The invention discloses an extremely-simple supersonic flying wing layout aircraft, and particularly relates to the field of aerodynamic design of aircrafts. An extremely-simple supersonic flying wing layout aircraft comprises a fuselage and two wings integrated with the fuselage, the front edge of the aircraft adopts a single sweepback type with a sweepback angle of 65 degrees, the rear edge of the aircraft is formed by inflection and splicing of three lambda shapes, and the sweepforward angles of the rear edge of the aircraft are all 28 degrees. By the adoption of the technical scheme, the problem of reasonable arrangement of the control surface of the full-tailless fighter is solved, and stable control over the full-tailless fighter can be achieved.

    本发明专利公开了一种极简超声速飞翼布局飞行器,具体涉及飞行器气动设计领域。一种极简超声速飞翼布局飞行器,包括机身和与机身融合一体的两幅机翼,所述飞行器的前缘采用后掠角为65°的单后掠型,所述飞行器的后缘采用三个“λ”型拐折拼接而成,所述飞行器后缘的前掠角均为28°。采用本发明技术方案解决了全无尾战斗机操纵面合理布置的问题,可实现全无尾战斗机的稳定控制。


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    Titel :

    Extremely-simple supersonic flying wing layout aircraft


    Weitere Titelangaben:

    一种极简超声速飞翼布局飞行器


    Beteiligte:
    HUANG JIANGTAO (Autor:in) / CHEN XIAN (Autor:in) / CHEN QISHENG (Autor:in) / YU LONGZHOU (Autor:in) / HE CHENGJUN (Autor:in) / ZHONG SHIDONG (Autor:in) / CHEN CHENG (Autor:in) / CHEN LILI (Autor:in) / WANG YINZHU (Autor:in) / DU XIN (Autor:in)

    Erscheinungsdatum :

    2021-06-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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