Accession Number : ADA325972

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

Descriptive Note : Final rept.,

Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA

Personal Author(s) : Neu, Thomas F. ; Huang, Shih L.

PDF Url : ADA325972

Report Date : 15 NOV 1973

Pagination or Media Count : 80

Abstract : 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.

Descriptors :   *STRESS ANALYSIS, *GRAPHITE EPOXY COMPOSITES, *SANDWICH CONSTRUCTION, *COMPOSITE WINGS, VIBRATION, FINITE ELEMENT ANALYSIS, DESIGN CRITERIA, WEIGHT REDUCTION, MARGIN OF SAFETY.

Subject Categories : Aircraft
      Laminates and Composite Materials
      Mfg & Industrial Eng & Control of Product Sys

Distribution Statement : APPROVED FOR PUBLIC RELEASE