Comprehensive mesh study for a direct numerical simulation of the transonic flow at \(\mathrm{Re}_{c} = 500,000\) around a NACA 0012 airfoil

DOI10.1016/j.compfluid.2015.08.030zbMath1390.76151OpenAlexW1444506293MaRDI QIDQ1646023

M. Gageik, H. Olivier, I. Klioutchnikov

Publication date: 22 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2015.08.030

zbMATH Keywords

transonic flowdirect numerical simulation (DNS)WENOcompressibleaeroacousticsmesh study

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20) General aerodynamics and subsonic flows (76G25) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05)

Related Items (1)

Unsteady effects in a hypersonic compression ramp flow with laminar separation

Cites Work

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• Turbulence in fluids. Stochastic and numerical modelling.
• Efficient implementation of weighted ENO schemes
• Stability and receptivity characteristics of a laminar separation bubble on an aerofoil
• Direct simulation of a turbulent boundary layer up to R_θ = 1410
• DIRECT NUMERICAL SIMULATION: A Tool in Turbulence Research
• Linear stability of WENO schemes coupled with explicit Runge–Kutta schemes
• Numerical investigation of the tone noise mechanism over laminar airfoils

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