2011
DOI: 10.1007/978-94-007-2482-2_52
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Direct Numerical Simulation of highly turbulent premixed flames burning methane

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Cited by 5 publications
(12 citation statements)
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“…It is much simpler than a full methane oxidation scheme such as the GRI-MECH 3.0 [5], containing 53 species and over 300 reaction and that cannot be used yet for systematic 3D DNS computations. The retained scheme provides sufficiently accurate results for lean up to stoichiometric conditions and has been successfully used/validated for direct simulations of 2D non-premixed methane jet flames [30] and turbulent premixed flames [17,19]. However, it could be inadequate for methane-rich flames due to the absence of C 2 and higher carbonchain reactions.…”
Section: Casementioning
confidence: 98%
“…It is much simpler than a full methane oxidation scheme such as the GRI-MECH 3.0 [5], containing 53 species and over 300 reaction and that cannot be used yet for systematic 3D DNS computations. The retained scheme provides sufficiently accurate results for lean up to stoichiometric conditions and has been successfully used/validated for direct simulations of 2D non-premixed methane jet flames [30] and turbulent premixed flames [17,19]. However, it could be inadequate for methane-rich flames due to the absence of C 2 and higher carbonchain reactions.…”
Section: Casementioning
confidence: 98%
“…This reaction mechanism is retained here due to its simplicity and stability, and provides sufficiently accurate results for lean up to stoichiometric conditions. It has been successfully used for large scale multi-dimensional direct computations of non-premixed methane jet flames [35] and most recently, highly turbulent premixed flames [27,36]. However, it would be inadequate for methane-rich flames due to the absence of C 2 and higher carbon-chain reactions, the reason why Φ ≤ 1.0 for the present study.…”
Section: Flame Configuration and Initializationmentioning
confidence: 99%
“…A spatial sixth-order central scheme and an explicit fourth-order Runge-Kutta time integrator are employed. In its recent version [26][27][28], the skew-symmetric formulation [29] has been implemented for the convective terms in order to reduce even further numerical dissipation and increase stability. The extended Navier-Stokes Characteristic Boundary Conditions (NSCBC) [30] are used, with non-reflecting boundaries and pressure relaxation applied along all open faces.…”
Section: Direct Numerical Simulationmentioning
confidence: 99%
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