Whilst all published information on the arrow wing concept for future Supersonic Transport designs has, in general, placed considerable importance on the benefits of this particular layout, we should now be investigating ways and means in which the theorising and experimenting may be supplanted by active in-flight research.


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    Titel :

    The Arrow Wing


    Untertitel :

    Its potentialities and drawbacks with regard to in-flight aerodynamic research


    Beteiligte:


    Erscheinungsdatum :

    1977-08-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Lift force of arrow-shaped wing

    Gurevich, M.I. | Engineering Index Backfile | 1949


    Scar Arrow-Wing Active Flutter Suppression System

    C. K. Gordon / O. E. Visor | NTIS | 1977


    SCAR arrow-wing active flutter suppression system

    Gordon, C. K. / Visor, O. E. | NTRS | 1977