Analysis of a Circular, Cylindrical Shell Loaded as a Simple Cantilever

Abstract

The stresses and deflections in a circular, cylindrical shell loaded at each end by a force and moment applied through rigid rings are presented. The shell may be stiffened by additional rings, and it is assumed that rapid changes in stress and deflection occur only in the axial direction in the immediate vicinity of a ring.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1961
Accession Number
ADB188325

Entities

People

  • H. E. Williams

Organizations

  • California Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautics
  • Boundaries
  • California
  • Coefficients
  • Contractors
  • Contracts
  • Deflection
  • Displacement
  • Engineering
  • Equations
  • Jet Propulsion
  • Membranes
  • Resistance
  • Revolutions
  • Rotation
  • Skeletal Muscle

Fields of Study

  • Physics

Readers

  • Structural Dynamics.