开展高超声速机动飞行器的气动布局概念设计研究,提出一种新的升力体机动飞行器气动布局方案,进行了机体的优化设计,并进行了控制舵的匹配设计,研究了飞行器的气动特性和操纵效率问题。研究表明,该方案可以获得较高的配平升阻比及配平攻角,有较高的机动控制效率,是高超声速飞行器实现高机动的潜在可行方案。 The concept design of aerodynamic layout of hypersonic maneuvering vehicle is studied. A new aerodynamic layout scheme of aerodynamic maneuvering vehicle is proposed, and the optimal design of the body is carried out. The matching design of the control rudder is carried out. The aerodynamic characteristics and steering efficiency of the aircraft are studied. problem. The results show that the proposed scheme can achieve a higher leveling drag ratio, a lower attack angle and a higher maneuvering efficiency, which is a potential solution to the high maneuver of hypersonic vehicles.