Stability of Honeycomb Sandwich Cylinders,

Abstract

This paper treats the instability of a honeycomb sandwich cylinder under axial compression, torsion and external lateral pressure. The simply supported honeycomb-sandwich cylinder considered here has face sheets of equal thickness and an isotropic honeycomb core. Curves are presented for the cases of axial compression and lateral pressure only, as well as torsion only. The combined case is handled by means of interaction equations based on the curves shown.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1961
Accession Number
ADA307463

Entities

People

  • Don Y. Konishi
  • Mehmet O. Kiciman

Tags

DTIC Thesaurus Topics

  • Axial Loads
  • Bending Stress
  • Buckling
  • Compression
  • Deflection
  • Department Of Defense
  • Digital Computers
  • Engineering
  • Engineers
  • Equations
  • Honeycomb Cores
  • Mechanical Engineering
  • Modulus Of Elasticity
  • Sandwich Construction
  • Simultaneous Equations
  • Stresses
  • Thickness

Readers

  • Structural Dynamics.