Paper shows that variable sweep compensates for environment of SST and provides solutions to stability and control problems; landing configuration (wings forward) approximates that of moderately swept conventional airplane; high span in low-speed configuration is compatible with good roll control; low roll inertia in high-speed configuration allows high roll acceleration; landing configuration has stable thrust-speed relationship; motions of aerodynamic center caused by wing sweep, Mach number, and aeroelastic distortion can be played against each other to minimize trim drag and to maintain good maneuverability.


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    Titel :

    Effect of variable sweep on supersonic transport handling qualities


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Higgins, H.C. (Autor:in) / Shomber, H.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Boeing variable-sweep supersonic transport

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


    Variable sweep -- Application to supersonic transport

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


    Variable sweep -- Application to supersonic transport

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