通过求解全机纵向运动状态方程，分析了全机模型带与不带机翼边条时纵向动态响应问题。
Aircraft longitudinal dynamic response of the system with and without LEX is analyzed by solving the state equation of aircraft longitudinal motion.
本文从控制和利用旋涡分离流的观点出发，说明了边条机翼的设计思想。
An idea for the aerodynamic design of a strake-wing is proposed from the control standpoint with utilization of vortex and separated flows.
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