A brief outline of augmentor wing research sponsored by Ames Research Center is presented and is followed by a discussion of large-scale wind-tunnel test results for a swept augmentor wing configuration. The results showed that the augmentor wing could be applied to high-speed swept wing designs with little adverse effect on either the basic performance of the augmentor or the longitudinal characteristics, including maximum lift and stall. Three lateral control devices were shown to be effective and ground effect was measured for several complete aircraft configurations.


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    Titel :

    Aerodynamic characteristics of a swept augmentor wing


    Beteiligte:
    Koenig, D. G. (Autor:in) / Falarski, M. D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Characteristics of a Swept Augmentor Wing

    D. G. Koenig / M. D. Falarski | NTIS | 1972


    Aerodynamic characteristics of a swept augmentor wing

    Koenig, D. G. / Falarski, M. D. | NTRS | 1972


    Advanced augmentor-wing research

    Aiken, T. N. | NTRS | 1972


    Wing and Thrust Augmentor

    H. J. P. von Ohain / W. S. Campbell | NTIS | 1971


    The Transonic Multifoil Augmentor Wing

    J.E. Farbridge / Ronald C. Smith | AIAA | 1978