supersonic inlet

[¦sü·pər¦sän·ik ′in‚let]

(aerospace engineering)

An inlet of a jet engine at which single, double, or multiple shock waves form.

supersonic inlet

An air inlet designed for supersonic flow both past it and through it at least for a part of the flight. Ideally, it has a center body or side wedge, which creates oblique shock waves.

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References in periodicals archive ?

Examples apply numerical procedures for solving one-dimensional Euler equations to flow within a supersonic inlet, a converging-diverging nozzle, and a piston tube, and flow past an expansion corner and a compression corner.

Numerical Computation of Compressible and Viscous Flow

Both of the Blackbird's twin nacelles contain an engine supersonic inlet, the J58 engine with its afterburner, and an exhaust ejector nozzle.

Thus the Blackbird's supersonic inlet must provide subsonic flow to the J58 compressor inlet, over the full range of flight speeds.

Powering out of trouble

Sagaut, "Time-frequency analysis and detection of supersonic inlet buzz," AIAA Journal, vol.

Unstart coupling mechanism analysis of multiple-modules hypersonic inlet

As a junior engineer working on supersonic inlets for NASA in the waning days of the old Supersonic Transport program, Robert Shaw had the feeling that the SST was vulnerable to "a big hit."

Research on higher plane revives supersonic jet

To achieve high performance levels, the mixed-compression inlet will need to operate close to its stability limit, much closer than military supersonic inlets. This requirement highlights the importance of the inlet control system on the inlet design and the ability of the inlet to handle atmospheric disturbances and inlet unstarts.