Stess Analysis of Landing Gear XB-36,

Abstract

A stress analysis has been made of the landing gear of the XB-36 bomber to determine whether or not the gear meets the requirements of existing criteria. The report is divided into two parts, one of which deals with the main landing gear and the other dealing with the nose gear. Descriptive matter for each gear appears under its respective analysis. Results of the analysis are shown in tables, diagrams, and formulas.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1948
Accession Number
ADB812167

Entities

People

  • D. A. Redwine
  • W. W. Brown

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Landing Gear
  • Nose Wheels
  • Stress Analysis
  • Stresses
  • Word Processors

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Aviation Science / Aeronautics.
  • Computer Science.