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

摘要

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.