Continuous mode transition in high-speed boundary-layers

DOI10.1007/s10494-011-9372-xzbMath1432.76110OpenAlexW2091935468MaRDI QIDQ453581

Paul A. Durbin, Jongwook Joo

Publication date: 27 September 2012

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10494-011-9372-x

zbMATH Keywords

direct numerical simulationcontinuous modeslaminar to turbulent transitionsupersonic boundary layer transition

Mathematics Subject Classification ID

Turbulent boundary layers (76F40) Supersonic flows (76J20)

Related Items

Nonlinear unsteady streaks engendered by the interaction of free-stream vorticity with a compressible boundary layer ⋮ Entrainment of short-wavelength free-stream vortical disturbances in compressible and incompressible boundary layers ⋮ Sensitivity of high-speed boundary-layer stability to base-flow distortion ⋮ Neural operator prediction of linear instability waves in high-speed boundary layers ⋮ On continuous spectra of the Orr–Sommerfeld/Squire equations and entrainment of free-stream vortical disturbances

Cites Work

• Unnamed Item
• Unnamed Item
• A robust high-order compact method for large eddy simulation.
• Numerical methods for hypersonic boundary layer stability
• On shear sheltering and the structure of vortical modes in single- and two-fluid boundary layers
• Effect of Mach number on the structure of turbulent spots
• Boundary-layer transition by interaction of discrete and continuous modes
• Discrete modes and continuous spectra in supersonic boundary layers
• Experiments on stability and transition at Mach 3
• Compressibility effects in a turbulent annular mixing layer. Part 1. Turbulence and growth rate
• Mode interaction and the bypass route to transition
• Heat transfer measurement of turbulent spots in a hypersonic blunt-body boundary layer