Direct computation of the noise induced by a turbulent flow through a diaphragm in a duct at low Mach number
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Publication:416516
DOI10.1016/j.compfluid.2007.02.004zbMath1237.76170OpenAlexW2160329333MaRDI QIDQ416516
Xavier Gloerfelt, Philippe Lafon
Publication date: 10 May 2012
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2007.02.004
Finite difference methods applied to problems in fluid mechanics (76M20) Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05)
Related Items (8)
Hybrid aeroacoustic computation of a low Mach number non-isothermal shear layer ⋮ Investigation of low-dissipation monotonicity-preserving scheme for direct numerical simulation of compressible turbulent flows ⋮ Effects of freestream turbulence on separated boundary layer in a low-Re high-lift LP turbine blade ⋮ On the turbulence amplification in shock-wave/turbulent boundary layer interaction ⋮ An optimized low-dissipation monotonicity-preserving scheme for numerical simulations of high-speed turbulent flows ⋮ Turbulent boundary-layer noise: direct radiation at Mach number 0.5 ⋮ Efficient numerical simulation of aeroacoustics for low Mach number flows interacting with structures ⋮ Influence of pressure gradients on wall pressure beneath a turbulent boundary layer
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