关键词: 高机动性飞机;飞机－发动机匹配;进气道－发动机匹配;一体化设计

Abstract: Aircraft airframe/engine integration has been always a major attention getting subject in maneuver fighter aircraft development internationally for the years,aiming at inproving the operating effectiveness and stability of propulsion system including inlet and nozzle.This paper lists the integration examples of some foreign fighter types,especially those of symmetrical twin intake air induction systems,and gived the alternative inlet configuration with the intention of performance and safety inprovements as viewed from fundamentals of fighter design.

Key words: ighly maneuverable aircraft;Airplane engine matching;Inlet engine matching;Integrated design