Vibrational Characteristics of Cracked Cantilever Plates.

Abstract

An analytical solution to the vibrational characteristics of a rectangular cantilever plate with a discontinuous boundary condition (crack) at the root is presented. Mechanical damping which may exist as a result of the contact between the crack's free surfaces during vibration has been eliminated by assuming the crack surface to be a free boundary. The approach to solution involves the use of the method of Ritz applied to Hamilton's Law of Varying Action. A comparison is made to the solution as obtained from conventional finite element theory (NASTRAN). No exact solution is available for comparison. The assumptions which underlie both theories are outlined. A comparison is made to the experimental results for a cantilever plate with a narrow slot of varying lengths at the root. Indications are that significant frequency deterioration and nodal pattern variations occur with increasing crack length. Further work on the effect of cracks/flaws on plate response is warranted.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1977
Accession Number
ADA046636

Entities

People

  • Jon S. Ogg

Tags

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  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aspect Ratio
  • Boundary Value Problems
  • Coordinate Systems
  • Eigenvalues
  • Equations
  • Frequency
  • Gas Turbines
  • Government Procurement
  • Governments
  • Kinetic Energy
  • Law
  • Mechanics
  • Power Series
  • Turbines
  • Vibration

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  • Materials Science (Mechanical Engineering).
  • Structural Dynamics.
  • Systems Analysis and Design