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Simulations of CrOr and fan broadband NoisE with reduced order modelling

CORDIS provides links to public deliverables and publications of HORIZON projects.

Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Deliverables

Publications

Characterization of the pressure fluctuationswithin an airfoil boundary layer using WMLES

Author(s): Boukharfane, R., Parsani, M., Joly, L., and Bodart
Published in: Parallel CFD International conference, 2021
Publisher: Parallel CFD International conference

Numerical simulation of the broadband noise of acounter-rotative open rotor configuration using phase-lagged conditions. Part 1: initialvalidation on a single rotor case

Author(s): Fiore, M., Biochini, R., Boussuge, J.-F.,
Published in: Aerospace Europe Conference,, 2020
Publisher: Aerospace Europe Conference

Monte-carlo computation of wall-pressure spectra under turbulent boundary layers for trailing-edge noise prediction

Author(s): G. Grasso, P. Jaiswal, S. Moreau
Published in: International Conference on Noise and Vibration Engineering, 2018, Page(s) 585-600
Publisher: International Conference on Noise and Vibration Engineering

Characterization of the pressure fluctuations within a Controlled-Diffusion airfoil boundary layer at large Reynolds numbers (opens in new window)

Author(s): Radouan Boukharfane, Julien Bodart, Marc C. Jacob, Laurent Joly, Thibault Bridel-Bertomeu, Thomas Node-Langlois
Published in: 25th AIAA/CEAS Aeroacoustics Conference, 2019, ISBN 978-1-62410-588-3
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-2722

Numerical simulation of the broadband noise ofthe upstream rotor of a counter-rotative open rotor configuration using phase-lagged conditions

Author(s): Fiore, M., Boussuge, J.-F., Node-Langlois, T.,
Published in: 55th 3AF International Conference on Applied Aerodynamics, 2021
Publisher: 55th 3AF International Conference on Applied Aerodynamics

Effect of sweep angle and of wall-pressure statistics on the free-field directivity of airfoil trailing-edge noise (opens in new window)

Author(s): Gabriele Grasso, Michel Roger, Stéphane Moreau
Published in: 25th AIAA/CEAS Aeroacoustics Conference, 2019, ISBN 978-1-62410-588-3
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-2612

Analytical model of the source and radiation of sound from the trailing edge of a swept airfoil (opens in new window)

Author(s): G. Grasso, M. Roger, S. Moreau
Published in: Journal of Sound and Vibration, Issue 493, 2021, Page(s) 115838, ISSN 0022-460X
Publisher: Academic Press
DOI: 10.1016/j.jsv.2020.115838

CFD-based prediction of wall-pressure spectra under a turbulent boundary layer with adverse pressure gradient (opens in new window)

Author(s): Gabriele Grasso, Hao Wu, Susanna Orestano, Marlène Sanjosé, Stéphane Moreau, Michel Roger
Published in: CEAS Aeronautical Journal, Issue 12/1, 2021, Page(s) 125-133, ISSN 1869-5582
Publisher: Springer Science + Business Media
DOI: 10.1007/s13272-020-00484-5

Characterization of pressure fluctuations within a controlled-diffusion blade boundary layer using the equilibrium wall-modelled LES (opens in new window)

Author(s): Radouan Boukharfane, Matteo Parsani, Julien Bodart
Published in: Scientific Reports, Issue 10/1, 2020, ISSN 2045-2322
Publisher: Nature Publishing Group
DOI: 10.1038/s41598-020-69671-y

Analytical models of the wall-pressure spectrum under a turbulent boundary layer with adverse pressure gradient (opens in new window)

Author(s): G. Grasso, P. Jaiswal, H. Wu, S. Moreau, M. Roger
Published in: Journal of Fluid Mechanics, Issue 877, 2019, Page(s) 1007-1062, ISSN 0022-1120
Publisher: Cambridge University Press
DOI: 10.1017/jfm.2019.616

Numerical Simulation of a Counter-Rotative Open Rotor Using Phase-Lagged Conditions: Initial Validation on a Single Rotor Case (opens in new window)

Author(s): Maxime Fiore, Romain Biolchini
Published in: Journal of Turbomachinery, Issue 142/12, 2020, ISSN 0889-504X
Publisher: ASME
DOI: 10.1115/1.4047891

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