Static fracture tests were performed on surface flawed specimens of aluminum and titanium alloys. A simulated proof overload cycle was applied prior to all of the cyclic tests. Variables included in each test series were flaw shapes and thickness. Additionally, test temperature was a variable for the aluminum test series. The crack opening displacement and stress-strain data obtained are presented
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature
Static tensile tests were performed on simple notched specimens containing fatigue cracks. Four type...
Stress corrosion cracking of high strength aluminum alloys investigated by electrochemical, mechanic...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
This experimental program was undertaken to investigate the crack growth behavior of deep surface fl...
Cryogenic testing of aluminum alloy specimens for fracture toughness and stress wave dat
Room-temperature static and cyclic tests were made on 21 aluminum plates in the shape of a 91.4x91.4...
The crack-closure and crack-growth characteristics of the titanium alloy Ti-6Al-4V were determined e...
Mechanism of stress corrosion cracking in aluminum alloys and techniques for detection of surface de...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The stable tearing behavior of thin sheets of 2024-T3 aluminum alloy was investigated for middle cra...
The variables studied in the stress-corrosion cracking performance of high strength aluminum alloys ...
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature
Static tensile tests were performed on simple notched specimens containing fatigue cracks. Four type...
Stress corrosion cracking of high strength aluminum alloys investigated by electrochemical, mechanic...
Conditions controlling the growth and fracture of deep surface flaws in aerospace alloys were invest...
This experimental program was undertaken to determine the effects of (1) combined tensile and bendin...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
This experimental program was undertaken to investigate the crack growth behavior of deep surface fl...
Cryogenic testing of aluminum alloy specimens for fracture toughness and stress wave dat
Room-temperature static and cyclic tests were made on 21 aluminum plates in the shape of a 91.4x91.4...
The crack-closure and crack-growth characteristics of the titanium alloy Ti-6Al-4V were determined e...
Mechanism of stress corrosion cracking in aluminum alloys and techniques for detection of surface de...
Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardeni...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The stable tearing behavior of thin sheets of 2024-T3 aluminum alloy was investigated for middle cra...
The variables studied in the stress-corrosion cracking performance of high strength aluminum alloys ...
Plane stress crack propagation of aluminum and titanium alloys at cryogenic temperature
Static tensile tests were performed on simple notched specimens containing fatigue cracks. Four type...
Stress corrosion cracking of high strength aluminum alloys investigated by electrochemical, mechanic...