DC-10 Composite Vertical Stabilizer Ground Test Program.

Abstract

A review of the structural configuration and ground test program is presented. Particular emphasis is placed on the testing of a full-scale stub box test subcomponent and a full span ground test unit. The stub box subcomponent was tested in an environmental chamber under ambient, cold/wet, and hot/wet conditions. The test program included design limit static loads, fatigue spectrum loading to approximately two service lifetimes (with and without damage), design limit damage tolerance tests, and a final residual strength test to a structural failure. The first full-scale ground test unit was tested under ambient condition. The test unit was to have undergone static, fatigue, and damage tolerance tests but a premature structural failure occurred at design limit load during the third limit load test. A failure theory was developed which explains the similarity in types of failure and the large load discrepancy at failure between the two test articles. The theory attributes both failures to high stress concentrations at the edge of the lower rear spar access opening. A second full-scale ground test unit has been modified to incorporate the various changes resulting from the premature failure. The article has been assembled and is active in the test program. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1983
Accession Number
ADA302448

Entities

People

  • C. O. Stephens
  • J. M. Palmer Jr.
  • J. O. Sutton

Organizations

  • McDonnell Douglas

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Composite Materials
  • Composite Structures
  • Damage Tolerance
  • Fabrication
  • Fail Safe
  • Fasteners
  • Graphitic Materials
  • Laminates
  • Manufacturing
  • Materials
  • Materials Processing
  • Mechanics
  • Production
  • Syntactic Foams
  • Test Fixtures
  • Trailing Edges

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Structural Health Monitoring of Composite Structures.