Fundamental aerodynamic, performance, and operational considerations which Boeing integrated into design of SST as result of 11,000 wind tunnel test hours on variable sweep; variable sweep SST factors and improved operational characteristics achieved, such as shorter takeoff and landings, lower takeoff and approach noise, and lower takeoff and landing speeds; smaller gross weight aircraft with smaller engines for given payload range mission is result of superior aerodynamic performance when compared to low aspect ratio fixed geometry approach; economics compare favorably with present subsonic jets. (see also Shell Aviation News n 317 1964 p 6-11)


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    Titel :

    Variable sweep -- Application to supersonic transport


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Swihart, J.M. (Autor:in) / Goodmanson, L.T. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Supersonic



    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Variable sweep -- Application to supersonic transport

    Swihart, J.M. / Goodmanson, L.T. | Engineering Index Backfile | 1964


    Variable Sweep - Application to the Supersonic Transport

    Swihart, John M. / Goodmanson, Lloyd T. | SAE Technical Papers | 1964


    Boeing variable-sweep supersonic transport

    Swihart, J.M. / Goodman, L.T. | Engineering Index Backfile | 1965


    The Boeing Variable-Sweep Supersonic Transport

    Swihart, J.M. / Goodman, L T. | Emerald Group Publishing | 1965