Natalya V. Guryleva, Mikhail A. Ivankin, Dmitry A. Lapinsky, Alexander M. Tereshin

DoI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-1147

Results of experimental studies of flow in sectioned duct of precombustion diffuser models divided into compartments by longitudinal partitions are presented. It is shown, that the presence of a gasdynamic connection between the channels reduces the flow irregularity, equalizes the flow parameters at the end of the channel, reduces the longitudinal dimensions of the flow deceleration area.

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In Categories: High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Propulsion, Propulsion Systems and Components
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