STABILITY AND RESPONSE OF CYLINDRICAL SHELLS TO MOVING LOADS

Abstract

The stability of a circular cylindrical shell subjected to a moving ring load with a constant velocity was examined in detail when both longitudinal and transverse inertia effects are included, using both the Timoshenko and the Flugge equations. A lower resonance speed has been found, which apparently has been concealed in a recent paper.

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Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1963
Accession Number
AD0403001

Entities

People

  • John P. Jones
  • Pravin G. Bhuta

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aerospace Craft
  • Air Force
  • Air Force Facilities
  • Amplification
  • Axisymmetric
  • Deflection
  • Differential Equations
  • Displacement
  • Dynamic Response
  • Equations
  • Equations Of Motion
  • Instability
  • Integrals
  • Modulus Of Elasticity
  • Space Systems
  • Steady State
  • Vehicles

Fields of Study

  • Physics

Readers

  • Structural Dynamics.