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- W2320231646 abstract "An array of carefully chosen configurations based on cavities and ramp mixers were examined for their efficacy in the enhancement of fuel-air mixing in supersonic flows . With the cavities, two back-to-back cavities on the strut, separated by a thin plate, referred to as the “twin cavity” configuration, has been considered along with the case where the thin plate is removed which is the “bottomless” configuration. In both cases, three injection locations are considered, one upstream of the cavity, another downstream of the cavity, and a third at the trailing edge wall of the cavity in the direction opposite to the main flow. The first two configurations have been compared with the cavity less case. In the case of ramps, three different injection locations were chosen, one pertaining to far upstream and another just behind the ramps, whereas a third location is at the base of the strut. The performances of all configurations are compared in the form of mole fraction contours. Static pressure measurements along the length of the test section and the combustor are compared. It is found that the cavity mixers fare better in terms of mixing enhancement and length required for achieving good mixing, when compared to the ramp mixers. Among the three different injection locations with cavities, the order of superior ability for mixing enhancement is the upstream location, followed by the downstream location, and then the opposing injection from the trailing edge wall of the cavity. In the case of ramp mixers, injection just upstream of the ramps is superior to injection far upstream, followed by base injection which shows the poorest mixing of all three injection locations." @default.
- W2320231646 created "2016-06-24" @default.
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- W2320231646 date "2004-06-26" @default.
- W2320231646 modified "2023-09-27" @default.
- W2320231646 title "Mixing in Confined Supersonic Flow Past Strut Based Cavity and Ramps" @default.
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- W2320231646 doi "https://doi.org/10.2514/6.2004-4194" @default.
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