27-4
Editor: International Institute of Acoustics and Vibration

Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°.

Autores: A. Holewa and S. Guérin
Publicado en: 21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, Dublin, 2017
Editor: CEAS

On the Azimuthal Structure of Installed Jet Noise

Autores: Georgy Faranosov, Victor Kopiev, Ivan V. Belyaev, Oleg Bychkov, Sergey Chernyshev
Publicado en: 23rd AIAA/CEAS Aeroacoustics Conference, Edición 2017-3527, 5-9 June 2017, once a year, 2017, ISBN 978-1-62410-504-3
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2017-3527

Towards Forced Eddy Simulation of Airframe Induced Noise Radiation from Coherent Hydrodynamic Structures of Jet Flow

Autores: Andrej Neifeld, Roland Ewert
Publicado en: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3463

Linear stability analysis in rotating frames and its application to fan blade transition prediction

Autores: Lucas Pascal, Raphaël Barrier, Gilles Billonet, Julien Marty
Publicado en: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-4215

Statistical Inference of Liner Impedance with Shear Grazing Flow

Autores: Fabien Mery, Rémi Roncen, Estelle Piot, Frank Simon
Publicado en: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3775

Design and performance of a Low Fan-Pressure-Ratio Propulsion System

Autores: R, Schnell, E. Goldhahn,M. Julian
Publicado en: ISABE-2019, 2019, Página(s) paper 24017
Editor: ISABE

Numerical Simulations of Fan/Airframe Interaction with Active Flow-Control

Autores: Fulvio Sartor, Alan Burlot, Michaël Méheut
Publicado en: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3065

CFD/CAA Analysis of UHBR Engine Tonal Noise

Autores: Martin Laban, Johan Kok, Harry Brouwer
Publicado en: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3780

Method Comparison for Fan Performance in Short Intake Nacelle

Autores: Alan Burlot, Fulvio Sartor, Maxime Vergez, Michaël Méheut, Raphaël Barrier
Publicado en: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-4204

Flutter Analysis of a Flexible UHBR Fan at Different Flight Conditions

Autores: Matthias Schuff, Jannik Reisberg
Publicado en: Volume 7C: Structures and Dynamics, 2018, Página(s) V07CT36A022, ISBN 978-0-7918-5115-9
Editor: ASME
DOI: 10.1115/GT2018-76930

Tone noise prediction of a full-scale UHBR engine with/without inflow distorsion

Autores: C. Polacsek, A. Chelius, G. Billonnet, R. Barrier
Publicado en: 25th ICSV, 2018
Editor: ICSV

Enhanced Fan Broadband Noise Prediction Based on a 2D Synthetic Turbulence Method

Autores: Carolin A. Kissner, Attila M. Wohlbrandt, Sebastien Guerin
Publicado en: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3452

Comparison of Non-Modal-Based and Modal-Based Impedance Eduction Techniques

Autores: Chenyang Weng, Lars Enghardt, Friedrich Bake
Publicado en: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3773