Development of MIL-HDBK-5 Design Allowable Properties and Fatigue-Crack Propagation Data for Several Aerospace Materials

Abstract

This final report describes a test program to determine certain missing MIL-HDBK-5 design allowable properties for 17-4PH bar, 15-5PH bar, and Alloy 188 sheet and to develop low stress intensity fatigue-crack-propagation data for 7075-T7351, 7475-T7351, and 2124-T851 plate.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1977
Accession Number
ADA054430

Entities

People

  • Paul E. Ruff
  • Samuel H. Smith

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aluminum Alloys
  • Bearing Strength
  • Computer Programs
  • Governments
  • Materials
  • Materials Laboratories
  • Measurement
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Physical Properties
  • Plastic Explosives
  • Stress Strain Relations
  • Tensile Modulus
  • Tensile Properties
  • Tensile Strength
  • Tensile Stress

Readers

  • Materials Science (Mechanical Engineering).
  • Materials Science and Engineering.
  • Software Engineering

Technology Areas

  • Space