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Design Allowables for Titanium Alloys

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