Relationship between vortex and sound in under-expanded supersonic impinging jets
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Publication:2884022
DOI10.1002/FLD.2596zbMath1394.76116OpenAlexW1638644281MaRDI QIDQ2884022
Zhao-Hui Yao, Xi-Wen Zhang, Xinguang Cui
Publication date: 14 May 2012
Published in: International Journal for Numerical Methods in Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/fld.2596
shock wavelarge-eddy simulationthird-order Runge-Kutta methodFavre-filtered Navier-Stokes equationthird-order upwind compact difference
Finite difference methods applied to problems in fluid mechanics (76M20) Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20)
Cites Work
- Time-dependent boundary conditions for hyperbolic systems. II
- Time dependent boundary conditions for hyperbolic systems
- A new way for constructing high accuracy shock-capturing generalized compact difference schemes.
- Approximate wall boundary conditions in the large eddy simulation of high Reynolds number flow
- Mechanisms for generating coherent packets of hairpin vortices in channel flow
- Oscillations of a moderately underexpanded choked jet impinging upon a flat plate
- Flow field and noise characteristics of a supersonic impinging jet
- Numerical simulation of two‐dimensional laminar slot‐jet impingement flows confined by a parallel wall
- Simulation of an impinging jet in a crossflow using a Reynolds stress transport model
- An experimental study of the oscillatory flow structure of tone-producing supersonic impinging jets
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