Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling

DOI10.1016/S1270-9638(00)01070-1zbMath1007.76047WikidataQ127012666 ScholiaQ127012666MaRDI QIDQ4528439

Michael Oevermann

Publication date: 27 March 2003

Published in: Aerospace Science and Technology (Search for Journal in Brave)

zbMATH Keywords

probability density functioncompressible flowapproximate Riemann solvercentral schemeturbulent diffusion flamestwo-equation \(k\)-epsilon turbulence modelsupersonic combustion ramjet enginefully implicit finite volume schemehydrogen injectionmean turbulent strain ratenon-equilibrium chemistrystretched laminar flamelet modelunstructured triangulated grids

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Reaction effects in flows (76V05) Turbulent transport, mixing (76F25)

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