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This paper investigates the accuracy of implicit Large Eddy Simulation in the prediction of acoustic phenomena associated with pressure fluctuations within a supersonic turbulent boundary layer. We assess the accuracy of implicit Large Eddy Simulation against Direct Numerical Simulation and experiments for attached turbulent supersonic flow with zero-pressure gradient, and further analyze and discuss the effects of turbulent boundary layer pressure fluctuations on acoustic loading both at the high and low frequency regimes. The results of high-order variants of the simulations show good agreement with theoretical models, experiments, as well as previously published Direct Numerical Simulations.
|Journal||Physics of Fluids|
|Publication status||Published - 17 Apr 2017|
- large eddy simulation
- acoustic phenomena
- supersonic turbulent boundary layer
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- 1 Finished
Shock-induced Turbulence and Acoustic Loading on Aerospace Structures
Drikakis, D. & Kokkinakis, I.
Air Force Office of Scientific Research AFOSR (the)
30/09/15 → 29/09/17