Conference Proceedings
Parametric study of multiple aerofoil self-noise sources using direct noise computation
Mathieu Deuse, Richard D Sandberg
American Institute of Aeronautics and Astronautics | Published : 2019
DOI: 10.2514/6.2019-2681
Abstract
Aerofoil noise is a central concern for a large range of applications, motivated both by economical and environmental interests. One major contributor to aerofoil noise is the selfnoise, defined as the noise produced by the interaction between the aerofoil blade and the pressure fluctuations in its boundary layer and wake. In the present study, the self-noise of an isolated controlled-diffusion aerofoil is investigated using direct noise computation. A highorder finite difference solver is used to conduct large eddy simulations (and one direct numerical simulation), using a new implementation of an overset grid method. The motivation is to investigate multiple sources of aerofoil self-noise ..
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Awarded by Australian Research Council
Funding Acknowledgements
The authors are grateful for the funding provided by the Australian Research Council, Discovery Project Grant #DP180100898. The first author acknowledges the University of Melbourne for funding his PhD. This work was supported by resources provided by the Pawsey Supercomputing Centre with funding from the Australian Government and the Government of Western Australia. This project was undertaken with the assistance of resources and services from the National Computational Infrastructure (NCI), which is supported by the Australian Government.