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 SAE -- Paper 858C for meeting Apr 27-30 1964 8 p)


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    Title :

    Variable sweep -- Application to supersonic transport


    Additional title:

    Shell Aviation News


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Variable sweep -- Application to supersonic transport

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


    Boeing variable-sweep supersonic transport

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


    Variable Sweep - Application to the Supersonic Transport

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


    The Boeing Variable-Sweep Supersonic Transport

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


    Effect of variable sweep on supersonic transport handling qualities

    Higgins, H.C. / Shomber, H.A. | Engineering Index Backfile | 1965