An aeroacoustic hybrid approach for non-isothermal flows at low Mach number

DOI10.1002/fld.707zbMath1085.76555OpenAlexW2014216602MaRDI QIDQ3157207

François Golanski, J.-C. Valiere, Véronique Fortuné, Eric Lamballais, Christian Prax

Publication date: 12 January 2005

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.707

zbMATH Keywords

source termsnon-isothermal flowaeroacousticsLow Mach numberlinearized Euler's equations

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Hydro- and aero-acoustics (76Q05)

Related Items (3)

Hybrid aeroacoustic computation of a low Mach number non-isothermal shear layer ⋮ Control of the vorticity mode in the linearized Euler equations for hybrid aeroacoustic prediction ⋮ A hybrid adaptive low-Mach number/compressible method: Euler equations

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