Broadband noise from serrated UAS propellers: Validation of a lattice Boltzmann approach

B. G. Marinus, D. Bontea, A. Halimi, A. Pire

Onderzoeksoutput: Hoofdstuk in Boek/Rapport/CongresprocedureConferentiebijdragepeer review

Samenvatting

With the increased use on Unmanned Aerial Systems equipped with propellers and rotors, serrated edges are considered to reduce broadband noise emissions without affecting the aerodynamic performance. In this context, a full sensitivity study is performed to assess the independence of the solution to the space (voxel resolution) and time discretization (time step, sampling rate and number of revolutions). This way, the computational tools are validated for the prediction of both the aerodynamic and aeroacoustic performance. The results show there is enough confidence in such models for them to be used to optimize serrated propeller geometries and achieve a reduction of the noise emissions by 3~10dB in the 1000Hz to 10.000Hz range.

Originele taal-2Engels
TitelProceedings of ISMA 2018 - International Conference on Noise and Vibration Engineering and USD 2018 - International Conference on Uncertainty in Structural Dynamics
RedacteurenD. Moens, W. Desmet, B. Pluymers, W. Rottiers
UitgeverijKU Leuven - Departement Werktuigkunde
Pagina's613-620
Aantal pagina's8
ISBN van elektronische versie9789073802995
StatusGepubliceerd - 2018
Evenement28th International Conference on Noise and Vibration Engineering, ISMA 2018 and 7th International Conference on Uncertainty in Structural Dynamics, USD 2018 - Leuven, België
Duur: 17 sep. 201819 sep. 2018

Publicatie series

NaamProceedings of ISMA 2018 - International Conference on Noise and Vibration Engineering and USD 2018 - International Conference on Uncertainty in Structural Dynamics

Congres

Congres28th International Conference on Noise and Vibration Engineering, ISMA 2018 and 7th International Conference on Uncertainty in Structural Dynamics, USD 2018
Land/RegioBelgië
StadLeuven
Periode17/09/1819/09/18

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