Enabling optimized disruptive airframe-propulsion integration concepts

Risultati finali

Second workshop opened to the public to present in a synthetic form the updated objectives and outcomes of the project External speakers will be invited to contribute whenever suitable The program of the workshops will be advertised early enough through the project web site and using social media see below Students will be particularly encouraged to attend the workshops and interact with the scientistsincharge of the projectRelated Tasks 12

1st public workshop

First workshop opened to the public to present in a synthetic form the updated objectives and outcomes of the project External speakers will be invited to contribute whenever suitable The program of the workshops will be advertised early enough through the project web site and using social media see below Students will be particularly encouraged to attend the workshops and interact with the scientistsincharge of the projectRelated Tasks 12

Web site (incl. intranet & link to Alfresco server)

Web site including internet and intranet sectionsThe web site aims at a broad audience including scientists but also industrial stakeholders and policymakers All the presentations and publications including those that would be in green open access following the embargo regulations of the journals will be also accessible there The public section of the web site will expose the project scope and objectives consortium composition with links to partners its achievements with all PU deliverables and executive summaries the job offers opened for this project linking to the EURAXESS web site and European Charter Code for Researchers upcoming events and public workshops etcRelated Tasks 11 12 13

Mock-ups dimensions, operating conditions, exp. results

A first public report will be produced at the end of the scalability workshop D71 recording the following data i the final dimensions of the mockups including mitigation devices span and length of the walls and wings propellers diameter and blade chord liner depth etc ii the range of operating points velocities propeller RPM relative positioning between propulsors and airframe etc and iii a firstorder estimation of the key quantities of interest TBL thickness wall pressure spectra noise emission spectra etc to be measuredsimulatedRelated Tasks 71

WP2 final public report

WP2 final public reportRelated Tasks 218

Documentation of exp. databases (without mitigation)

Documentation of experimental databases without mitigation incl CAD files inflow conditions measurement uncertainties file naming conventions etcRelated Tasks 313

WP3 final public report

WP3 final public reportRelated Tasks 313

Config. B experimental databases (without mitigation)

Configuration B experimental databases (without mitigation), constituting the baseline validation database for the simulations to be conducted in WP4.Related Task(s): 3.2.

Config. C experimental databases (without mitigation)

Configuration C experimental databases (without mitigation), constituting the baseline validation database for the simulations to be conducted in WP4.Related Task(s): 3.3.

Config. A experimental databases (without mitigation)

Configuration A experimental databases (without mitigation), constituting the baseline validation database for the simulations to be conducted in WP4.Related Task(s): 3.1.

Data Management Plan (1st revision)

Data Management Plan first revision to be issued at M3 and revised at each sixmonthly meeting of the project The purpose is to establish benchmarks to enable the validation of existing and future simulation platforms developed by the global research communityRelated Tasks 11 12 81

Pubblicazioni

"“Under expanded jet noise prediction using surrogate models based on artificial neural networks"""

Autori: Centracchio, F., Meloni, S., Jawahar, H.K., Azarpeyvand, M., Camussi, R., Iemma, U.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-3025

Investigation of Curle's Dipolar Sources on a Porous Airfoil Interacting with Incoming Turbulence

Autori: Riccardo Zamponi, Sutharsan Satcunanathan, Stephane Moreau, Matthias Meinke, Wolfgang Schroeder and Christophe F. Schram
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: American Institute of Aeronautics and Astronautics, Inc.
DOI: 10.2514/6.2022-2985

"""Fuselage scattering effects in a hovering quadcopter drone"""

Autori: Zarri, A., Dell'Erba, E., Schram, C.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-3031

Experimental analysis of the noise of small propellers subjected to non-uniform inflow

Autori: Castelucci, L. A., Venner, C. H., Santana, L. D. D
Pubblicato in: AIAA SCITECH 2023 Forum, 2023
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2023-1545

Low-order acoustic prediction tool for estimating noise emissions from distributed propeller configurations

Autori: Monteiro, F. do N., Ragni, D., Avallone, F., Sinnige T.
Pubblicato in: AIAA Aviation 2023 Forum, 2023
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2023-4180

"""A mid-to-high fidelity aerodynamic noise simulation framework for installed propeller configurations"""

Autori: Moghadam, S.A.M., Dierke, J., Mößner, M., Ewert, R., Delfts, J.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-3007

