A final aeroelastic analysis of the NAVAIRDEVCEN advanced graphite-epoxy composite wing for the unmanned supersonic BQM-34E aerial target indicates flutter free behavior within the 15% margin flight envelope. The wing is also divergent free throughout the flight regime and exhibits an expected forward and inboard shift of the aerodynamic center of pressure. (Author)


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    Title :

    NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E: Aeroelastic Analysis


    Contributors:
    A. R. Somoroff (author) / H. Rubin (author)

    Publication date :

    1973


    Size :

    19 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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