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

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.

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Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1973
Accession Number
ADA325972

Entities

People

  • Shih L. Huang
  • Thomas F. Neu

Organizations

  • Naval Air Warfare Center Warminster

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Aerial Targets
  • Aircrafts
  • Composite Materials
  • Composite Wings
  • Epoxy Composites
  • Fabrication
  • Graphite Epoxy Composites
  • Graphitic Materials
  • Honeycomb Cores
  • Intellectual Property
  • Laminates
  • Materials Processing
  • Network Protocols
  • Plastic Explosives
  • Shear Stresses
  • Stress Analysis
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Reinforced Composite Materials
  • Unmanned Aerial System (UAS) Autonomous Capabilities and Mission Reconnaissance.

Technology Areas

  • 5G