Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones
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Publication:3557109
DOI10.1063/1.2033909zbMath1187.76309OpenAlexW2076865829MaRDI QIDQ3557109
Publication date: 22 April 2010
Published in: Physics of Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1063/1.2033909
Navier-Stokes equationsdispersion relationssupersonic flowRunge-Kutta methodsMach numberjetsflow simulationflow instabilityaeroacousticsnozzlesconfined flowshear turbulenceshock wave effects
Related Items
Numerical study of screech generation in a planar supersonic jet ⋮ Numerical simulation of the three-dimensional screech phenomenon from a circular jet ⋮ Investigation on the Source Locations of Axisymmetric Screech Tones Utilizing Data from Numerical Simulation ⋮ Numerical prediction of supersonic jet screech frequency ⋮ Absorbing boundary conditions for nonlinear Euler and Navier-Stokes equations based on the perfectly matched layer technique ⋮ Assessment of upwind/symmetric WENO schemes for direct numerical simulation of screech tone in supersonic jet ⋮ Acoustic feedback loops for screech tones of underexpanded free round jets at different modes
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