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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    Title :

    Aerodynamic Characteristics of a Swept Augmentor Wing


    Contributors:

    Publication date :

    1972


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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