Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack

DOI10.1007/S10483-007-0804-2zbMath1231.76114OpenAlexW2008486724MaRDI QIDQ940372

Ming Dong, Ji-Sheng Luo

Publication date: 1 September 2008

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10483-007-0804-2

zbMATH Keywords

stabilitytransitionzero angle of attacksharp cone boundary layer

Mathematics Subject Classification ID

Transition to turbulence (76F06)

Related Items (3)

Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer ⋮ Interactions between second mode and low-frequency waves in a hypersonic boundary layer ⋮ Inflow boundary condition for DNS of turbulent boundary layers on supersonic blunt cones

Cites Work

• A mechanism for excitation of coherent structures in wall region of a turbulent boundary layer
• Study of mechanism of breakdown in laminar-turbulent transition of supersonic boundary layer on flat plate
• Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers

This page was built for publication: Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack