A generalized non-reflecting inlet boundary condition for steady and forced compressible flows with injection of vortical and acoustic waves
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Publication:2313691
DOI10.1016/j.compfluid.2019.06.027zbMath1496.76118OpenAlexW2955179007WikidataQ127620995 ScholiaQ127620995MaRDI QIDQ2313691
Publication date: 19 July 2019
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://oatao.univ-toulouse.fr/25689/1/Daviller_25689.pdf
characteristic boundary conditionsacoustic forcingturbulence injectionnon reflecting boundary conditions
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Cites Work
- Generalized characteristic relaxation boundary conditions for unsteady compressible flow simulations
- Three-dimensional boundary conditions for numerical simulations of reactive compressible flows with complex thermochemistry
- Time-dependent boundary conditions for hyperbolic systems. II
- Absorbing boundary conditions for nonlinear Euler and Navier-Stokes equations based on the perfectly matched layer technique
- Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows
- Time dependent boundary conditions for hyperbolic systems
- A nonreflecting outflow boundary condition for subsonic Navier-Stokes calculations
- Boundary conditions for subsonic compressible Navier-Stokes calculations
- Boundary conditions for direct simulations of compressible viscous flows
- A perfectly matched layer for the absorption of electromagnetic waves
- Development of high-order Taylor-Galerkin schemes for LES
- Improved boundary conditions for the direct numerical simulation of turbulent subsonic flows. I: Inviscid flows
- Partially reflecting and non-reflecting boundary conditions for simulation of compressible viscous flow
- Using staggered grids with characteristic boundary conditions when solving compressible reactive Navier-Stokes equations
- Characteristic boundary conditions for simulations of compressible reacting flows with multi-dimensional, viscous and reaction effects
- Numerical simulation of compressible homogeneous flows in the turbulent regime
- Numerically Nonreflecting Boundary and Interface Conditions for Compressible Flow and Aeroacoustic Computations
- Proposed Inflow/Outflow Boundary Condition for Direct Computation of Aerodynamic Sound
- On the identification of a vortex
- Compositional inhomogeneities as a source of indirect combustion noise
- Characteristic boundary conditions for direct simulations of turbulent counterflow flames
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