Stress Analysis of Inflatoplane Model GA-468

Abstract

Loads in the entire airframe (Government number YAO-3), including the wing, fuselage, engine mount, empennage, cockpit, and landing gear, are calculated and used to determine the stresses in these parts.

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Document Details

Document Type
Technical Report
Publication Date
Jan 18, 1961
Accession Number
AD0257896

Entities

Organizations

  • Goodyear Aerospace

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Doors
  • Aircrafts
  • Airframes
  • Bulkheads
  • Control Sticks
  • Engine Mounts
  • Fuselages
  • Landing Gear
  • Materials
  • Mechanical Structure
  • Mounts
  • Relief Valves
  • Spark Plugs
  • Stress Analysis
  • Stresses
  • Valves

Readers

  • Aerospace Engineering
  • Asian Economic Studies
  • Phased Array Antenna Design.