Investigation on the Source Locations of Axisymmetric Screech Tones Utilizing Data from Numerical Simulation

DOI10.1142/S2591728518500585OpenAlexW2898384774MaRDI QIDQ6120494

Unnamed Author, Duck Joo Lee

Publication date: 25 March 2024

Published in: Journal of Theoretical and Computational Acoustics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s2591728518500585

zbMATH Keywords

feedbackcompact schemesupersonic jetscreech toneshock cell

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05)

Cites Work

• Unnamed Item
• Dispersion-relation-preserving finite differene schemes for computational acoustics
• Compact finite difference schemes with spectral-like resolution
• Numerical simulation of evolution of helical-vortex instability in a fluid layer heated from below
• Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones
• Optimized compact finite difference schemes with maximum resolution
• Use of Linearized Euler Equations for Supersonic Jet Noise Prediction
• A NOTE ON PRANDTL'S FORMULA FOR THE WAVE-LENGTH OF A SUPERSONIC GAS JET

This page was built for publication: Investigation on the Source Locations of Axisymmetric Screech Tones Utilizing Data from Numerical Simulation