Axial-Load Fatigue Properties of PH 15-7 Mo Stainless Steel in Condition TH 1050 at Ambient Temperature and 500 Degrees F

Abstract

Axial-load fatigue tests were conducted on notched and unnotched sheet specimens of PH 15-7 Mo stainless steel in Condition TH 1050. Fatigue lives at three mean stresses at ambient temperature (approx. 80 deg F) and at 500 deg F were determined throughout the lifetime range from 10(exp 2)to 10(exp 7) cycles. A special furnace incorporating guide plates is also described. A 500 deg F environment increased the fatigue limit but reduced the fatigue strength at short lifetimes. An effect of cyclic frequency was noted.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1964
Accession Number
ADA392801

Entities

People

  • Claude B. Castle
  • Walter Illg

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Alloys
  • Aluminum Alloys
  • Axial Loads
  • Chromium Alloys
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Frequency
  • Materials
  • Notch Sensitivity
  • Stainless Steel
  • Strain Gages
  • Stress Concentration
  • Stress Strain Relations
  • Tensile Properties
  • Tensile Strength

Fields of Study

  • Materials science

Readers

  • Mathematics or Statistics
  • Structural Health Monitoring of Composite Structures.
  • Thermal Physics or Thermal Science.