RESEARCH IN AIRCRAFT STRUCTURES ANALYSIS AND DESIGN

Abstract

The paper outlines new approaches to the experimental study of the instability of shell bodies and provides fresh analyses in this field. It abstracts from recent extensions to the maximum strength analysis for flat plates and gives an outline of a generalization in the theory of buckling of sandwich plates. It refers to research efforts on the stability of conical shells and indicates progress in studies of the influence of higher order linear and nonlinear effects on the lateral vibrations of solid and sandwich beams.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1965
Accession Number
AD0622585

Entities

People

  • Jean Mayers
  • Wilfred H. Horton

Organizations

  • Stanford University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aeronautics
  • Aircrafts
  • Army Aviation
  • Astronautics
  • Classification
  • Commerce
  • Contracts
  • Security
  • Standards
  • Vehicles

Readers

  • Aerodynamics/Aeronautics.
  • Structural Health Monitoring of Composite Structures.
  • Technical Research and Report Writing.