A method of designing an aircraft shape of a supersonic aircraft according to an embodiment of the present invention includes: obtaining an equivalent cross-sectional area distribution of an initial shape at an off-track position of an aircraft; setting a target equivalent cross-sectional area distribution at the off-track position of the aircraft for reducing sonic booms on the basis of the obtained equivalent cross-sectional area distribution; and converting, on the basis of a required additional cross-sectional area distribution that is a difference between the equivalent cross-sectional area distribution and the target equivalent cross-sectional area distribution, a required additional cross-sectional area of a cross-section of the aircraft on an off-track Mach plane that extends through an arbitrary position in an airflow direction into a required additional cross-sectional area of a cross-section of the aircraft on an on-track Mach plane of the aircraft that is located near the off-track Mach plane and adding the required additional cross-sectional area of the cross-section of the aircraft on the on-track Mach plane.


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    Titel :

    METHOD OF DESIGNING AIRFRAME SHAPE OF SUPERSONIC AIRCRAFT, METHOD OF PRODUCING SUPERSONIC AIRCRAFT, AND SUPERSONIC AIRCRAFT


    Weitere Titelangaben:

    VERFAHREN ZUM ENTWURF DER FLUGWERKFORM VON ÜBERSCHALLFLUGZEUGEN, VERFAHREN ZUR HERSTELLUNG VON ÜBERSCHALLFLUGZEUGEN UND ÜBERSCHALLFLUGZEUG
    PROCÉDÉ DE CONCEPTION DE LA FORME D'UNE CELLULE D'UN AÉRONEF SUPERSONIQUE, PROCÉDÉ DE PRODUCTION D'UN AÉRONEF SUPERSONIQUE, ET AÉRONEF SUPERSONIQUE


    Beteiligte:
    UENO ATSUSHI (Autor:in)

    Erscheinungsdatum :

    2024-03-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung