9th International Space Planes and Hypersonic Systems and Technologies Conference 1999
DOI: 10.2514/6.1999-4917
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Non-premixed combustion in supersonic turbulent flows - A numerical study for co-flowing H2-air jets

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Cited by 6 publications
(4 citation statements)
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“…In this particular but very important practical case the combustion and mixing can develop simultaneously affecting each other [4][5][6] (see also [7] with many example of particular recently performed studies in the field). The combustion as an elementary chemical reaction between fuel and oxidant molecules needs the direct contact (collision) of these molecules.…”
Section: Introductionmentioning
confidence: 99%
“…In this particular but very important practical case the combustion and mixing can develop simultaneously affecting each other [4][5][6] (see also [7] with many example of particular recently performed studies in the field). The combustion as an elementary chemical reaction between fuel and oxidant molecules needs the direct contact (collision) of these molecules.…”
Section: Introductionmentioning
confidence: 99%
“…A more detailed inspection of the system of Eqs. (1) for ξ and Y leads to different responses depending on the values of the characteristic mixing time scales τ ξ and τ Y . On the IEM mixing lines, the chemical source terms can be neglected with respect to the mixing terms and the system (1) becomes:…”
Section: Lagrangian Path In the Composition Spacementioning
confidence: 99%
“…Then, a direct comparison between this chemical time scale and an estimated convection time scale or particle age allows the identification of a self-ignition domain in the composition space. Such a convection time scale or particle age τ a is the time needed by a Lagrangian particle to reach a given value of the mixture fraction ξ from its originating stream of pure oxidizer (0) or pure fuel (1). Its value is obtained by integrating the Lagrangian trajectory along the IEM pathlines as previously proposed by Izard and Mura [11,13].…”
Section: Extension To High Velocity Flowsmentioning
confidence: 99%
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