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Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 3. Tables of Data Collected

Report Number: ASD TDR 62-335 Volume 3
Author: None Given
Corporate Author: Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-01
Pages: 332
Contract: AF 33(616)-6346
Project: 7381
Task: 738103
AD Number: ADD850331

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 alloys in sheet form.

Four alloys were investigated: B120VCA(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 and 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 -320F to 80F and physical properties from -420F to 1200 F were obtained.

Volume 1 summarizes mechanical and physical properties in a form consistent with those given in MIL-HDBK-5. Experimental procedures and test results for static mechanical properties and physical properties are reported in Volume 2a. Volume 2b contains procedures and results for creep and fatigue tests and Volume 3 is a tabular compilation of all data obtained in the program.

Lockheed Martin Missiles & Fire Control
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