Titlebook: Aerothermodynamics in Combustors; IUTAM Symposium Taip Richard S. L. Lee,James H. Whitelaw,T. S. Wung Conference proceedings 1992 Springer-

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搬运工

Experimental Investigation of the Reduction of Burning Rate Due to Finite Spacing Between Dropletsl sprays the droplet diameter ranges typically from 10 . up to 500 .. If the distances between the droplets are small, the mutual interactions of the droplets have to be taken into account for the description of the physical and chemical processes in the combustor. Usually it is very difficult to in

ANTE

Blue Flame Combustion in a Jet-Mixing-Type Spray Combustortional-type swirl atomizer into the combustor and combustion air was introduced through a baffle plate with 16 inlet holes. The basic mechanism of this combustion method was revealed as a rapid mixing of the air and the spray, which was achieved by a high-speed air jet. Combustion characteristics in

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菊花

Control of Oscillations in Ducted Premixed Flamessk and a rearward-facing step in ducts without and with an exit nozzle, by the oscillation of the pressure field and by the oscillatory injection of secondary fuel upstream of the flame holding plane, and quantifies the influence of heat release rate on attenuation. Control was not sensitive to powe

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https://doi.org/10.1007/978-3-642-84755-4Aerodynamik; Combustors; Flow; Strömung; Thermodynamik; Verbennung; thermodynamics; fluid- and aerodynamics

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mechanism

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