Hysteresis of shock wave locations in divergent bent channels

DOI10.1016/j.compfluid.2019.02.016zbMath1411.76038OpenAlexW2917696467MaRDI QIDQ1735017

Alexander Kuz'min

Publication date: 28 March 2019

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2019.02.016

zbMATH Keywords

hysteresisshock wavesturbulent boundary layerflow instabilitywall bends

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Turbulent boundary layers (76F40)

Cites Work

• Unnamed Item
• Shock wave bifurcation in channels with a bend
• Leading edge bluntness effect on the flow in a model air-inlet
• Aerodynamic response of internal passages to pulsating inlet supersonic conditions
• Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:turning angle effects
• Non-unique transonic flows over airfoils
• Review of the shear-stress transport turbulence model experience from an industrial perspective

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