Studies of generic aircraft configurations to determine the payoff of thrust vectoring for direct lift during STOL landings and takeoff and for control power augmentation during weapons-delivery maneuvers are described. Results show that for a nominal 1000-foot landing distance, direct-lift benefits are small, but significant improvements in control power augmentation contribute to payoffs in takeoff distance and recovery from roll-pitch-coupling-induced departures at high angles of attack.


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    Titel :

    Application of thrust vectoring for STOL


    Beteiligte:
    Whitten, P. D. (Autor:in) / Woodrey, R. W. (Autor:in) / Hames, J. E. (Autor:in)

    Kongress:

    V/STOL Conference ; 1981 ; Palo Alto, CA


    Erscheinungsdatum :

    1981-12-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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