|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 60/2701|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 12 인용 특허 : 0|
A hypersonic inlet and a hypersonic engine and flight vehicle having such an inlet. The three-dimensionally-swept inlet has an upper member with a caret-shaped lower surface portion producing a two-dimensional wedge flow below such lower surface portion. The inlet also has a lower member having two inverted and transposed semi-caret-shaped upper surface portions producing a two-dimensional wedge flow above such upper surface portions. An inlet aft portion connects together the upper and lower members and has an orifice defining the engine inlet throat wh...
A flight vehicle engine inlet comprising: (a) a first member having at least a partial generally caret-shaped surface portion for producing a first generally two-dimensional wedge flow; (b) a second member having at least a partial generally caret-shaped surface portion for producing a second generally two-dimensional wedge flow, wherein said first and second members are disposed to generally oppose each other across a capture region which at least partially includes said first and second two-dimensional wedge flows; and (c) an aft portion having an orif...