A brief outline of augmentor wing research is presented and is followed by a discussion of large scale wind tunnel test results for a swept augmentor wing configuration. The results show that the augmentor wing can 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. (Author)


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    Titel :

    Aerodynamic Characteristics of a Swept Augmentor Wing


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

    Erscheinungsdatum :

    1972


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aerodynamic characteristics of a swept augmentor wing

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