Experimental/numerical acoustic correlation of helicopter unsteady manoeuvres

Massimo Gennaretti; Giovanni Bernardini; Sander Hartjes; Alessandro Scandroglio; Luca Riviello; Enrico Paolone

Experimental/numerical acoustic correlation of helicopter unsteady manoeuvres

Massimo Gennaretti, Giovanni Bernardini, Sander Hartjes, Alessandro Scandroglio, Luca Riviello, Enrico Paolone

Aerospace Transport & Operations

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Abstract

One of the main factors that limit public acceptance of rotorcraft is the noise emitted over densely populated areas, which prevents a wider diffusion of these vehicles capable of performing flight operations otherwise unattainable. It is the result of complex phenomena generated aerodynamically, through the main and tail rotors, as well as mechanically, by the engine and transmission system. Significant research effort is currently made for reducing rotorcraft acoustic impact, both by helicopter manufacturers and by research institutes and academia.

Original language	English
Title of host publication	42nd European Rotorcraft Forum 2016
Publisher	3AF
Pages	395-397
Number of pages	3
Volume	1
ISBN (Electronic)	9781510839144
Publication status	Published - 2016
Event	42nd European Rotorcraft Forum 2016 - Lille, France Duration: 5 Sep 2016 → 8 Sep 2016 Conference number: 42 http://erf2016.com/

Conference

Conference	42nd European Rotorcraft Forum 2016
Abbreviated title	ERF2016
Country	France
City	Lille
Period	5/09/16 → 8/09/16
Internet address	http://erf2016.com/

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title = "Experimental/numerical acoustic correlation of helicopter unsteady manoeuvres",

abstract = "One of the main factors that limit public acceptance of rotorcraft is the noise emitted over densely populated areas, which prevents a wider diffusion of these vehicles capable of performing flight operations otherwise unattainable. It is the result of complex phenomena generated aerodynamically, through the main and tail rotors, as well as mechanically, by the engine and transmission system. Significant research effort is currently made for reducing rotorcraft acoustic impact, both by helicopter manufacturers and by research institutes and academia.",

author = "Massimo Gennaretti and Giovanni Bernardini and Sander Hartjes and Alessandro Scandroglio and Luca Riviello and Enrico Paolone",

note = "Waarschijnlijk is de proceeding een misdruk. Meerdere titels komen dubbel voor in het boek; 42nd European Rotorcraft Forum 2016, ERF2016 ; Conference date: 05-09-2016 Through 08-09-2016",

year = "2016",

language = "English",

volume = "1",

pages = "395--397",

booktitle = "42nd European Rotorcraft Forum 2016",

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Experimental/numerical acoustic correlation of helicopter unsteady manoeuvres. / Gennaretti, Massimo; Bernardini, Giovanni; Hartjes, Sander; Scandroglio, Alessandro; Riviello, Luca; Paolone, Enrico.

42nd European Rotorcraft Forum 2016. Vol. 1 3AF, 2016. p. 395-397.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

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AU - Bernardini, Giovanni

AU - Hartjes, Sander

AU - Scandroglio, Alessandro

AU - Riviello, Luca

AU - Paolone, Enrico

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BT - 42nd European Rotorcraft Forum 2016

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