Hypersonic inlet systems and methods

Hypersonic inlet systems and methods are disclosed. In one embodiment, an inlet for an airbreathing propulsion system includes an inboard surface at least partially shaped to conform to a plurality of streamline-traces of a design flowfield approaching an aperture, an outboard surface spaced apart f...

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Main Authors LEYLEGIAN JOHN C, TYLL JASON S, CHUE RANDY S. M, ROBERTSON ANDREW, GIRLEA FLORIN, ESPINOSA ANGEL M, FARRELL DANIEL J, SMITH THOMAS R, ALIFANO JOSEPH A
Format Patent
LanguageEnglish
Published 23.10.2012
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Summary:Hypersonic inlet systems and methods are disclosed. In one embodiment, an inlet for an airbreathing propulsion system includes an inboard surface at least partially shaped to conform to a plurality of streamline-traces of a design flowfield approaching an aperture, an outboard surface spaced apart from the inboard surface, an upper surface extending between the inboard and outboard surfaces, and a lower surface extending between the inboard and outboard surfaces, wherein leading edges of the inboard, outboard, upper, and lower surfaces cooperatively define the aperture.
Bibliography:Application Number: US20080133289