The dynamic stability and control characteristics of a four-engine turbofan transport model having an upper-surface blown jet flap were investigated by means of the free-flight technique in the Langley full-scale tunnel. The flight characteristics of the model were investigated through a range of lift coefficients from 3 to 8 with all four engines operating and with one outboard engine not operating. Static characteristics were investigated by conventional power-on force tests over the flight-test angle-of-attack range and through the stall.


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    Titel :

    Free-flight wind-tunnel investigation of a four-engine sweptwing upper-surface blown transport configuration


    Beteiligte:
    Parlett, L. P. (Autor:in)

    Erscheinungsdatum :

    01.08.1977


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :