STRESS REPORT, NOSE LANDING GEAR ASSEMBLY

Abstract

The report consists of data substantiating the structural integrity of the nose landing gear assembly and the trunnion pins required for attachment to the airplane.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1963
Accession Number
AD0648007

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Aircrafts
  • Army Aviation
  • Bending Moments
  • Bending Stress
  • California
  • Department Of Defense
  • Department Of Veterans Affairs
  • Government Procurement
  • Governments
  • Landing Gear
  • Modulus Of Elasticity
  • Nose Wheels
  • Research Aircraft
  • Shear Modulus
  • Shear Stresses
  • Stresses
  • United States Government

Readers

  • Aerospace Engineering
  • ballistics.