Experimental investigation of axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions

DOI10.1017/JFM.2012.464zbMath1284.76025OpenAlexW2095697164MaRDI QIDQ5406433

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Publication date: 1 April 2014

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2012.464

zbMATH Keywords

shock wavescompressible flowscompressible boundary layers

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Turbulent boundary layers (76F40) Hypersonic flows (76K05)

Related Items (2)

On the length scales of hypersonic shock-induced large separation bubbles near leading edges ⋮ Transition scenario in hypersonic axisymmetrical compression ramp flow

Cites Work

• Unnamed Item
• Numerical simulation of Görtler vortices in hypersonic compression ramps
• Experimental and computational study of laminar cavity flows at hypersonic speeds
• Some properties of boundary layer flow during the transition from laminar to turbulent motion
• QUASI-STEADY ASPECTS OF THE ADJUSTMENT OF SEPARATED FLOW REGIONS TO TRANSIENT EXTERNAL FLOWS
• Dilatation-dissipation corrections for advanced turbulence models
• Shock Wave-Boundary-Layer Interactions
• Effects of upstream boundary layer on the unsteadiness of shock-induced separation
• CRITICAL HYPERSONIC AEROTHERMODYNAMIC PHENOMENA

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