Coupled Euler/boundary-layer method for nonequilibrium, chemically reacting hypersonic flows

DOI10.2514/3.11626zbMath0769.76041OpenAlexW2088937094MaRDI QIDQ5285484

Samuel Wüthrich, Mark L. Sawley

Publication date: 29 June 1993

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.11626

zbMATH Keywords

spheresecond-order termsfive speciesseventeen reactionssurface coefficients

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Related Items (6)

Hypersonic flow in chemical non-equilibrium: A comparison of thin-layer Navier-Stokes and coupled Euler/boundary layer computations ⋮ INTERFACE TREATMENT OF A THREE-DIMENSIONAL HYBRID INVISCID/VISCOUS FLOW PROBLEM ⋮ Comparison between coupled Euler/defect boundary-layer and Navier-Stokes computations for nonequilibrium hypersonic flows ⋮ Derivation, implementation, and initial testing of a compressible wall-layer model ⋮ Linear well-posedness of a hybrid inviscid/viscous flow problem with smooth and discontinuous solutions at the interface ⋮ A finite volume scheme for two‐dimensional chemically reactive hypersonic flow

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