Vibrations of Axially Loaded Stiffened Cylindrical Shells. Part 1: Theoretical Analysis

Abstract

A method of analysis and a computer program were developed for determination of the frequencies and mode shapes of the free vibrations of stiffened cylindrical shells. The shells are stiffened by closely spaced stringers and rings, have different boundary conditions, and are subjected to either a static axial load or a hydrostatic pressure. The stiffeners are considered 'smeared' over the shell. The system of equations which was obtained is solved by a method known as the 'exact method'. The theoretical investigation includes a study of the variation in frequencies and mode shapes with increase in the static load until buckling. The results of the present analysis are compared to those of other methods which appear in the literature, and good agreement is obtained.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1974
Accession Number
AD0784917

Entities

People

  • Aviv Rosen
  • Josef Singer

Organizations

  • Technion – Israel Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Computer Programs
  • Contracts
  • Difference Equations
  • Differential Equations
  • Dynamic Response
  • Equations
  • Frequency
  • Geometry
  • Hydrostatic Pressure
  • Internal Pressure
  • Mechanics
  • Numerical Analysis
  • Resonant Frequency
  • Scientific Research
  • Three Dimensional
  • Vibration

Fields of Study

  • Engineering
  • Physics

Readers

  • Structural Dynamics.

Technology Areas

  • Space