Thermal-ignition analysis in boundary-layer flows
- 15 May 1979
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 92 (1) , 97-108
- https://doi.org/10.1017/s0022112079000537
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.Keywords
This publication has 9 references indexed in Scilit:
- Ignition of a Reactive Solid Exposed to a Step in Surface TemperatureSIAM Journal on Applied Mathematics, 1979
- On the stagnation-point ignition of a premixed combustibleInternational Journal of Heat and Mass Transfer, 1978
- Ignition of a gas in a boundary layer at a heated plateFluid Dynamics, 1978
- Theory of Combustion in Laminar FlowsAnnual Review of Fluid Mechanics, 1971
- On the Ignition of a Pre-Mixed Fuel by a Hot ProjectileCombustion Science and Technology, 1970
- Asymptotic Analysis of Laminar Flame Propagation for General Lewis NumbersCombustion Science and Technology, 1970
- Ignition and combustion in a laminar boundary layer over a hot surfaceSymposium (International) on Combustion, 1957
- Ignition and Combustion in a Laminar Mixing ZoneJournal of Jet Propulsion, 1954
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949