Conference Presentation (Other) FZJ-2016-00807

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A direct-hybrid method for computational aeroacoustics

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2015

21st AIAA/CEAS Aeroacoustics Conference, Dallas, TXDallas, TX, USA, 22 Jun 2015 - 26 Jun 20152015-06-222015-06-26

Abstract: In this work, a highly scalable numerical method is presented that allows to compute the aerodynamic sound from the flow field for large-scale problems. The acoustic perturbation equations are solved by a high-order discontinuous Galerkin method and by using the acoustic source terms obtained from an approximate solution of the Navier-Stokes equations. Both solvers operate on the same hierarchical Cartesian grid. This direct-hybrid method is validated by monopole and pressure pulse simulations and is used to compute the aeroacoustics of a turbulent mixing layer. The results indicate that the new method is capable of efficiently predicting the acoustic field and show that it is suitable for highly parallel simulations.


Contributing Institute(s):
  1. Jülich Supercomputing Center (JSC)
  2. JARA - HPC (JARA-HPC)
Research Program(s):
  1. 511 - Computational Science and Mathematical Methods (POF3-511) (POF3-511)

Appears in the scientific report 2015
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 Record created 2016-01-21, last modified 2021-01-29



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