Design Allowables for Titanium Alloys
Report Number: AFML TR 69-161
Author(s): Martin, Gardner R., Sommer, Alfred W.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-06
Pages: 388
Contract: AF 33(615)-3979
DoD Project: 7381
DoD Task: 738106
Identifier: AD0857807
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.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Martin, Gardner R., Sommer, Alfred W.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-06
Pages: 388
Contract: AF 33(615)-3979
DoD Project: 7381
DoD Task: 738106
Identifier: AD0857807
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.
Provenance: Lockheed Martin Missiles & Fire Control