TRANSVERSE VIBRATIONS OF NON-UNIFORM, FREE-FREE BEAMS.

Abstract

Transverse vibrations in one plane of a non-uniform, free-free beam are considered, which include the effects of rotary inertia, shear deflection, and a constant axial acceleration, which is provided by an axial thrust at one end of the beam. The equations of motion are derived. An energy formulation for approximate solution of the natural frequencies, and a matrix formulation for the approximate solution of the natural frequencies and mode shapes are derived, which include these effects. Both formulations are altered to give the critical axial acceleration for buckling. It is shown that rotary inertia, shear deflection, and axial acceleration all reduce the natural frequency of vibration, however the first two effects are important in short beams, while the latter effect is important in long slender beams.

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1962
Accession Number
AD0610230

Entities

People

  • William F. Bozich

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Buckling
  • Deflection
  • Equations
  • Equations Of Motion
  • Frequency
  • Frequency Shift
  • Mechanical Waves
  • Motion
  • Resonant Frequency
  • Transverse
  • Vibration
  • Waves

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Mechanics and Fluid Dynamics.