Effect of Ratio of Rivet Pitch to Rivet Diameter on the Fatigue Strength of Riveted Joints of 24S-T Aluminum-Alloy Sheet

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1946
Accession Number
ADA801043

Entities

People

  • David W. Ochiltree
  • Harold Crate
  • Walter T. Graves

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Diameters
  • Electrical Resistance
  • Elements
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Joints
  • Mechanical Properties
  • Riveted Joints
  • Rivets
  • Static Loads
  • Tensile Strength
  • Thickness