Design Allowables for Titanium Alloys

Item

Title
Design Allowables for Titanium Alloys
Date
1969
Index Abstract
Not Available
Photo Quality
Complete
Report Number
AFML TR 69-161
Corporate Author
North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory
Air Force Materials Laboratory
Extent
388
Identifier
AD0857807
Access Rights
Export Controls
Distribution Classification
1
Contract
AF 33(615)-3979
DoD Project
7381
DoD Task
738106
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
AFSC USAF LTR
Distribution Conflict
No
Abstract
The purpose of this program was to develop design information on four titanium alloys for inclusion into Military Handbook-5. The alloys investigated were Ti-6Al-4V Condition STA, Ti-4Al-3Mo-1V Annealed Condition, Ti-13V-11Cr-3Al Annealed Condition, and Ti-6Al-6V-2Sn Annealed Condition and Condition STA. The mechanical properties investigated were tensile, compression, shear, bearing, fracture toughness and fatigue. The general results obtained are presented in Section VII of this report and the data generated for Military Handbook-5 are presented in Section VIII.
Report Availability
Full text available
Date Issued
1969-06
Provenance
Lockheed Martin Missiles & Fire Control
Creator
Martin, Gardner R.
Sommer, Alfred W.
Type
report
Format
1 online resource