The YF-16 and F-16 developmental wind tunnel test program was reviewed and all force data pertinent to the design of forebody and nose strakes extracted. A complete set of these data is presented without analysis.


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    Title :

    Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience. Volume 2: Data base


    Contributors:

    Publication date :

    1978-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English