EFFECT OF HEAT TREATMENT ON THE METALLURGICAL AND MECHANICAL PROPERTIES OF 7Al-3Mo TITANIUM ALLOY. Period covered : September 18, 1957 to January 13, 1959. Project title: METALLIC MATERIALS. Task title: HIGH STRENGTH METALLIC MATERIALS

Technical Report · Fri May 01 00:00:00 EDT 1959

OSTI ID:4180820

Hendricks, P L

Metallurgical and mechanical properties of 7% Al-3% Mo Ti alloy were determined on a production size heat. The investigation included heat treatment, the determination of tensile properties, stress rupture, creep stability, compressive yield, modulus, and impact strength. The testing conditions varied from room temperature up to 1900 deg F. (auth)

• Research Organization: Wright Air Development Center. Materials Lab., Wright-Patterson AFB, Ohio
• DOE Contract Number: AF33-(600)-35886
• NSA Number: NSA-14-006684
• OSTI ID: 4180820
• Report Number(s): WADC-TR-59-263
• Resource Relation: Other Information: Orig. Receipt Date: 31-DEC-60
• Country of Publication: United States
• Language: English

Related Subjects

METALS
CERAMICS AND MATERIALS
ALUMINUM ALLOYS
CREEP
ELASTICITY
FAILURES
HEAT TREATMENTS
HIGH TEMPERATURE
IMPACT SHOCK
MATERIALS TESTING
MECHANICAL PROPERTIES
METALLURGY
MOLYBDENUM ALLOYS
PRESSURE
PRODUCTION
QUANTITATIVE ANALYSIS
STABILITY
STRESSES
TEMPERATURE
TENSILE PROPERTIES
TITANIUM ALLOYS