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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    Titel :

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


    Beteiligte:
    A. R. Somoroff (Autor:in) / H. Rubin (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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