Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26

Abstract This paper presents the activities performed in the GARTEUR Action Group HC/AG-26 to study the acoustic and aerodynamic characteristics of small rotor configurations, including the influence of the rotor-rotor interactions. This paper will focus on comparisons between numerical activities and wind tunnel results on a small rotor provided by DLR. The wind tunnel models included a Rotor/Rotor/Pylon in isolated, tandem and coaxial configuration. The wind tunnel experiments for acoustics were performed in DLR’s Acoustic Wind Tunnel Braunschweig (AWB) and PIV test were performed in CIRA within a joint CIRA/DLR test program. For simulations, the numerical approaches from each partner are applied. The aerodynamic simulations necessary for the aeroacoustic predictions are conducted with various fidelity numerical methods, varying from lifting line to CFD. The acoustic values on the microphone positions are evaluated using Ffowcs Williams/Hawking (FW-H) formulation by all partners. The acoustic and aerodynamic predictions are compared to test data, including performance, PIV and acoustic directivity.

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Institutions

Publication Details

Journal
CEAS Aeronautical Journal
Published
2024-11-23
DOI
https://doi.org/10.1007/s13272-024-00790-2
Citations
14
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
16.89

Funders

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article

Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26

Alex Zanotti, Claudio Testa, Francesco Caccia, A. Visingardi et al.
14 citations
CEAS Aeronautical Journal
Aerodynamics and Acoustics in Jet Flows
16.89
article

Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26

Alex Zanotti, Claudio Testa, Francesco Caccia, A. Visingardi, Junjun Yin, Giovanni Bernardini, Fabrizio De Gregorio, M. Barbarino, Manuel Keßler, Giuseppe Ceglia, Karl-Stéphane Rossignol, Gabriel Reboul, Francesco Petrosino, Luca Abergo, G. Qiao, Alberto Savino, Markus Muth, Stefano Zaghi, Caterina Poggi, George N. Barakos, Lukas Rottmann, N. Oberti, Alberto Guardone
article en
14 citations

Abstract

Abstract This paper presents the activities performed in the GARTEUR Action Group HC/AG-26 to study the acoustic and aerodynamic characteristics of small rotor configurations, including the influence of the rotor-rotor interactions. This paper will focus on comparisons between numerical activities and wind tunnel results on a small rotor provided by DLR. The wind tunnel models included a Rotor/Rotor/Pylon in isolated, tandem and coaxial configuration. The wind tunnel experiments for acoustics were performed in DLR’s Acoustic Wind Tunnel Braunschweig (AWB) and PIV test were performed in CIRA within a joint CIRA/DLR test program. For simulations, the numerical approaches from each partner are applied. The aerodynamic simulations necessary for the aeroacoustic predictions are conducted with various fidelity numerical methods, varying from lifting line to CFD. The acoustic values on the microphone positions are evaluated using Ffowcs Williams/Hawking (FW-H) formulation by all partners. The acoustic and aerodynamic predictions are compared to test data, including performance, PIV and acoustic directivity.

CEAS Aeronautical JournalVol. 16(4)
University of Stuttgart (DE), Roma Tre University (IT), Office National d'Études et de Recherches Aérospatiales (FR), Italian Aerospace Research Centre (IT), Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR) (DE), Institute of Marine Engineering (IT), University of Glasgow (GB), Politecnico di Milano (IT)
Bundesministerium für Wirtschaft und Technologie
Affordable and clean energy
Openalex Percentile: Top 1%
Aerodynamics and Acoustics in Jet Flows
16.89
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