Structural Testing and Analysis of a Joined Wing Technology Demonstrator

Abstract

This report covers the load testing, subsequent structural failure, redesign, and structural analysis of said redesign of the Air Vehicles Joined Wing Technology Demonstrator.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2004
Accession Number
ADA425641

Entities

People

  • Jason Robinson

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Airplanes
  • Aspect Ratio
  • Carbon Fibers
  • Construction
  • Contracts
  • Engineering
  • Graphitic Materials
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Software Testing
  • Structural Analysis
  • Three Dimensional
  • Vehicles

Readers

  • Aerospace logistics and air mobility.
  • Software Engineering
  • Structural Health Monitoring of Composite Structures.