STRUCTURAL PROOF TEST PROGRAM

Abstract

The test program is designed to demonstrate integrity of aircraft structure and the information presented will be used to establish detail test procedures. The particular flight and landing load conditions to be simulated during test have been derived from structural analysis using the conditions specified in the Airplane Structural Design Criteria and have been found critical. A detailed listing of all test data requirements is given. The particular loads and reactions to be applied to the airframe and the major components are also given. Along with the strength tests, some additional control system tests are to be performed and are also described.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0640340

Entities

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Actuators
  • Aircrafts
  • Airframes
  • Airplanes
  • Army Aviation
  • Control Sticks
  • Control Systems
  • Fuselages
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Landing Gear
  • Landing Gear Doors
  • Load Distribution
  • Measurement
  • Nose Wheels
  • Spars

Readers

  • Pavement Materials Engineering.
  • Systems Analysis and Design