A weight saving of 54 percent has been achieved in the in-house design and fabrication of a composite wing for the BQM-34E aerial target vehicle. Design criteria are identical to those of the 5g production metal wing. Results of the stress analyses indicate adequate margins of safety.


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    Titel :

    NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E; Stress and Vibration Analysis


    Beteiligte:
    T. F. Neu (Autor:in) / S. L. Huang (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    80 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E: Static Test Results

    M. Libeskind / J. Minecci / S. L. Huang et al. | NTIS | 1973



    GRAPHITE-EPOXY WING FOR BQM-34E SUPERSONIC AERIAL TARGET

    MCQUILLEN, EDWARD / HUANG, SHIH | AIAA | 1970


    Graphite-Epoxy Wing for BQM-34E Supersonic Aerial Target

    EDWARD J. MC&UILLEN AND SHIH L. HUANG | AIAA | 1971