Titanium 3Al-2.5V CW Hydraulic Tubing Development

Abstract

This report contains the fatigue, metallurgical, and bend test results on titanium alloy 3Al-2.5V cold worked and stress relieved tubing procured during the prototype supersonic transport test program, and the new texture-controlled tubing. The tubing procured for the prototype program was tested with three different inside-diameter finishes developed by Boeing, Grumman Aerospace, and McDonnell-Douglas. The texture-controlled tubing was developed during this program, and its requirements are defined in the new Boeing-proposed specification, which is included in this report.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1972
Accession Number
AD0904766

Entities

People

  • G. W. Harruff
  • J. Vandervelden
  • W. Quist
  • W. Spurr
  • William G. Nelson

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Cyber

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Commercial Aircraft
  • Failure Mode And Effect Analysis
  • Finishes
  • Jet Transport Aircraft
  • Manufacturing
  • Materials
  • Measurement
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Surface Properties
  • Surface Roughness
  • Tensile Strength
  • Test And Evaluation
  • Three Dimensional

Readers

  • Aerospace Engineering
  • Metallurgy

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster