The stability of two-dimensional wakes and shear layers at high Mach numbers

DOI10.1063/1.858011zbMath0733.76019OpenAlexW2003039931MaRDI QIDQ3359870

Demetrios T. Papageorgiou

Publication date: 1991

Published in: Physics of Fluids A: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.858011

zbMATH Keywords

inviscid stabilitytwo-dimensional wakeshypersonic stabilitylaminar free-shear-layer

Mathematics Subject Classification ID

Parallel shear flows in hydrodynamic stability (76E05) Hypersonic flows (76K05)

Related Items (4)

Centrifugal instabilities in curved compressible wakes ⋮ On the instability of hypersonic flow past a flat plate ⋮ Compressible Modes of the Rotating‐Disk Boundary‐Layer Flow Leading to Absolute Instability ⋮ Instability of the flow in the vicinity of trailing edge of a class of thin aerofoils

Cites Work

• Linear instability of the supersonic wake behind a flat plate aligned with a uniform stream
• On the Görtler vortex instability mechanism at hypersonic speeds
• On the instabilities of supersonic mixing layers: a high-Mach-number asymptotic theory
• On the instability of hypersonic flow past a wedge
• The inviscid instability of a Blasius boundary layer at large values of the Mach number
• Linear instability of the wake behind a flat plate placed parallel to a uniform stream
• Inviscid spatial stability of a compressible mixing layer
• On the flow near the trailing edge of a flat plate II
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• THE VELOCITY DISTRIBUTION IN THE LAMINAR BOUNDARY LAYER BETWEEN PARALLEL STREAMS

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