Methods developed permit computation of lift and drag of delta wings for large family of plan forms and thickness distributions; delta wing properly designed can be used to reduce minimum drag to roughly two thirds that of low aspect ratio rectangular wing, without impairing its lifting efficiency. Before Inst Aeronautical Sciences.


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    Titel :

    Aerodynamic performance of Delta wings at supersonic speeds


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Puckett, A.E. (Autor:in) / Stewart, H.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1947


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic performance of Delta wings at supersonic speeds

    Puckett, A.E. / Stewart, H.J. | Engineering Index Backfile | 1948


    Aerodynamic performance of Delta wings at supersonic speeds

    Puckett, A.E. / Stewart, H.J. | Engineering Index Backfile | 1948



    Aerodynamic Characteristics of Wings at Supersonic Speeds

    R. M. Snow / E. A. Bonney | NTIS | 1947


    Aerodynamic characteristics of rectangular wings at supersonic speeds

    Bonney, E.A. | Engineering Index Backfile | 1947