Major considerations leading to development of L-1011 configuration selection, and operating requirements used in establishing basic design of airplane are presented; parametric study and design trade study together with airline operations feedback, systematically and rationally applied to requirements, configuration, and design have been extensively used; examples of selected studies; aerodynamic, propulsion, and guidance and control characteristics and their effect on flight operations and economics are examined. (07978)


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    Titel :

    Development of requirement, configuration and design for lockheed 1011 jet transport


    Weitere Titelangaben:

    SAE Paper


    Beteiligte:
    Magruder, W.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1968


    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    33 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Lockheed L-1011 TriStar

    Kappner, Ulrich | TIBKAT | 1993


    Anschluss verpasst : Lockheed L-1011 Tristar

    Hoeveler, Wolfdietrich | SLUB | 2001


    Flight controls for Lockheed L-1011

    Flapper, J.A. / Throndsen, E.O. | Engineering Index Backfile | 1968


    Development of The Lockheed L-1011's Flying Stabilizer

    Whitmore, C. A. | SAE Technical Papers | 1971