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.