Innovative and conventional thrust vectoring moment balance mechanisms, as applied to advanced tactical fighters, are examined. The innovative mechanisms include thrust line translation, life line translation, and auxiliary power control; the conventional mechanisms under investigation are horizontal tails, canards, and variable sweep wings. These mechanisms are tested for their ability to provide negative static margins for landing approach or relocation of the vectored thrust line nearer the aircraft's center of gravity. The net pitching moment due to wing, flaps, and vectored thrust lift would then be small, making possible beneficial trim forces from small trimming devices. These innovative mechanisms are, however, possibly heavy and must be evaluated on their complexity, reliability, maintainability, and STOL capabilities. Several candidate fighter configurations are compared and evaluated.


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    Titel :

    Tactical STOL moment balance through innovative configuration technology


    Beteiligte:
    Eckard, G. J. (Autor:in) / Sutton, R. C. (Autor:in) / Poth, G. E. (Autor:in)

    Kongress:

    V/STOL Conference ; 1981 ; Palo Alto, CA


    Erscheinungsdatum :

    01.12.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Innovative concepts for tactical STOL

    ECKARD, G. / POTH, G. | AIAA | 1983


    STOL Tactical Aircraft Investigation. Volume I. Configuration Definition

    J. Hebert / C. Whitney / R. E. Johnston et al. | NTIS | 1973


    STOL Tactical Aircraft Investigation

    Hebert, Joseph | SAE Technical Papers | 1973


    Air Force STOL Tactical Transport Technology Program

    Oates, Garland S. / Lowry, Randall B. | SAE Technical Papers | 1971