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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:
    T. F. Neu (author) / S. L. Huang (author)

    Publication date :

    1973


    Size :

    80 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    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