Supersonic flux-split procedure for second moments of turbulence

DOI10.2514/3.12544zbMath0846.76071OpenAlexW2052941506MaRDI QIDQ4876501

Foluso Ladeinde

Publication date: 10 June 1996

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.12544

zbMATH Keywords

finite volume procedureflux-difference splittingflux-vector splittingsix components of Reynolds stress tensorsolenoidal dissipation

Mathematics Subject Classification ID

Shear flows and turbulence (76F10) Supersonic flows (76J20)

Related Items (4)

Low-diffusion approximate Riemann solvers for Reynolds-stress transport ⋮ A parallelized ENO procedure for direct numerical simulation of compressible turbulence ⋮ Implicit meanflow-multigrid algorithms for Reynolds stress model computation of 3-D anisotropy-driven and compressible flows ⋮ An Approximate Roe-Type Riemann Solver for a Class of Realizable Second Order Closures

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