An Alternative Closed-Form Stress Intensity Solution for Single Part-Through and Through-the-Thickness Cracks at Offset Holes

Abstract

This report describes work performed to develop a new closed-form stress intensity solution for single cracks at non-centered (offset) holes in plates. The solution is compared to hundreds of finite element and boundary element models and is shown to be in very good agreement.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1998
Accession Number
ADA363701

Entities

People

  • James A. Harter

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Agreements
  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Aircrafts
  • Boundaries
  • Diameters
  • Equations
  • Geometry
  • Intensity
  • Mechanics
  • Military Research
  • Numbers
  • Stresses
  • Structural Integrity
  • Thickness

Readers

  • Fluid Dynamics.
  • Mathematics or Statistics
  • Structural Health Monitoring of Composite Structures.