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Installation effects of a propeller mounted on a wing with Coanda flap

Dierke, Jürgen and Akkermans, Rinie A.D. and Delfs, Jan Werner (2015) Installation effects of a propeller mounted on a wing with Coanda flap. Journal of Sound and Vibration, 357, pp. 118-119. Elsevier. doi: 10.1016/j.jsv.2015.07.005. ISSN 0022-460X.

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Official URL: https://www.sciencedirect.com/science/article/pii/S0022460X15005787


The effect of installation on propeller noise was investigated. The chosen configuration consists of a nine bladed propeller in tractor configuration with a high-lift wing. Tests in the 3m acoustic wind tunnel DNW-NWB provided a valuable dataset for validation purpose of numerical codes. The CAA computations were based on a new highly efficient concept to represent the propeller as a perturbation consisting of rotating mass and momentum source distributions fed by CFD RANS data on the propeller blades, thus avoiding rotating grids. This approach will allow quantifying the installation effect at propeller driven aircraft especially to assess design changes with moderate computational effort. The validation showed good agreement. The particular tractor propeller/ high-lift wing arrangement showed excess noise due to the impingement of the propeller tip vortices on the (swept) wing nose and trailing edge flap.

Item URL in elib:https://elib.dlr.de/125645/
Document Type:Article
Title:Installation effects of a propeller mounted on a wing with Coanda flap
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Dierke, JürgenJuergen.Dierke (at) dlr.deUNSPECIFIED
Akkermans, Rinie A.D.TU BraunschweigUNSPECIFIED
Delfs, Jan WernerJan.Delfs (at) dlr.deUNSPECIFIED
Date:6 August 2015
Journal or Publication Title:Journal of Sound and Vibration
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:Yes
DOI :10.1016/j.jsv.2015.07.005
Page Range:pp. 118-119
EditorsEmailEditor's ORCID iD
Series Name:Aeroacoustics research in Europe: The CEAS-ASC report on 2014 highlights
Keywords:installed propeller noise, computational aeroacoustics, Perturbation Approach aeroacoustics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Delfs, Prof.Dr. Jan Werner
Deposited On:07 Jan 2019 16:15
Last Modified:31 Jul 2019 20:23

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