Studies of Fatigue Crack Growth in Alloys Suitable for Elevated-Temperature Applications

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1965
Accession Number
ADA396923

Entities

People

  • C. M. Hudson

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Alloys
  • Aluminum Alloys
  • Axial Loads
  • Crack Propagation
  • Heat Treatment
  • Materials
  • Mechanical Working
  • Resistance
  • Stainless Steel
  • Supersonic Aircraft
  • Tensile Properties
  • Tensile Strength
  • Titanium
  • Titanium Alloys