URANS computations of shock-induced oscillations over 2D rigid airfoils: influence of test section geometry

DOI10.1007/S10494-005-0557-ZzbMath1200.76084OpenAlexW1983536378MaRDI QIDQ608064

Eric Coustols, Mylène Thiery

Publication date: 25 November 2010

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10494-005-0557-z

zbMATH Keywords

modellingturbulenceunsteadinessRANSbuffetshock-induced oscillations

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Shear flows and turbulence (76F10) Finite volume methods applied to problems in fluid mechanics (76M12)

Related Items (1)

URANS computations of shock-induced oscillations over 2D rigid airfoils: influence of test section geometry

Uses Software

• elsA
• Spalart-Allmaras

Cites Work

• URANS computations of shock-induced oscillations over 2D rigid airfoils: influence of test section geometry
• Approximate Riemann solvers, parameter vectors, and difference schemes
• Separated flow and buffeting control
• Efficiency and accuracy of time-accurate turbulent Navier-Stokes computations
• Reassessment of the wall functions approach for RANS computations
• Implicit methods of second-order accuracy for the Euler equations
• The mixing layer over a deep cavity at high-subsonic speed

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