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

Item

Title
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
Date
1962
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
ASD TDR 62-335 Volume 1
Corporate Author
Lockheed-Georgia Company
Laboratory
Directorate of Materials and Processes
Extent
180
Identifier
ADD850333
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-6346
DoD Project
7381
DoD Task
738103
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
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.
Report Availability
Full text available
Date Issued
1962-01
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Creator
Hughes, P. J.
Media
ASDTDR62-335volume01.pdf