Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone

DOI10.1017/S0022112008003030zbMath1151.76310MaRDI QIDQ5302674

D. A. Bountin, A. N. Shiplyuk, Anatoly A. Maslov

Publication date: 8 January 2009

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (8)

Characterization of instability mechanisms on sharp and blunt slender cones at Mach 6 ⋮ Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer ⋮ Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer ⋮ Interaction and breakdown induced by multiple optimal disturbances in hypersonic boundary layer ⋮ Interactions between second mode and low-frequency waves in a hypersonic boundary layer ⋮ Linear, nonlinear and transitional regimes of second-mode instability ⋮ Nonlinear behaviour of the Mack mode in a hypersonic boundary layer ⋮ Bispectral analysis of nonlinear processes in the hypersonic boundary layer on a porous cone surface

Cites Work

• Nonlinear spectral dynamics of hypersonic laminar boundary layer flow
• Subharmonic transition to turbulence in a flat-plate boundary layer at Mach number 4.5
• Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating
• Non-linear resonant instability in boundary layers

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