Boundary conditions for low Mach number reacting flows

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Abstract

    In this paper we explore the specification of time dependent boundary conditions for the simulation of low Mach number reacting flows. A new approach is presented which is derived from the method of characteristics and an application of a Mach number based double expansion. Through the double expansion, it is possible to identify and seperate inertial events from acoustic events. By controlling the inertial components of the flow, non-reflecting conditions for a wide variety of problems may be specified. The accuracy of the method is demonstrated using a curved stagnating flame, in which the reaction zone crosses the boundary.
    Original languageEnglish
    Title of host publicationWSEAS Transactions on Mathematics|WSEAS Trans. Math.
    Pages1102-1107
    Number of pages5
    Volume5
    Publication statusPublished - Oct 2006
    Event4th WSEAS International Conference on Fluid Mechanics and Aerodynamics -
    Duration: 1 Jan 1824 → …

    Conference

    Conference4th WSEAS International Conference on Fluid Mechanics and Aerodynamics
    Period1/01/24 → …

    Keywords

    • Boundary conditions
    • Characteristics
    • Turbulence

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