EFFECT OF DAMPING CONSTANTS AND STRESS DISTRIBUTION ON THE RESONANCE RESPONSE OF MEMBERS

Abstract

The amplitade of vibration of a member at resonance, as defined by its resonance amplification factor, is analyzed in relationship to the damping properties of materials. Data are presented on damping energy to indicate the effect of stress magnitude, stress history and temperature. Based on the mathematical relationship found to exist between damping and stress magnitude the resonance amplification factors ars determined for a variety of direct stress members and beams. It is shown that the amplification in vibration caused by resonance may be considered to be the product of three basic factors: (a) the mathematical factor, (b) the cross-sectional shape factor, and (c) the longitudinal stress distribution factor. The first of these factors may be calculated from the damping and dynamic modulus properties of the material and the last two from the shape and loading characteristics of the member. Diagrams are presented to show these basic factors as functions of the damping exponent and other variables for members commonly encountered in engineering practice. Experimental data are presented to confirm the equations derived for resonance amplification factors of members having various shapes and stress distribution.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1952
Accession Number
AD0003566

Entities

People

  • B. J. Lazan

Organizations

  • University of Minnesota

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Bending Stress
  • Cantilever Beams
  • Elastic Properties
  • Engineering
  • Engineers
  • Machines
  • Materials
  • Materials Laboratories
  • Mechanical Properties
  • Mechanics
  • Minnesota
  • Modulus Of Elasticity
  • New York
  • Stresses
  • United States
  • Universities

Fields of Study

  • Engineering
  • Physics

Readers

  • Plasma Physics / Magnetohydrodynamics
  • Regression Analysis.
  • Structural Health Monitoring of Composite Structures.