Thermal-ignition analysis in boundary-layer flows

Author:

Law C. K.,Law H. K.

Abstract

The weakly reactive state leading to the ignition of a steady laminar boundary-layer flow of a combustible mixture over a hot, isothermal, non-permeable, non-catalytic flat plate is studied both numerically and using matched asymptotic analysis in the realistic limit of large activation energy. It is shown that the flow consists of a locally similar diffusive-reactive region next to the plate and a non-similar diffusive-convective region outside it; that the analytic solution obtained reproduces the lower half of the S-shaped ignition-extinction response curve such that ignition is expected to occur when a suitably defined Damköhler number, which increases with the streamwise distance, reaches unity; and that at the point of ignition the heat transfer from the wall vanishes identically. An explicit expression for the minimum distance for ignition to occur is also derived.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference16 articles.

1. Chapman, D. R. & Rubesin, M. W. 1949 Temperature and velocity profiles in the compressible boundary layer with arbitrary distribution of surface temperature.J. Aero. Sci. 16,547.

2. Dooley, D. A. 1957 Ignition in the laminar boundary layer of a heated plate.Heat Transfer Fluid Mech. Inst., Stanford Univ. pp.321–342.

3. Law, C. K. 1978 On the stagnation-point ignition of a premixed combustible.Int J. Heat Mass Transfer 21,1363.

4. Chung, P. M. 1965 Chemically reacting nonequilibrium boundary layers. In Advances in Heat Transfer , vol. 2,pp.109–270.Academic Press.

5. Fendell, F. E. 1965 Ignition and combustion of initially unmixed reactants.J. Fluid Mech. 21,281.

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