Mechanical Properties Of Two Titanium Forging Alloys, Ti 155A and C135AMo

Item

Title
Mechanical Properties Of Two Titanium Forging Alloys, Ti 155A and C135AMo
Date
1961
Index Abstract
Contrails and DTIC
Photo Quality
Not Needed
Report Number
WADD TR 61-43
Corporate Author
Metals and Ceramics Laboratory
Laboratory
Metals and Ceramics Laboratory
Extent
208
Identifier
AD0271526
AD0271526
Access Rights
OTS
Distribution Classification
1
Contract
Laboratory Research - No Contract
DoD Project
7351 - Metallic Materials
DoD Task
73521
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
Mechanical properties of two annealed titanium forging alloys, Ti 155A and C135AMo, were obtained. These properties included tensile, compressive, pin shear, bearing, and notched tensile at room, 200, 400, 600, 800, and 1000°F temperatures. Stressed and nonstressed exposure tests were conducted at 600, 800, and 1000°F. Torsion tests were conducted at room temperature only.

Properties vs. temperature graphs and tensile, compressive, and bearing stress-strain curves were presented. The ratio of the various properties to room temperature tensile results were plotted vs. temperature.
Report Availability
Full text available
Date Issued
1961-04
Subject
Forging
Titanium Alloys
Alloys
Compressive Properties
Elastic Properties
Fracture (Mechanics)
High Temperature
Impact Shock
Cryogenics
Mechanical Properties
Shear Stresses
Stability
Tables (Data)
Tensile Properties
Thermal Stresses
Torsion Meters
Publisher
Wright-Patterson Air Force Base, OH : Aeronautical Systems Division, Air Force Systems Command, United States Air Force
Distribution Conflict
No
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Creator
Henning, R. G.