The high subsonic and transonic characteristics of fighter aircraft and the factors affecting aerodynamic boundaries, such as maximum obtainable lift, buffet onset, pitchup, wing rock, and nose slice are discussed. Investigations were made using a general research configuration which encompassed a systematic matrix of wing design parameters. These results emphasized the sensitivity to section and planform geometry at the selected design point. The incorporation of variable-wing-geometry devices in the form of leading-edge slats or flaps was shown in a number of flight and wind-tunnel studies to provide controlled flow over a wide range of flight conditions and substantial improvements in maneuver capabilities. Additional studies indicated that the blending of a highly swept maneuver strake with an efficient moderately swept wing offers a promising approach for improving maneuver characteristics at high angles of attack without excessive penalties in structural weight.


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    Titel :

    Maneuver and buffet characteristics of fighter aircraft


    Beteiligte:
    Ray, E. J. (Autor:in) / Mckinney, L. W. (Autor:in) / Carmichael, J. G. (Autor:in)


    Erscheinungsdatum :

    01.11.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Maneuver and buffet characteristics of fighter aircraft

    Ray, Edward J. / MacKinney, Linwood W. / Carmichael, Julian G. | TIBKAT | 1973


    Maneuver and Buffet Characteristics of Fighter Aircraft

    E. J. Ray / L. W. Mckinney / J. G. Carmichael | NTIS | 1973


    Maneuver and buffet characteristics of fighter aircraft

    Ray, E. J. / Mckinney, L. W. / Carmichael, J. G. | NTRS | 1973


    Airbrake-Induced Fin-Buffet Loads On Fighter Aircraft

    Breitsamter, Christian / Schmid, Arne | AIAA | 2008


    Airbrake-Induced Fin-Buffet Loads on Fighter Aircraft

    Breitsamter, C. | Online Contents | 2008