On the interaction between the shock wave attached to a wedge and freestream disturbances

DOI10.1007/BF00311809zbMath0822.76028OpenAlexW1964721360MaRDI QIDQ1892192

D. Glenn Lasseigne, M. Yousuff Hussaini, Peter W. Duck

Publication date: 8 June 1995

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00311809

zbMATH Keywords

supersonic flowacoustic wavesvorticity wavesentropy wavesshock- body coupling

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Parallel shear flows in hydrodynamic stability (76E05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (5)

HTR approach to the asymptotic solutions of supersonic boundary layer problem: the case of slow acoustic waves interacting with streamwise isolated wall roughness ⋮ Response and receptivity of the hypersonic boundary layer past a wedge to free-stream acoustic, vortical and entropy disturbances ⋮ Interactions between vortical, acoustic and thermal components during hypersonic transition ⋮ Generation of first Mack modes in supersonic boundary layers by slow acoustic waves interacting with streamwise isolated wall roughness ⋮ Receptivity of inviscid modes in supersonic boundary layers to wall perturbations

Cites Work

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• On the non-uniqueness of the solution of the problem on steady flow about the plane wedge and circular cone
• Stability of Shock Waves Attached to Wedges and Cones
• Multi-valued solutions of steady-state supersonic flow. Part 1. Linear analysis
• Interaction of disturbances with an oblique detonation wave attached to a wedge
• Interaction of Linear Waves with Oblique Shock Waves
• On the stability of the supersonic flows past a wedge
• On supersonic flow past an oscillating wedge

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