The invention provides a design method of a sweepback controllable double-sweepback osculating cone full waverider aircraft, which comprises the following steps of: designing a central body bus of a reference flow field, and solving position coordinates and flow parameters of each point in a flow field area and a shock wave molded line by applying a characteristic line theory; designing projection molded lines of the front edge and the air inlet lip of the aircraft on the horizontal plane, and defining the sweepback and the size of the aircraft; designing a shock wave outlet die line of the aircraft, and determining shock wave shapes and flow field parameters on each osculating plane and an included angle between the osculating plane and a vertical plane; the shape and position coordinates of the aircraft three-dimensional front edge molded line and the air inlet lip molded line are solved, and the position coordinates of the intersection points of the osculating planes and the aircraft front edge molded line and the air inlet lip molded line are obtained; a reference flow field in each osculating plane is solved, and streamlines on the molded surfaces of all the parts of the corresponding aircraft in the osculating planes are obtained through streamline tracking; and smoothly connecting the streamlines to obtain the basic configuration of the aircraft. The performance of the aircraft is guaranteed on the basis that the design freedom degree is improved.

    本发明提供了一种后掠角可控的双后掠吻切锥全乘波飞行器设计方法,包括:设计基准流场中心体母线,应用特征线理论求解流场区域和激波型线内各点位置坐标及流动参数;设计飞行器前缘、进气道唇口在水平面投影型线,定义后掠角大小以及飞行器尺寸;设计飞行器激波出口型线,确定各吻切面上激波形状与流场参数,以及与竖直面之间的夹角;求解飞行器三维前缘型线及进气道唇口型线的形状和位置坐标,获得各吻切面与飞行器前缘型线、进气道唇口型线交点的位置坐标;求解各吻切面内的基准流场,利用流线追踪获得吻切面内对应飞行器各部件型面上的流线;将流线平滑连接,获得飞行器的基本构型。本发明在提升设计自由度的基础上保证了飞行器的性能。


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    Titel :

    Design method of sweepback-angle-controllable double-sweepback osculating-cone full waverider aircraft


    Weitere Titelangaben:

    一种后掠角可控的双后掠吻切锥全乘波飞行器设计方法


    Beteiligte:
    WANG DOU (Autor:in) / WANG YI (Autor:in) / ZHOU CHUANGXIN (Autor:in) / TIAN JIAQI (Autor:in)

    Erscheinungsdatum :

    02.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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