"""Experimental and Analytical Study of the Aerodynamic Noise emitted by distributed electric propulsion systems"""

Autori: Acevedo-Giraldo, D., Roger, M., Jacob, M., Bériot, H.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-2830

"""Numerical Analysis of Poro-Serrated Trailing-Edge Noise"""

Autori: Satcunanathan,S., Meinke, M., Schröder, W.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-2817

"""Wavelet-based decomposition of the tonal-broadband components of propeller noise"""

Autori: Meloni, S., de Paola, E., Grande, E., Ragni, D., Stoica, L.G., Di Marco, A., Camussi, R.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-2876

"""Annoyance Factors of a maneuvering multicopter drone"""

Autori: Gallo, E., Beaulieu, G., Schram, C.
Pubblicato in: AIAA Meeting Paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-2837

Aeropropulsive Performance Modelling of Over-The-Wing Propulsion at Incidence

Autori: Dekker, H. N.J. , Tuinstra, M., Baars, W. J., Scarano, F., & Ragni, D.
Pubblicato in: AIAA AVIATION 2023 Forum , 2023
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2023-3355

"""Simplified models for propeller potential interaction noise"""

Autori: Gallo, E., Zarri, A., Bampanis, G., Fasinella, M.C., Schram, C.
Pubblicato in: AIAA Meeting paper (28th AIAA/CEAS Aeroacustics Conference, Southampton, June 14-17, 2022), 2022
Editore: AIAA
DOI: 10.2514/6.2022-2974

Aerodynamic Interactions of Side-by-Side Rotors in Ground Proximity

Autori: Dekker, H. N. J., Ragni, D., Baars, W. J., Scarano, F., & Tuinstra, M
Pubblicato in: AIAA Journal, Numero 60(7), 2022, Pagina/e 4267-4277, ISSN 1533-385X
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.j061105

A Wavelet-based separation method for tonal and broadband components of low Reynolds-number propeller noise

Autori: Meloni, S., de Paola, E., Grande, E., Ragni, D., Stoica, L. G., Di Marco, A., Camussi, R.
Pubblicato in: Measurement Science and Technology, Numero Vol. 34, n.4, 2023, ISSN 0957-0233
Editore: Institute of Physics and the Physical Society
DOI: 10.1088/1361-6501/acb071

Experimental characterisation and data-driven modelling of unsteady wall pressure fields induced by a supersonic jet over a tangential flat plate

Autori: Meloni, S., Centracchio, F., De Paola, E., Camussi, R., & Iemma, U.
Pubblicato in: Journal of Fluid Mechanics, Numero Volume 958, 2023, Pagina/e A27, ISSN 0022-1120
Editore: Cambridge University Press
DOI: 10.1017/jfm.2023.84

"""Effect of porosity on Curle's dipolar sources on an aerofoil in turbulent flow"""

Autori: Zamponi, R., Satcunanathan, S., Moreau, S., Meinke, M., Schroeder, W. and Schram C. F.
Pubblicato in: Journal of Sound and Vibration, Numero 0022460X, 2022, ISSN 0022-460X
Editore: Academic Press
DOI: 10.1016/j.jsv.2022.117353

Direct and adjoint problems for sound propagation in non-uniform flows with lined and vibrating surfaces

Autori: Sophie Le Bras, Gwénaël Gabard, Hadrien Bériot
Pubblicato in: Journal of Fluid Mechanics, Numero Volume 953, 2022, ISSN 0022-1120
Editore: Cambridge University Press
DOI: 10.1017/jfm.2022.949

“Acoustic versus Aerodynamic Installation Effects on a Generic Propeller-Driven Flying Architecture”

Autori: Roger, M., Acevedo Giraldo, D., Jacob, M.
Pubblicato in: International Journal of Aeroacoustics, 2022, ISSN 1475-472X
Editore: Multi-Science Publishing Co. Ltd
DOI: 10.1177/1475472x221107372

"""Aeroacoustic installation effects in multi-rotorcraft: numerical investigations of a small-size drone model”"

Autori: Zarri, A., Dell’Erba, E., Munters, W. Schram, C.
Pubblicato in: Journal of Aerospace Science and Technology, Numero Vol. 128, 2022, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2022.107762

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