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- W2171102013 abstract "A non-reacting experimental study on a normal injection into a Mach 1.92 crossflow which flows over various geometries (flat plate, small cavity, large cavity) was carried out to investigate the effect of the momentum flux ratio (J). The aft ramp of the cavity advances the increase of the penetration height and the strong two-dimensional shock from recompression region mainly affects the shock structure and mixing layer at the downstream flow. As flow runs downsward, the transverse penetration height increases with increasing J (J = 0.9, 1.7, 3.4). However, above some critical ratio, jet penetration height growth with increasing J is not appeared in flow-field. Large scale cavity has a good mixing efficiency but it increases the drag loss in the combustor." @default.
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- W2171102013 date "2007-01-01" @default.
- W2171102013 modified "2023-09-24" @default.
- W2171102013 title "Mixing and Penetration Studies of Transverse Jet into a Supersonic Crossflow" @default.
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