This paper describes the conceptual design of an airplane having a low aspect ratio wing with fuselages that are attached to each wing tip. The concept is proposed for a high-capacity transport as an alternate to progressively increasing the size of a conventional transport design having a single fuselage with cantilevered wing panels attached to the sides and tail surfaces attached at the rear. Progressively increasing the size of conventional single body designs may lead to problems in some area's such as manufacturing, ground-handling and aerodynamic behavior. A limited review will be presented of some past work related to means of relieving some size constraints through the use of multiple bodies. Recent low-speed wind-tunnel tests have been made of models representative of the inboard-wing concept. These models have a low aspect ratio wing with a fuselage attached to each tip. Results from these tests, which included force measurements, surface pressure measurements, and wake surveys, will be presented herein.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An Airplane Design having a Wing with Fuselage Attached to Each Tip


    Beteiligte:

    Kongress:

    39th AIAA Aerospace Sciences Meeting and Exhibit ; 2001 ; Reno, NV, United States


    Erscheinungsdatum :

    2001-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch






    An Airplane Design having a Wing with a Fuselage Attached to Each Tip

    Spearman, M. L. / AIAA | British Library Conference Proceedings | 2001


    Rear fuselage of airplane

    LI YAOHUA / SHU ZHAOXIN / OUYANG DI | Europäisches Patentamt | 2022

    Freier Zugriff

    Airplane with a fuselage having side outgrowth delimiting storage spaces

    GALLANT GUILLAUME / DELAHAYE ROMAIN | Europäisches Patentamt | 2017

    Freier Zugriff