Aerofoil tones at moderate Reynolds number
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Publication:2893854
DOI10.1017/jfm.2011.465zbMath1241.76352OpenAlexW2328089404MaRDI QIDQ2893854
Christopher K. W. Tam, Hongbin Ju
Publication date: 26 June 2012
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2011.465
Related Items (6)
On the origin of quadrupole sound from a two-dimensional aerofoil trailing edge ⋮ Using steady flow analysis for noise predictions ⋮ Implementation of a stable high-order overset grid method for high-fidelity simulations ⋮ Effect of serrated trailing edges on aerofoil tonal noise ⋮ Physical processes influencing acoustic radiation from jet engine inlets ⋮ A semi-implicit immersed boundary method for simulating viscous flow-induced sound with moving boundaries
Cites Work
- Dispersion-relation-preserving finite differene schemes for computational acoustics
- A STUDY OF THE SHORT WAVE COMPONENTS IN COMPUTATIONAL ACOUSTICS
- An approximate deconvolution model for large-eddy simulation with application to incompressible wall-bounded flows
- On the three families of instability waves of high-speed jets
- Nonparallel stability of boundary-layer flows
- Boundary-layer instability noise on aerofoils
- Multi-size-mesh Multi-time-step Dispersion-relation-preserving Scheme for Multiple-scales Aeroacoustics Problems
- Numerical investigation of the tone noise mechanism over laminar airfoils
- Sources of noise in axial flow fans
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