Static and Dynamic Formulation of a Symmetrically Laminated Beam Finite Element for a Microcomputer.

Abstract

This paper is to introduce a formulation, an efficient solution procedure, a microcomputer program, and a graphics routine for an anisotropic symmetrically laminated beam finite element including the effect of shear deformation. The emphasis of the formulation and solution procedure is for simplicity, efficiency, and easy implementation in microcomputers. The element possesses six d.o.f.'s at each of the two nodes: transverse deflection and slope due to bending and shear, respectively; and a twisting angle and its derivative with respect to the beam axis.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1985
Accession Number
ADA170885

Entities

People

  • Alex T. Chen
  • T. Y. Yang

Organizations

  • Purdue University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Aspect Ratio
  • Bending Moments
  • Cantilever Beams
  • Composite Materials
  • Computer Programs
  • Computers
  • Materials
  • Materials Laboratories
  • Mechanics
  • Modulus Of Elasticity
  • Personal Computers
  • Resonant Frequency
  • Transverse
  • Two Dimensional

Readers

  • Computational Fluid Dynamics (CFD)
  • Computer Science.
  • Mechanical Engineering/Mechanics of Materials.