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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    Titel :

    F-16 flutter model studies with external wing stores


    Beteiligte:

    Kongress:

    JTCG/MD Aircraft Stores Compatibility Symp. ; 1977 ; Fort Walton Beach, FL, United States


    Erscheinungsdatum :

    01.10.1977


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    F-16 Flutter Model Studies with External Wing Stores

    J. T. Foughner / C. T. Bensinger | NTIS | 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