Results from transonic flutter model studies are presented. The flutter model was constructed to support the flutter prevention and clearance program from preliminary design through flight flutter tests. The model tests were conducted in the Langley transonic dynamics tunnel. The large full span free-flying model was shown to be an effective tool in defining airplane flutter characteristics by demonstrating freedom from flutter for most configurations and by defining optimum solutions for a few troublesome configurations.


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    Title :

    F-16 Flutter Model Studies with External Wing Stores


    Contributors:

    Publication date :

    1977


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    F-16 flutter model studies with external wing stores

    Foughner, J. T., Jr. / Bensinger, C. T. | NTRS | 1977


    F-16 flutter model studies with external wing stores

    Foughner, J. T., Jr. / Bensinger, C. T. | NTRS | 1977


    Flutter study of an advanced composite wing with external stores

    COLE, STANLEY / RIVERA, JR., JOSE / NAGARAJA, K. | AIAA | 1987


    Flutter study of an advanced composite wing with external stores

    Cole, Stanley R. / Rivera, Jose A., Jr. / Nagaraja, K. S. | NTRS | 1987