Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer

DOI10.1007/S10483-017-2227-9zbMath1428.76187OpenAlexW2731737421MaRDI QIDQ1674131

Cunbo Zhang, Ji-Sheng Luo

Publication date: 1 November 2017

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

Full work available at URL: https://doi.org/10.1007/s10483-017-2227-9

zbMATH Keywords

supersonic boundary layernonlinear mode interactionboundary layer instability

Mathematics Subject Classification ID

Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

Interactions between oblique second mode and oblique waves in a high-speed boundary layer

Uses Software

• LASTRAC

Cites Work

• Three-wave interactions between disturbances in the hypersonic boundary layer on impermeable and porous surfaces
• Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack
• PSE as applied to problems of transition in compressible boundary layers
• Oblique-mode breakdown and secondary instability in supersonic boundary layers
• Interaction of phase-locked modes: a new mechanism for the rapid growth of three-dimensional disturbances
• Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone
• Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack

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