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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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Convex Analysis and Global Optimization. The interacting droplet is modeled with a centrally located droplet and its vapor bubble which is surrounded by a cloud of droplets. The distribution of the droplets and the size of cloud are characterized by a pair-distribution function. The analysis reveals that the vaporization of a droplet is
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Successive Partitioning Methodsl 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
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Successive Partitioning Methodstional-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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https://doi.org/10.1007/978-1-4757-2809-5s. The heat loss mechanism is composed of the external heat loss represented by the bulk heat conduction form the spray to a tube wall, and the internal heat loss associated with the droplet gasification process. The enhancement of upstream prevaporization is achieved by varying the wall temperature
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https://doi.org/10.1007/978-1-4757-2809-5sk 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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Discussion, Limitations, and Implications,rements along with CCD video-cameras visualizations allow for a qualitative description of the various combustion processes involved. More precisely, it is clearly evidenced that more than one model should be used to represent numerically the whole flowfield characteristics.
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Convex Analysis and Global Optimizationd chemical effects render their study very complex. In particular, high spatial and temporal resolution measurement methods are needed to increase the understanding of the microscopic processes which are believed to drive the macroscopic behaviour of these reacting turbulent flows.
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June 1991 and was attended by 130 delegates from eight countries. The topics of the forty formal presentations included measurements and calculations of isothermal simulations and of combusting flows with one and two phases, and with consideration of configurations ranging from simple diffusion to
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