Numerical modeling of the stabilization of a supersonic flat-plate boundary layer by a porous coating
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Publication:604604
DOI10.1007/s10697-006-0051-xzbMath1198.76117OpenAlexW2003303766MaRDI QIDQ604604
Publication date: 11 November 2010
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10697-006-0051-x
stabilityNavier-Stokes equationssupersonic flowboundary layernumerical modelingacoustic wavesporous coatings
Flows in porous media; filtration; seepage (76S05) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25)
Related Items (3)
Effect of wall perturbations on the receptivity of a hypersonic boundary layer ⋮ Control of disturbances of a hypersonic viscous shock layer on a flat plate ⋮ Wave processes in a viscous shock layer and control of fluctuations
Cites Work
- Numerical modeling of the receptivity of a supersonic boundary layer to acoustic disturbances
- Influence of nonparallel flow on the development of disturbances in a supersonic boundary layer
- Numerical modeling of perturbation propagation in a supersonic boundary layer
- Leading-edge receptivity to free-stream disturbance waves for hypersonic flow over a parabola
- Initial-value problem for three-dimensional disturbances in a compressible boundary layer
- Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating
- Receptivity of a high-speed boundary layer to acoustic disturbances
- Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
- Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
- Prehistory of instability in a hypersonic boundary layer.
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