Simulation of hypersonic boundary layer on porous surfaces using OpenFOAM
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Publication:2083904
DOI10.1016/j.compfluid.2022.105437OpenAlexW4221028704MaRDI QIDQ2083904
Minwoo Kim, Donghun Park, Jaeyoung Park, Solkeun Jee, Jiseop Lim, Taesoon Kim
Publication date: 17 October 2022
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2022.105437
Related Items (1)
Uses Software
Cites Work
- A sequel to AUSM: AUSM\(^ +\)
- Boundary conditions for direct simulations of compressible viscous flows
- Large-eddy simulation of the shock/turbulence interaction
- A low-dissipative solver for turbulent compressible flows on unstructured meshes, with openfoam implementation
- Generalized conservative approximations of split convective derivative operators
- Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
- Receptivity of a hypersonic boundary layer over a flat plate with a porous coating
- Secondary instabilities in compressible boundary layers
- Shock-induced heating and transition to turbulence in a hypersonic boundary layer
- Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers
- Interactions between second mode and low-frequency waves in a hypersonic boundary layer
- Numerical Methods for High-Speed Flows
- Second-mode attenuation and cancellation by porous coatings in a high-speed boundary layer
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