Uncertainty Quantification in Direct Noise Computations of Cavity Feedback

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Image: IAG, University of Stuttgart

In order to quantify the uncertainty due to stochastic input in computer fluid dynamic simulations, researchers from the Institute of Aerodynamics and Gas Dynamics developed an Uncertainty Quantification framework and applied it to direct noise computations of aeroacoustic cavity flows. Simulations have been performed with the discontinuous Galerkin spectral element method on HLRS's Hazel Hen system. The aim of this investigation is to gain insight into the sensitivity of uncertain input with respect to the acoustic results and to get a reliable comparison between numerical and experimental results.

Read the complete user research report at the Gauss Centre for Supercomputing.

Principal Investigators 

Andrea Beck1, Claus-Dieter Munz1, Christian Rohde2

1 Institute of Aerodynamics and Gas Dynamics, University of Stuttgart
2 Institute of Applied Analysis and Numerical Simulation, University of Stuttgart