Abstract
Higher-order effects in the boundary-layer theory are included in the present analysis to evaluate the interaction of the expansion process from the premixed combustion of reacting gases with the potential flow. Two cases are considered: (1) the premixed combustion process, which takes place above the flat plate; and (2) the premixed flame, which is generated in the wake of the flat plate. In both cases, the strong expansion process, when interacting with the outer inviscid flow, produces relatively strong pressure gradients, modifying the aerodynamic structure of the flow. 14 refs.
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