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

Pubblicazioni

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

Autori: V.F. Kopiev, G.A. Faranosov, I.V. Belyaev, M.Yu. Zaytsev, O.P. Bychkov.
Pubblicato in: Proceedings of the 24th International Congress on Sound and Vibration, Numero 596, 23-27 July 2017, once a year, 2017, ISBN 978-1-906913-27-4
Editore: 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°.

Autori: A. Holewa and S. Guérin
Pubblicato in: 21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, Dublin, 2017
Editore: CEAS

On the Azimuthal Structure of Installed Jet Noise

Autori: Georgy Faranosov, Victor Kopiev, Ivan V. Belyaev, Oleg Bychkov, Sergey Chernyshev
Pubblicato in: 23rd AIAA/CEAS Aeroacoustics Conference, Numero 2017-3527, 5-9 June 2017, once a year, 2017, ISBN 978-1-62410-504-3
Editore: 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

Autori: Andrej Neifeld, Roland Ewert
Pubblicato in: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editore: 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

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

Statistical Inference of Liner Impedance with Shear Grazing Flow

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

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

Autori: R, Schnell, E. Goldhahn,M. Julian
Pubblicato in: ISABE-2019, 2019, Pagina/e paper 24017
Editore: ISABE

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

Autori: Fulvio Sartor, Alan Burlot, Michaël Méheut
Pubblicato in: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3065

CFD/CAA Analysis of UHBR Engine Tonal Noise

Autori: Martin Laban, Johan Kok, Harry Brouwer
Pubblicato in: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3780

Method Comparison for Fan Performance in Short Intake Nacelle

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

Flutter Analysis of a Flexible UHBR Fan at Different Flight Conditions

Autori: Matthias Schuff, Jannik Reisberg
Pubblicato in: Volume 7C: Structures and Dynamics, 2018, Pagina/e V07CT36A022, ISBN 978-0-7918-5115-9
Editore: ASME
DOI: 10.1115/GT2018-76930

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

Autori: C. Polacsek, A. Chelius, G. Billonnet, R. Barrier
Pubblicato in: 25th ICSV, 2018
Editore: ICSV

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

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

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

Autori: Chenyang Weng, Lars Enghardt, Friedrich Bake
Pubblicato in: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3773

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