Výsledky vyhledávání - "Massimiliano Di Giulio"

Evaluation of the noise impact of flap-tip fences installed on laminar wings

Autor: Thomas Ahlefeldt, Alessandro Di Marco, Lorenzo Burghignoli, Francesco Centracchio, Stephan Adden, Arne Henning, Massimiliano Di Giulio, Roberto Camussi

Publikováno v: CEAS Aeronautical Journal. 11:849-872

The aeroacoustics of laminar wings and the noise abatement provided by flap-tip fences are studied experimentally on a scaled model installed in the closed test section of a subsonic wind tunnel. The activity has been developed under an international

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::354638da9734932aeb936cf85d8504ff
https://doi.org/10.1007/s13272-020-00454-x

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Aeroacoustic Wind Tunnel Testing of a 1:6.5 Model Scale Innovative Regional Turboprop

Autor: Riccardo Gemma, Jürg Müller, Massimiliano Di Giulio, Lorenzo Burghignoli, Roberto Camussi, Stephan Adden, Peter Aschwanden, Stefan Haxter, Francesco Amoroso, Francesco Centracchio, Alessandro Di Marco, Tobias Berkefeld, Michele Averardo

Publikováno v: 2018 AIAA/CEAS Aeroacoustics Conference.

The aeroacoustics of an innovative regional turboprop aircraft is experimentally investigated on a 6.5 scaled model. The measurement campaign was performed at the RUAG Large Subsonic Wind Tunnel in Emmen. The model was mounted on a ceiling strut in t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e2305a02a74ee2a4933e653664495b45
https://doi.org/10.2514/6.2018-3601

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Aircraft composite structures modeling and vibro-acoustic optimization analysis

Autor: Ernesto Monaco, Francesco Amoroso, Massimiliano Di Giulio, Antonio Paonessa

Publikováno v: Scopus-Elsevier

This paper presents activities developed by the authors within the EC funded research program named FACE (Friendly Aircraft Cabin Environment) aimed at characterising some aeronautical composite structural components from the vibro-acoustic behaviour

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6b5aa459b4bd05232bfa6eebab84a6e8
http://hdl.handle.net/11588/427056

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WENEMOR: Wind Tunnel Tests for the Evaluation of the Installation Effects of Noise Emissions of an Open Rotor Advanced Regional Aircraft

Autor: John Kennedy, Gareth J. Bennett, Massimiliano Di Giulio

Publikováno v: 19th AIAA/CEAS Aeroacoustics Conference.

This paper presents the key objectives from an European Union funded collaborative project investigating the noise installation effects for novel regional advanced aircraft concepts using Open Rotor (OR) propulsion systems. The consortium for the pro

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::27c3ecfb291821467f6f2afca3831bcf
https://doi.org/10.2514/6.2013-2092

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WIND TUNNEL MEASUREMENTS OF PRESSURE FLUCTUATIONS AND STRUCTURAL RESPONSE INDUCED BY THE TURBULENT BOUNDARY LAYER AT HIGH MACH NUMBER, PART 2: COMPARISONS BETWEEN EXPERIMENTAL AND NUMERICAL DATA FOR THE STRUCTURAL RESPONSE

Autor: Sergio De Rosa, Francesco Franco, Elena Ciappi, Francesca Magionesi, Vincenzo Quaranta, Pasquale Vitiello, Massimiliano Di Giulio

Publikováno v: NOVEM 2012 Noise and Vibration: Emerging Methods, Sorrento (Napoli)-Italia, 1-4 Aprile 2012
info:cnr-pdr/source/autori:Sergio De Rosa, Francesco Franco, Elena Ciappi, Francesca Magionesi, Vincenzo Quaranta, Pasquale Vitiello, Massimiliano Di Giulio/congresso_nome:NOVEM 2012 Noise and Vibration: Emerging Methods/congresso_luogo:Sorrento (Napoli)-Italia/congresso_data:1-4 Aprile 2012/anno:2012/pagina_da:/pagina_a:/intervallo_pagine

Measurements of the acceleration response of typical homogeneous and composite aeronautical panels with different lay-up to turbulent boundary layer excitation have been performed in a transonic wind tunnel for Mach number values ranging between 0.4

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::b65670d87e862303e42a6d3ecb5964ab
http://hdl.handle.net/11588/437977

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Vibration and Acoustic Correlation on Aircraft Fuselage Composite Stiffened Panels

Autor: Tiziano Polito, Antonio Paonessa, Massimiliano Di Giulio, Francesco Marulo

Publikováno v: 11th AIAA/CEAS Aeroacoustics Conference.

The structural dynamics and the transmission loss behaviour of composite stiffened panels specifically designed for an aircraft fuselage structure application are an important issue with regard to the noise levels transmitted inside aircraft cabin. I

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6a6139d1769b3a297d645a76dd41ba8a
https://doi.org/10.2514/6.2005-3035

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