Print Email Facebook Twitter Experimental/numerical acoustic correlation of helicopter unsteady MANOEUVRES Title Experimental/numerical acoustic correlation of helicopter unsteady MANOEUVRES Author Gennaretti, Massimo (University of Roma Tre) Bernardini, Giovanni (University of Roma Tre) Hartjes, S. (TU Delft Air Transport & Operations) Scandroglio, Alessandro (Leonardo Helicopters) Riviello, Luca (Leonardo Helicopters) Paolone, Enrico (Leonardo Helicopters) Date 2016 Abstract This paper presents one of the main objective of WP1 of Clean Sky GRC5 MANOEUVRES project, which consists in the correlation of ground noise data measured during flight tests, with numerical predictions obtained by a numerical process aimed at the analysis of the acoustic field emitted by helicopter rotors in arbitrary unsteady manoeuvring flight. Two of the helicopter trajectories analysed by the dedicated GRC5 flight test campaign are considered. Noise measurements obtained by microphones located on the ground at several positions along and aside the ground projection of the vehicle fly-over trajectory are used for correlation. The numerical simulation starts with the aeromechanic identification of the flown trajectory, followed by the corresponding prediction of aerodynamic loads, rotor noise radiation and far field atmospheric propagation. To reference this document use: http://resolver.tudelft.nl/uuid:c8454c3a-1fc8-4688-902b-46718f071b66 Publisher 3AF ISBN 9781510839144 Source 42nd European Rotorcraft Forum 2016, 1 Event 42nd European Rotorcraft Forum 2016, 2016-09-05 → 2016-09-08, Lille, France Part of collection Institutional Repository Document type conference paper Rights © 2016 Massimo Gennaretti, Giovanni Bernardini, S. Hartjes, Alessandro Scandroglio, Luca Riviello, Enrico Paolone Files PDF 20170831152906.pdf 7.89 MB Close viewer /islandora/object/uuid:c8454c3a-1fc8-4688-902b-46718f071b66/datastream/OBJ/view