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|Title: ||Experimental and computational study of hybrid diffusers for gas turbine combustors|
|Authors: ||Walker, Alastair Duncan|
Denman, Paul A.
McGuirk, James J.
|Issue Date: ||2003|
|Publisher: ||© ASME|
|Citation: ||WALKER, A.D., DENMAN, P.A. and MCGUIRK, J.J., 2003. Experimental and computational study of hybrid diffusers for gas turbine combustors. IN: Proceedings of the ASME International Gas Turbine and Aeroengine Congress and Exposition. ASME Turbo Expo 2003, Atlanta, Georgia, 16th-19th June 2003, vol. 2, pp. 311-320|
|Abstract: ||The increasing radial depth of modern combustors poses a particularly difficult aerodynamic challenge for the prediffuser. Conventional diffuser systems have a finite limit to the diffusion that can be achieved in a given length and it is, therefore, necessary for designers to consider more radical and unconventional diffuser configurations. This paper will report on one such unconventional diffuser; the hybrid diffuser which, under the action of bleed, has been shown to achieve high rates of diffusion in relatively short lengths. However, previous studies have not been conducted under representative conditions and have failed to provide a complete description of the relevant flow mechanisms making optimisation difficult. Utilising an isothermal representation of a modern gas turbine combustor an experimental investigation was undertaken to study the performance of a hybrid diffuser compared to that of a conventional, single passage, dump diffuser system. The hybrid diffuser achieved a 53% increase in area ratio within the same axial length generating a 13% increase in the pre-diffuser static pressure recovery coefficient which, in turn, produced a 25% reduction in the combustor feed annulus total pressure loss coefficient. A computational investigation was also undertaken in order to investigate the governing flow mechanisms. A detailed examination of the flow field, including an analysis of the terms within the momentum equation, demonstrated that the controlling flow mechanisms were not simply a boundary layer bleed but involve a more complex interaction between the accelerating bleed flow and the diffusing mainstream flow. A greater understanding of these mechanisms enabled a more practical design of hybrid diffuser to be developed that not only simplified the geometry but also improved the quality of the bleed air making it more attractive for use in component cooling.|
|Description: ||This item is closed access. It is a conference paper [© ASME ]. For more information on how to obtain this article please visit the ASME Digital Library, http://www.asmedl.org/ .|
|Version: ||Closed access|
|Appears in Collections:||Closed Access (Aeronautical and Automotive Engineering)|
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