Residual Strength Test on Stiffened Panels With Multiple-Site Damage

Abstract

In Federal Aviation Administration and the Netherlands Department of Civil Aviation (FAA/RLD) collaboration, residual strength tests were carried out on stiffened panels with multiple-site damage (MSD). The main purpose of this test program was to generate experimental data to verify tools to predict the residual strength of such panels. In this report these tests are described and the results are presented in such a way that they can be used to verify new and existing models.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1999
Accession Number
ADA361537

Entities

People

  • A. L. Michielsen
  • H. J. Tenhoeve
  • H. Vlieger
  • L. Schra

Organizations

  • National Aerospace Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Actuators
  • Aluminum
  • Civil Aviation
  • Computer Programs
  • Computers
  • Crack Tips
  • Load Control
  • Materials
  • Measurement
  • Mechanical Properties
  • Modulus Of Elasticity
  • Plastic Properties
  • Resistance
  • Stiffness
  • Strain Gages
  • Stress Strain Relations
  • Stresses

Readers

  • European Security and Defence Policy (ESDP).
  • Structural Health Monitoring of Composite Structures.