STRESS CONDITION OF AN OPEN THINWALLED MEMBER, WHICH IS MADE UP OF PLATES AND COVERS,

Abstract

A solution is given to the problem of bending of a thin walled structure made of three strips and two quarter circle cylindrical shells of infinite length. For arbitrary loads, the stress strain state of the structure is described by general linear equations of the thin plate bending theory, the plane problem of the elasticity theory, and the engineering theory of shells. The boundary conditions at the lines of junction between the plates and shells are used for the determination of constants entering into the general solutions of the respective equations. The development of the theory is complemented by a list of values of certain auxiliary functions. The theory is applied to the cases of C and shaped structures. The solutions may be used for the study of stresses in longerons of mobile freight elevators and other load carrying elements. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 27, 1970
Accession Number
AD0706654

Entities

People

  • N. P. Fleishman
  • Yu. H. Rozental

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundaries
  • Elastic Properties
  • Engineering
  • Equations
  • Mathematics

Fields of Study

  • Engineering

Readers

  • Structural Dynamics.