Mechanical Properties Of Two Titanium Forging Alloys, Ti 155A and C135AMo
Report Number: WADD TR 61-43
Author(s): Henning, R. G.
Corporate Author(s): Metals and Ceramics Laboratory
Laboratory: Metals and Ceramics Laboratory
Date of Publication: 1961-04
Pages: 208
Contract: Laboratory Research - No Contract
DoD Project: 7351 - Metallic Materials
DoD Task: 73521
Identifier: AD0271526
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.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Henning, R. G.
Corporate Author(s): Metals and Ceramics Laboratory
Laboratory: Metals and Ceramics Laboratory
Date of Publication: 1961-04
Pages: 208
Contract: Laboratory Research - No Contract
DoD Project: 7351 - Metallic Materials
DoD Task: 73521
Identifier: AD0271526
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.
Provenance: Lockheed Martin Missiles & Fire Control