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

Publikacje

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

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

Autorzy: A. Holewa and S. Guérin
Opublikowane w: 21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, Dublin, 2017
Wydawca: CEAS

On the Azimuthal Structure of Installed Jet Noise

Autorzy: Georgy Faranosov, Victor Kopiev, Ivan V. Belyaev, Oleg Bychkov, Sergey Chernyshev
Opublikowane w: 23rd AIAA/CEAS Aeroacoustics Conference, Numer 2017-3527, 5-9 June 2017, once a year, 2017, ISBN 978-1-62410-504-3
Wydawca: 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

Autorzy: Andrej Neifeld, Roland Ewert
Opublikowane w: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Wydawca: 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

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

Statistical Inference of Liner Impedance with Shear Grazing Flow

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

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

Autorzy: R, Schnell, E. Goldhahn,M. Julian
Opublikowane w: ISABE-2019, 2019, Strona(/y) paper 24017
Wydawca: ISABE

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

Autorzy: Fulvio Sartor, Alan Burlot, Michaël Méheut
Opublikowane w: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Wydawca: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3065

CFD/CAA Analysis of UHBR Engine Tonal Noise

Autorzy: Martin Laban, Johan Kok, Harry Brouwer
Opublikowane w: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Wydawca: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3780

Method Comparison for Fan Performance in Short Intake Nacelle

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

Flutter Analysis of a Flexible UHBR Fan at Different Flight Conditions

Autorzy: Matthias Schuff, Jannik Reisberg
Opublikowane w: Volume 7C: Structures and Dynamics, 2018, Strona(/y) V07CT36A022, ISBN 978-0-7918-5115-9
Wydawca: ASME
DOI: 10.1115/GT2018-76930

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

Autorzy: C. Polacsek, A. Chelius, G. Billonnet, R. Barrier
Opublikowane w: 25th ICSV, 2018
Wydawca: ICSV

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

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

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

Autorzy: Chenyang Weng, Lars Enghardt, Friedrich Bake
Opublikowane w: 2018 AIAA/CEAS Aeroacoustics Conference, 2018, ISBN 978-1-62410-560-9
Wydawca: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3773

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