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- W2331778462 abstract "This paper presents an experimental study on the effect of geometry on the flow structure of experimental swirl-stabilized gas turbine burners. Measurements were conducted in a cold flow air channel on a series of one-quarter scale experimental swirlers. The swirler models were designed with different blade angles and spacings in order to alter the swirl number of the flow. Stereo PIV measurements are presented for four different combinations of blade angle and spacing. Tests showed that wider blade spacing resulted in a reduced swirl number and a weaker vortex breakdown. A greater blade angle was observed to increase the swirl number and the strength of the vortex breakdown. An optimal swirler design requires careful balance of these two parameters in order to ensure sufficient recirculation and flame stability without excessive pressure loss." @default.
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- W2331778462 date "2002-07-07" @default.
- W2331778462 modified "2023-10-05" @default.
- W2331778462 title "The Effect of Fuel Injector Geometry on the Flow Structure of a Swirl Stabilized Gas Turbine Burner" @default.
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- W2331778462 doi "https://doi.org/10.2514/6.2002-4012" @default.
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