Aircraft Engine Exhaust Nozzle System for Jet Noise Reduction
[摘要] The aircraft exhaust engine nozzle system includes a fan nozzle to receive a fan flow from a fan disposed adjacent to an engine disposed above an airframe surface of the aircraft, a core nozzle disposed within the fan nozzle and receiving an engine core flow, and a pylon structure connected to the core nozzle and structurally attached with the airframe surface to secure the engine to the aircraft.
[发布日期] 2014-11-04 [发布机构]
[效力级别] [学科分类] 航空航天科学
[关键词] [时效性]