Sudden Stretching of a Four-Layered Composite Plate.

Abstract

An approximate theory 0% laminated plates is developed by assuming that the extensional and thickness node 0% vibration are coupled.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1980
Accession Number
ADA302471

Entities

People

  • E. P. Chen
  • George C. Sih

Organizations

  • Lehigh University

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Composite Materials
  • Computer Programs
  • Computers
  • Engineering
  • Integral Equations
  • Jet Propulsion
  • Materials
  • Materials Laboratories
  • Mechanics
  • Navy
  • Physics Laboratories
  • Stress Analysis
  • Stress Strain Relations
  • Stresses

Fields of Study

  • Physics