Invention Grant
US08739514B2 Low shock strength propulsion system 有权
低冲击强度推进系统

Low shock strength propulsion system
Abstract:
A supersonic nacelle design is disclosed herein that employs a bypass flow path internal to the nacelle and around the engine. By shaping the nacelle, the nacelle may function to reduce sonic boom strength, cowl drag, and /or airframe interference drag. The nacelle may also function to improve total pressure recovery and/or total thrust of the primary flow path through the engine.
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