Stress Analysis by Recurrence Formula of Reinforced Circular Cylinders under Lateral Loads

Abstract

A recurrence formula is developed for the stress analysis of reinforced circular cylinders loaded in the planes of their rings. In contrast to the elementary engineering analysis, deformations of rings and sheet are considered. The recurrence formula in conjunction with appropriate boundary equations can be used to obtain sets of simultaneous linear algebraic equations. The solutions of these equations enable the stress analyst to find the shear flows and direct stresses in the sheet, as well as the shear forces, axial forces, and bending moments in the rings. In order to reduce the amount of computation involved in the stress analysis of relatively long reinforced cylinders, an approximate method of analysis is presented. In this method the cylinder under the consideration is assumed to be infinitely long, and the recurrence formula is treated as a fourth-order finite-difference equations. It is recommended that the approximate solution be utilized for the stress analysis of cylinders loaded at rings located two or more bays from external restraints.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1947
Accession Number
ADA801341

Entities

People

  • John E. Duberg
  • Joseph Kempner

Organizations

  • National Advisory Committee for Aeronautics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Bending Moments
  • Bending Stress
  • Boundaries
  • Computations
  • Difference Equations
  • Engineering
  • Equations
  • Flow
  • Linear Algebraic Equations
  • Modulus Of Elasticity
  • Shear Flow
  • Shear Modulus
  • Shear Stresses
  • Simultaneous Equations
  • Stress Analysis
  • Stresses
  • Structural Components

Readers

  • Calculus or Mathematical Analysis
  • Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics