Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers

DOI10.1007/s10483-006-0601-1zbMath1178.76214OpenAlexW2510636771MaRDI QIDQ944688

Ji-Sheng Luo, Wei Cao, Ming Dong

Publication date: 17 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/s10483-006-0601-1

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20) Stability and instability of nonparallel flows in hydrodynamic stability (76E09)

Related Items (3)

Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack ⋮ The effects of variable specific heat on the stability of hypersonic boundary layer on a flat plate ⋮ Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack

Cites Work

• Boundary conditions for direct simulations of compressible viscous flows
• Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets

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