Effects of various boundary-layer bleed locations on the stability of an axisymmetric

supersonic inlet has been investigated experimentally. The bleeds were located on the inlet

compression cone and were designed to improve...

Buzz phenomenon is shock oscillation ahead of the supersonic air intake when its mass flow rate is decreasing at off design condition. The buzz onset and the buzz cycle of an axisymmetric mixed-compression supersonic intake ...

Supersonic inlet is often considered to be the most crucial element in the air-breathing engine of a

flying vehicle designed to operate at supersonic speeds. The function of the inlet is to provide

subsonic flow at the desired velocity...

The flow over a supersonic inlet has been investigated experimentally and numerically at a

free stream Mach number of 2 and a zero degree angle of attack. Wind tunnel tests were performed to

obtain the performance parameters...

boundary-layer interactions relevant to the supersonic inlets. Each of these flow interaction phenomena has different effects on the stability and on the performance of the inlet. Interaction of terminal normal shock with internal duct boundary-layer causes...