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Simulation of noise radiation from installed pusher propeller aircraft configurations (Section 8.3)

Yin, Jianping and Stuermer, Arne (2011) Simulation of noise radiation from installed pusher propeller aircraft configurations (Section 8.3). Journal of Sound and Vibration, 330 (2011), pp. 4975-4976. DOI: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X.

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Abstract

The aeroacoustic phenomena characteristic of a pusher-propeller configuration and their aerodynamic causes are discussed and analyzed. The work was done in the frame of the European-funded project CESAR (Cost Effective Small AiRcraft). The configuration under study is an industrially relevant design with a wing-mounted pusher propeller, which features a close coupling of the turboshaft engines exhaust nozzles and a five bladed propeller. The coupling of an Actuator Disc (TAU AD) model and unsteady free wake panel method (UPM) is employed for the computation of the propeller unsteady aerodynamic force in "pusher" installations. The Ffowcs-Williams/Hawkings (FW-H) equations based code APSIM is used to compute the sound propagation into the far field. A detailed comparison of the current fast coupling method with high-fidelity uRANS (TAU) simulation results and the differences between the two approaches are discussed. The noise reduction through a redesigned engine exhaust nozzle is presented.

Document Type:Article
Title:Simulation of noise radiation from installed pusher propeller aircraft configurations (Section 8.3)
Authors:
AuthorsInstitution or Email of Authors
Yin, Jianpingjianping.yin@dlr.de
Stuermer, Arnearne.stuermer@dlr.de
Date:24 June 2011
Journal or Publication Title:Journal of Sound and Vibration
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:330
DOI:10.1016/j.jsv.2010.06.001
Page Range:pp. 4975-4976
Editors:
EditorsEmail
Nagy, Attila BalazsUNSPECIFIED
Series Name:Aeroacoustics research in Europe: The CEAS-ASC report on 2010 highlights
ISSN:0022-460X
Status:Published
Keywords:Noise radiation, installation effect, pusher propeller, unsteady panel method (UPM), Actuator disk (TAU), FW-H APSIM
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Quiet and Comfortable Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Dr.-Ing. Jianping Yin
Deposited On:28 Sep 2011 16:16
Last Modified:07 Feb 2013 20:35

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