The invention discloses a modular design method for a hypersonic cruise aircraft, and relates to the technical field of aircraft design, and the technical scheme is characterized in that based on a plurality of reference conical flow fields, the layout configuration of the aircraft is subjected to segmented design in the longitudinal direction, and the aircraft is divided into a front body, a center body and wings according to functions; and the front body, the center body and the wings are independently designed according to requirements, so that different flight requirements can be met. The multi-component design of the hypersonic aircraft is realized on the basis of a plurality of reference conical flow fields, so that the aircraft can have the performance of a traditional waverider, the design parameters of different components can be changed, the design parameters of the aircraft are diversified and convenient to adjust, the block design processing of the hypersonic aircraft can be realized, and the design cost is reduced. And the method has better engineering application value.

    本发明公开了一种高超声速巡航飞行器模块化设计方法,涉及飞行器设计技术领域,其技术方案要点是:以多个基准圆锥流场基础,将飞行器布局构型沿着纵向进行分段设计,并根据功能分为前体、中心体和机翼,实现飞行器部件分段分块的模块化设计,且前体、中心体和机翼根据需求单独设计,供适应不同飞行需求。本发明以多个基准圆锥流场基础实现高超飞行器的多部件设计,不但可以保证飞行器具有传统乘波体性能,又能改变不同部件的设计参数,使得飞行器设计参数多样化且便于调整,可实现高超声速飞行器的分块设计加工,具有更好的工程应用价值。


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    Title :

    Modular design method for hypersonic cruise aircraft


    Additional title:

    一种高超声速巡航飞行器模块化设计方法


    Contributors:
    CHEN LILI (author) / HOU ZHONGXI (author) / GUO ZHENG (author) / HUANG JIANGTAO (author) / LIU JIANXIA (author) / WANG WENKAI (author) / ZHONG SHIDONG (author)

    Publication date :

    2022-07-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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



    Handling qualities of hypersonic cruise aircraft

    Walker, H. J. / Thompson, M. O. | NTRS | 1967


    Boundary-layer transition on hypersonic-cruise aircraft

    Czarnecki, K. R. / Allen, J. M. / Jackson, M. W. | NTRS | 1967