|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||137/152 ; 244/53B|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 27 인용 특허 : 0|
A flush inlet and inlet air passage for supersonic aircraft including provisions for efficiently decelerating a supersonic airstream entering the inlet and converting such airstream to subsonic airflow within the inlet air passage prior to introduction into the aircraft\s jet propulsion engine. More specifically, a two-dimensional inlet and convergent/divergent inlet air passage for supersonic jet aircraft wherein the inlet is flush with the aircraft\s external surface, and the supersonic airflow entering the inlet is reduced to transonic or subsonic vel...
A flush supersonic air inlet and convergent/divergent inlet air passage for supersonic aircraft of the type having a jet propulsion engine, comprising, in combination: (a) a flush mounted air inlet formed in the surface of the aircraft body; (b) a convergent/divergent inlet air passage having a throat at the juncture of the convergent and divergent portions of said passage and extending from said flush mounted air inlet to the jet propulsion engine inlet; (c) an expansion corner defining an adjustable cant angle formed at the upstream leading edge of sai...