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Showing 1 to 2 of 2 for “"inlet buzz"”.
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Preliminary experiment and analysis of supersonic inlet buzz
The inlet buzz phenomenon was investigated experimentally and analytically. An external-compression axisymmetric inlet model, having 74 mm in cowl lip diameter, was tested in the 229x229 sq mm blowdown wind tunnel at Mach 2.4. The test facility has shown potential for the supersonic inlet research. …
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The effects of micro-vortex generators on normal shock wave/boundary layer interactions
… and transonic flow fields such as engine inlets. This investigation was undertaken to study the effects of passive flow control devices on normal shock wave/boundary layer interactions in an effort to gain insight into the physics that govern these complex interactions. The work …