Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 1. Summary of Mechanical and Physical Property Data Collected, Including Tensile Creep and Fatigue
Report Number: ASD TDR 62-335 Volume 1
Author(s): Hughes, P. J.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-01
Pages: 180
Contract: AF 33(616)-6346
DoD Project: 7381
DoD Task: 738103
Identifier: ADD850333
Abstract:
Mechanical and physical property data, necessary to fulfill the requirements of Phase II of the Department of Defense Titanium Alloy Sheet Rolling Program, were obtained for selected solution treated and aged titanium alloy in sheet form.Four alloys were investigated: BI20VCA (ti-13V-11Cr-3Al), Ti-6Al-4V, Ti-2.5Al-16V and Ti-4Al-3Mo-1V. They were supplied by the producers in the heat treated condition from three or more heats and three thicknesses of each alloy. Static mechanical property data for tension, compression, bearing shear and crippling; creep and rupture data for tension, compression, bearing and shear; and axial-load fatigue data were obtained at room and elevated temperatures. Fastener and weld joint data from -320 degrees F to 80 degrees F and physical properties from -420 degrees F to 1200 degrees F were obtained.Volum I summarizes mechanical and physical properties in a form consistent with those given in MIL-HDBK-5.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Hughes, P. J.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-01
Pages: 180
Contract: AF 33(616)-6346
DoD Project: 7381
DoD Task: 738103
Identifier: ADD850333
Abstract:
Mechanical and physical property data, necessary to fulfill the requirements of Phase II of the Department of Defense Titanium Alloy Sheet Rolling Program, were obtained for selected solution treated and aged titanium alloy in sheet form.Four alloys were investigated: BI20VCA (ti-13V-11Cr-3Al), Ti-6Al-4V, Ti-2.5Al-16V and Ti-4Al-3Mo-1V. They were supplied by the producers in the heat treated condition from three or more heats and three thicknesses of each alloy. Static mechanical property data for tension, compression, bearing shear and crippling; creep and rupture data for tension, compression, bearing and shear; and axial-load fatigue data were obtained at room and elevated temperatures. Fastener and weld joint data from -320 degrees F to 80 degrees F and physical properties from -420 degrees F to 1200 degrees F were obtained.Volum I summarizes mechanical and physical properties in a form consistent with those given in MIL-HDBK-5.
Provenance: Lockheed Martin Missiles & Fire Control