Journal
COMBUSTION THEORY AND MODELLING
Volume 9, Issue 4, Pages 617-646Publisher
TAYLOR & FRANCIS LTD
DOI: 10.1080/13647830500307378
Keywords
nonreflecting boundary conditions; compressible reacting flows; direct numerical simulation; counterflow; LODI
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Improved Navier-Stokes characteristic boundary conditions (NSCBC) are formulated for the direct numerical simulations (DNS) of laminar and turbulent counterflow flame configurations with a compressible flow formulation. The new boundary scheme properly accounts for multi-dimensional flow effects and provides nonreflecting inflow and outflow conditions that maintain the mean imposed velocity and pressure, while substantially eliminating spurious acoustic wave reflections. Applications to various counterflow configurations demonstrate that the proposed boundary conditions yield accurate and robust solutions over a wide range of flow and scalar variables, allowing high fidelity in detailed numerical studies of turbulent counterflow flames.
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