Crack Growth and Stress Intensity Prediction Techniques. Delivery Order 0004: Implementing Models and Libraries

Abstract

The challenges of designing modern aircraft continue to drive the development of more advanced analytical tools; often these more advanced analytical tools themselves require development of other enabling technologies such as powerful computers and associated software. The primary historical objective of this project was to develop the infrastructure and to demonstrate that key enabling technologies such as faster and bigger personal computers, as well as database and programming software, have evolved to the point that more advanced analytical tools for analyzing the damage tolerance of aircraft structures are now possible.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2006
Accession Number
ADA467841

Entities

People

  • Craig Brooks
  • Kyle Honeycutt
  • Scott P. Domasky

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircraft Industry
  • Aircrafts
  • Computer Programming
  • Computer Programs
  • Computers
  • Damage Tolerance
  • Finite Element Analysis
  • Fracture (Mechanics)
  • Infrastructure
  • Intensity
  • Mechanics
  • Modulus Of Elasticity
  • Operating Systems
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Computer science

Readers

  • Software Engineering.
  • Structural Health Monitoring of Composite Structures.
  • Systems Analysis and Design