Physical processes influencing acoustic radiation from jet engine inlets

DOI10.1017/jfm.2013.181zbMath1287.76205OpenAlexW2096926834MaRDI QIDQ5417420

Christopher K. W. Tam, Eugene W. Chien, Edmane Envia, Sarah A. Parrish

Publication date: 21 May 2014

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/b1d26c290ca4cc88e8547d50fc6e47ccf034ff02

zbMATH Keywords

acousticsaeroacoustics

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05)

Cites Work

• Development of PML absorbing boundary conditions for computational aeroacoustics: a progress review
• Dispersion-relation-preserving finite differene schemes for computational acoustics
• Aerofoil tones at moderate Reynolds number
• Wave envelope and finite element approximations for turbofan noise radiation in flight
• Computation of sound radiating from engine inlets
• Multi-size-mesh Multi-time-step Dispersion-relation-preserving Scheme for Multiple-scales Aeroacoustics Problems
• A stable, perfectly matched layer for linearized Euler equations in unsplit physical variables

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