STRESS ANALYSIS MAIN LANDING GEAR

Abstract

The report consists of data substantiating the structural integrity of the main landing gear shock strut.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0654042

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Autonomy

DTIC Thesaurus Topics

  • Aircrafts
  • Assembly
  • Axial Loads
  • Bending Moments
  • California
  • Cams
  • Fittings
  • Joints
  • Landing Gear
  • Lift Fans
  • Machines
  • Research Aircraft
  • Shear Stresses
  • Stress Analysis
  • Stresses
  • Structural Integrity
  • Universal Joints