The invention provides an aerodynamic configuration of a supersonic large maneuvering target, and the aerodynamic configuration is characterized in that a head cover is molded by adopting a von Karman curve lofting; the two canards are arranged at the two ends of the hood respectively, and the canards are medium-sweepback trapezoidal wings. The bullet body middle-rear section is located at the rear end of the head cover and is a circular-section equal-straight section. The two missile wings are arranged on the two sides of the middle-rear section of the missile body respectively. The inter-stage transition cabin is connected with the task stage and the booster in series; the booster bomb body is positioned at the rear end of the interstage transition cabin and adopts a circular-section equal straight section; the four rotating empennages are arranged at the tail part of the booster bomb body; the two ailerons are arranged on the two sides of the rear section of the missile body respectively and located at the rear edge ends of the missile wings. And the vertical tails are swallow-shaped vertical tails and are respectively arranged at two ends of the wingtips of the missile wings. According to the shape, the target can fly in a wide speed domain range, meanwhile, the target with the aerodynamic shape is excellent in aerodynamic performance and good in maneuverability during supersonic high-maneuverability flight, the blank in the field of supersonic high-maneuverability targets is filled up, and the requirements of novel weapon identification and battle training can be met.

    本发明提出一种超音速大机动靶标气动外形,其中,头罩采用冯卡门曲线放样成型;鸭翼为两个,分别设置在头罩的两端,鸭翼采用中等后掠角梯形翼;弹身中后段位于头罩后端,采用圆形截面等直段;弹翼为两个,分别设置在弹身中后段两侧;级间过渡舱串联连接任务级与助推器;助推器弹身位于级间过渡舱后端,采用圆形截面等直段;旋转尾翼为四个,设置于助推器弹身尾部;副翼为两个,分别设置在弹身后段两侧并位于弹翼后缘端;立尾为燕形立尾,分别设置在弹翼翼尖两端。该外形能够使靶标实现宽速域范围飞行,同时该气动外形的靶标在超音速大机动飞行时气动性能优异,操纵性能好,填补了超音速大机动靶标领域的空白,能够满足新型武器鉴定和战训的需求。


    Access

    Download


    Export, share and cite



    Title :

    Aerodynamic appearance structure of supersonic high-maneuverability target


    Additional title:

    一种超音速大机动靶标气动外形结构


    Contributors:
    YU YUNFENG (author) / HAN SHANSHAN (author) / LI HONGJUN (author) / QIU SHAOHUA (author) / FENG XIAOQIANG (author) / GUO XIAOWEN (author) / FAN YONGHUA (author) / LIU CHANG'AN (author)

    Publication date :

    2022-03-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aerodynamic layout of supersonic high-maneuverability stealth target

    HAN SHANSHAN / FENG XIAOQIANG / QUAN JINGGE et al. | European Patent Office | 2022

    Free access

    CFD Aerodynamic Characterization of a High Maneuverability Airframe

    Coyle, Craig J. / Silton, Sidra I. | AIAA | 2015


    High-stealth high-maneuverability unmanned target drone

    WANG LING | European Patent Office | 2022

    Free access

    CFD Aerodynamic Characterization of a High Maneuverability Airframe (AIAA 2015-3015)

    Coyle, Craig J. / Silton, Sidra I. | British Library Conference Proceedings | 2015


    High-maneuverability submersible

    WU BINGFA / WU DANHUI | European Patent Office | 2016

    Free access