Nonparallel instability of supersonic and hypersonic boundary layers

DOI10.1063/1.857898zbMath0746.76058OpenAlexW2087785615MaRDI QIDQ4000997

Nabil M. El-Hady

Publication date: 26 September 1992

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

Full work available at URL: http://hdl.handle.net/2060/19910012772

zbMATH Keywords

flat platemultiple scaling technique

Mathematics Subject Classification ID

Turbulence (76F99) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (7)

Modeling of nonparallel effects in temporal direct numerical simulations of compressible boundary-layer transition ⋮ Mixed convection flow in a curved annulus: Effect of radius ratio ⋮ On transition in supersonic and hypersonic boundary layers ⋮ Effect of pressure gradient on first mode of instability in compressible boundary layers ⋮ Instability and low-frequency unsteadiness in a shock-induced laminar separation bubble ⋮ 3D global optimal forcing and response of the supersonic boundary layer ⋮ An adjoint compressible linearised Navier–Stokes approach to model generation of Tollmien–Schlichting waves by sound

Cites Work

• On the stability of almost parallel boundary layer flows
• An experiment on the stability of hypersonic laminar boundary layers
• Stability and transition of a supersonic laminar boundary layer on an insulated flat plate
• Evolution of resonant wave triads in three-dimensional boundary layers
• The flat plate boundary layer. Part 3. Comparison of theory with experiment

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