On jet instability modes of a subsonic Hartmann whistle

DOI10.1007/S12046-018-0921-ZzbMath1402.76116OpenAlexW2883527671MaRDI QIDQ1628277

Y. Aharonov

Publication date: 4 December 2018

Published in: Sādhanā (Search for Journal in Brave)

Full work available at URL: https://www.ias.ac.in/describe/article/sadh/043/09/0140

zbMATH Keywords

subsonic flowlarge-eddy simulationHartmann whistlejet-instability mode

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05)

Cites Work

• Computation of a high Reynolds number jet and its radiated noise using large eddy simulation based on explicit filtering
• Boundary conditions for direct simulations of compressible viscous flows
• Compact finite difference schemes with spectral-like resolution
• Compact implicit MacCormack-type schemes with high accuracy
• Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
• An explicit filtering method for large eddy simulation of compressible flows

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