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Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity

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Publication:2853486
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DOI10.1016/J.AST.2007.04.003zbMath1273.76429OpenAlexW1986274775MaRDI QIDQ2853486

Manfred Aigner, P. Stoll, Markus Kindler, Peter Gerlinger, Fernando Schnieder

Publication date: 22 October 2013

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

Full work available at URL: https://elib.dlr.de/54473/1/gerlinger2008ast_manuscript.pdf


zbMATH Keywords

scramjetmixing enhancementstreamwise vorticitysupersonic combustorhydrogen/air combustionlobed strut injector


Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05) Supersonic flows (76J20)


Related Items (2)

Streamwise vortex breakdown due to the interaction with crossed shock waves ⋮ Assumed PDF Modeling of Turbulence Chemistry Interaction in Scramjet Combustors







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