Material Nonlinearity Effects in Optimization Considerations of Stiffened Cylinders and Interpretation of Test Data Scatter for Compressive Buckling

Abstract

A limited optimization study is undertaken of imperfect, eccentrically stiffened 2024-T3 aluminum alloy cylinders under axial compression based on (1) a linear theory with applied buckling load reduction factors to account for initial imperfections and inelasticity and (2) a kinematically and constitutively nonlinear maximum strength analysis. The latter is shown to be less conservative for the most efficient design: combined stringer- and ring- stiffening. Credibility of the maximum strength approach is domonstrated through its use in correlating experimental results obtained for 10- and 14-in. diameter steel cylinders having different proportional-limit stresses, respectively. Finally, material nonlinearity is shown to offer a plausible qualitative explanation for a significant amount of the scatter in axial compression tests for cylinders with radius-to-thickness ratios of practical interest.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1972
Accession Number
AD0743951

Entities

People

  • E. Meller
  • J. Mayers

Organizations

  • Stanford University

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Aluminum Alloys
  • Bending Stress
  • Composite Materials
  • Compression
  • Contracts
  • Failure Mode And Effect Analysis
  • Geometry
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Plastic Properties
  • Sandwich Construction
  • Shear Modulus
  • Stress Strain Relations

Fields of Study

  • Physics

Readers

  • Structural Dynamics.