Stresses Around Central Holes in a Stiffened Orthotropic Strip

Abstract

This paper deals with the stress analysis of orthotropic panels with edge stiffeners and central holes, elliptical or circular in cross section. Stress profiles are obtained for fixed hole geometry as functions of stiffener geometry. Stress variations are also computed as functions of hole size for different stiffening geometries.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1975
Accession Number
ADA011255

Entities

People

  • Chatta Lakshmikantham

Organizations

  • United States Army Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Chemical Engineering
  • Complex Variables
  • Composite Materials
  • Engineering
  • Engineers
  • Materials
  • Materials Laboratories
  • Mechanical Engineering
  • Mechanics
  • Military Research
  • New York
  • Stiffening
  • Stress Analysis
  • Stresses
  • United States

Readers

  • Structural Dynamics.