A direct design method for generating an osculating curved waverider based on a complex leading edge, includes obtaining a leading edgeleading edge through determining a leading edge of a waverider according to a spread length, a front-to-rear length, and a sweep angle at each position of an aircraft, and arranging leading-edge discrete points on the leading edgeleading edge; drawing a small shock cone corresponding to each leading-edge discrete point by starting from each leading-edge discrete point, taking a local shock angle as a half cone angle and taking a free streamline direction as an axis; finding envelope surfaces of all small shock cones, namely, a shock curved surface corresponding to the leading edgeleading edge; generating a waverider by using the osculating curved waverider design method.


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    Titel :

    DIRECT DESIGN METHOD FOR GENERATING OSCULATING CURVED WAVE-RIDER BASED ON COMPLEX LEADING-EDGE PROFILE


    Beteiligte:
    JIANG CHONGWEN (Autor:in) / LI ZHIHAO (Autor:in) / HU SHUYAO (Autor:in) / XU CHENHAO (Autor:in) / GAO ZHENXUN (Autor:in) / LI CHUNXUAN (Autor:in)

    Erscheinungsdatum :

    2024-06-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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



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