Tension-Tension Fatigue Investigation of High Strength Aircraft Bolts Effect of Nut Engagement and Thread Root Radius

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Document Details

Document Type
Technical Report
Publication Date
Feb 15, 1958
Accession Number
AD0155865

Entities

People

  • Corey Crisphi
  • Edward F. Gowen Jr.
  • Thomas C. Baumgartner

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Alloys
  • Diameters
  • Dynamic Loads
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Heat Treatment
  • Materials
  • Measurement
  • Mechanical Properties
  • Self Assembly
  • Standards
  • Stress Concentration
  • Stresses
  • Tensile Strength
  • Tensile Stress
  • Test Equipment
  • Yield Strength