The YF-16 and F-16 developmental wind tunnel test program was reviewed. Geometrical descriptions, general comments, representative data, and the initial efforts toward the development of design guides for the application of strakes to future aircraft are presented.


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    Title :

    Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience. Volume 1: Summary and analysis


    Contributors:
    Smith, C. W. (author) / Ralston, J. N. (author) / Mann, H. W. (author)

    Publication date :

    1979-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :