An engine inlet for efficient operation at both design Mach number and off-design Mach numbers has a fixed compression surface and a leading edge that is variably extendible over the fixed compression surface to simultaneously vary capture area, compression and shock wave position.
Variable-capture supersonic inlet
2018-03-06
Patent
Electronic Resource
English
Study of Supersonic Cavity Flow in Advanced Variable Geometry Inlet
Online Contents | 2005
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