The Effect of Internal Pressure on the Buckling Stress of Thin-Walled Circular Cylinders under Torsion

Abstract

Tests indicates that internal pressure raises the shear buckling stress. Formula was developed to represent approximately the buckling of a cylinder of moderate length under the combined effects of torsion and internal pressure. This formula makes use of the ratio of critical shear stress with internal pressure to critical shear stress without internal pressure and the ratio of internal pressure to the critical pressure in the absence of torsion.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1944
Accession Number
ADB225433

Entities

People

  • George W. Baab
  • Harold Crate
  • S. B. Batdorf

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircraft Industry
  • Aircrafts
  • Aluminum Alloys
  • Buckling
  • Elastic Properties
  • Equations
  • Experimental Data
  • Internal Pressure
  • Mechanics
  • Modulus Of Elasticity
  • Shear Modulus
  • Shear Stresses
  • Strain Gages
  • Stresses
  • Walls

Readers

  • Combustion and Flow Dynamics.
  • Structural Health Monitoring of Composite Structures.