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- W2313692726 abstract "Experimental investigations of the flow fiel d associated with three upstream direct - injection acoustic resonance cavities coupled with a previously designed downstream combustion cavity in a non -reacting flow are described. All of the upstr eam mixing cavities were acoustically open (shear layer r ea ttachment on the downstream wall of the cavity) with the length -to -depth ratio (L/D) on the order of 1. The previously established downstream combustion cavity had an L/D of 4.7 and an aft ramp angle ( �) of 22.5 degrees. The three upstream mixing cavities we re characterized in Mach 2 free stream flow with injection at three locations (upstream wall, center, downstream wall) within each cavity. Injection at the upstream wall of the cavity provided great er penetration height into the free stream as well as faster mixing with the free stream compared with injection at the center or downstream wall of the cavity. Injection at the center of the cavity resulted in the injectant diffusing laterally in the cav ity bef ore being ejected into the free stream. Injection at the downstream wall of the cavity displayed characteristics of both injection at the upstream wall and center of the cavity . The flow over the downstream cavity was similar for all injection loca tions. Pressure taps along the ceiling and floor of the test section showed no distinct change in pressure readings due to either cavity length or injection location within the cavity." @default.
- W2313692726 created "2016-06-24" @default.
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- W2313692726 date "2005-07-10" @default.
- W2313692726 modified "2023-09-26" @default.
- W2313692726 title "Upstream Mixing Cavity Coupled wtih a Downstream Flameholding Cavity Behavior in Supersonic Flow" @default.
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- W2313692726 doi "https://doi.org/10.2514/6.2005-3709" @default.
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