Controlling supersonic boundary layer stability by means of distributed mass transfer through a porous wall

DOI10.1134/S0015462813060070zbMath1287.76192OpenAlexW2089878557MaRDI QIDQ2450338

N. M. Terekhova, S. A. Gaponov

Publication date: 21 May 2014

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462813060070

zbMATH Keywords

hydrodynamic stabilitylaminar-turbulent transitionsupersonic boundary layer

Mathematics Subject Classification ID

Flows in porous media; filtration; seepage (76S05) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (5)

Joint effect of heat and mass transfer on the compressible boundary layer stability ⋮ Tangential gas blowing and boundary layer stability of a compressible gas ⋮ Disturbance evolution in compressible boundary layers on impermeable and porous surfaces under external pressure gradient ⋮ Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition ⋮ Joint permeability and roughness effect on the supersonic flat-plate boundary layer stability and transition

Cites Work

• Three-wave interactions of disturbances in a hypersonic boundary layer on a porous surface
• Linear evolution and interaction of disturbances in the boundary layers on impermeable and porous surfaces in the presence of heat transfer
• Three-wave interactions between disturbances in the hypersonic boundary layer on impermeable and porous surfaces

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