DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0904766
Title:
Titanium 3Al-2.5V CW Hydraulic Tubing Development
Corporate Author:
BOEING COMMERCIAL AIRPLANE CO SEATTLE WA
Report Date:
1972-10-01
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.
Descriptive Note:
Final rept. on Task 2
Supplementary Note:
Report on SST Technology Follow-On Program-Phase 1.
Pages:
0153
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
DOT-FA-SS-71-12
File Size:
4.74MB
