FEASIBILITY OF JOINING ADVANCED COMPOSITE FLIGHT VEHICLE STRUCTURES.

Abstract

The purpose of this study is to establish the feasibility of using rational engineering methods to design bonded and mechanically fastened joints fabricated from composite and composite-metal adherends. Work during this quarter has concentrated on Literature Survey and selection and computer programming of analytical expressions to be used in the design methods. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 19, 1966
Accession Number
AD0801465

Entities

People

  • Dieter Kutscha

Organizations

  • IIT Research Institute

Tags

DTIC Thesaurus Topics

  • Composite Materials
  • Computer Programming
  • Computers
  • Computing-Related Activities
  • Engineering
  • Literature
  • Literature Surveys

Readers

  • Reinforced Composite Materials
  • Systems Analysis and Design