Investigation of Compressive-Creep Properties of Aluminum Columns at Elevated Temperatures. Part I

Abstract

An experimental investigation of the behavior of 24S-T4 (stabilized) aluminum columns at three elevated temperatures has been conducted. Tests were performed on long- and short-hinged-end columns of five slenderness ratios. By using an adjustable end eccentricity, it was possible to fix the eccentricity for a column of a given slenderness ratio and thereby obtain comparable results for different loads. Deflection measurements were taken at the mid-point throughout the duration of each test, and curves of deflection versus time with load as the parameter were obtained for each slenderness ratio. Test results indicate that, for a column of a given slenderness ratio and eccentricity, there is a limiting load below which collapse due to creep will not occur. It is concluded that this lower limit should be considered the limiting or allowable load. It is suggested that an approximate method of the type introduced in the report should be employed to determine this load.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1952
Accession Number
ADA076046

Entities

People

  • A. D. Schwope
  • R. L. Carlson

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aluminum Alloys
  • Bending Stress
  • Creep
  • Creep Tests
  • Elastic Properties
  • Materials Laboratories
  • Measurement
  • Mechanical Properties
  • Modulus Of Elasticity
  • Plastic Flow
  • Shape
  • Stress Strain Relations
  • Stresses
  • Tensile Properties
  • Tensile Stress
  • Yield Strength

Readers

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