Research on Energy Absorbing Structures. Part 11

Abstract

A numerical method for analyzing large deflections of shells of revolution under axisymmetric loading with arbitrary creep characteristics is given. Creep strain is treated as an equivalent external loading. Two nonlinear differential equations similar to Reissner's equations are presented and solved by the iterative scheme and the finite difference approximation. The multiaxial stress-strain-time relationship is formulated from the empirical uniaxial curve based on the second deviated stress and strain invariants. Examples are given for a corrugated tube subject to an axial load at an elevated temperature. The results show the nonlinear effects due to finite strain and creep strain. The method shown may also be applied to axisymmetric shells subject to thermal and plastic strains.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1973
Accession Number
AD0760161

Entities

People

  • Bernard Mazelsky
  • Sheng-rong Lin
  • Shih-chang Liu
  • Tung Hua Lin

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Aluminum Alloys
  • Axial Loads
  • Creep
  • Differential Equations
  • Equations
  • Fatigue Life
  • Grain Size
  • Lepidoptera
  • Materials
  • Mechanical Working
  • Mechanics
  • Nonlinear Differential Equations
  • Residual Stress
  • Shear Stresses
  • Strain Hardening

Fields of Study

  • Engineering
  • Physics

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Structural Dynamics.