The high temperature deformation and fracture behavior of T-111 and ASTAR-811C were studied over the temperature range 982 to 2205 C (1800 to 4000 F). As-cast and wrought-recrystallized material as well as GTA welds in sheet and plate were evaluated using conventional tensile and creep tests. Post test examinations were performed using optical metallography, scanning electron microscopy and transmission electron microscopy. A high temperature region of reduced ductility, in terms of tensile elongation, was identified for both alloys. The reduction in tensile elongation became more severe with increase in grain size, being near catastrophic for the as-cast specimens. Optical and electron metallography indicated that even for failures at very...
The Department of Homeland Security (DHS) funded National Transportation Security Center of Excellen...
Grain size and annealing temperature effects on creep properties of dispersion strengthened tantalum...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The notched-tensile, tensile, and bend properties of GTA welds in T-111 and ASTAR-811C sheet were de...
The metallurgical factors influencing the ductility of T-111 (Ta-8W-2Hf) alloy following long-time e...
Metallurgical condition was shown to have a significant effect on the creep properties of ASTAR-811C...
Low cycle fatigue tests have been performed on the tantalum base alloys T-111 and ASTAR 811C with sy...
Mechanical properties determined for precipitation hardened tantalum base alloy /ASTAR-811C/ for pot...
Elevated temperature tensile and stress rupture properties were evaluated for forged TDNiCr (Ni-20Cr...
Four separate studies of various aspects of the vacuum creep behavior of two tantalum alloys (T-111 ...
Ultrahigh vacuum creep tests were conducted on tantalum, tungsten, and molybdenum alloys to develop ...
Creep tests were conducted on two tantalum alloys (ASTAR 811C and T-111 alloy), on a molybdenum allo...
Two tantalum base alloys, Ta-12W-1.0Re-0.7Hf-0.025C(ASTAR-1211C) and Ta-15W-1.0Re-0.7Hf-0.025C(ASTAR...
Determination of weldability and elevated temperature stability of refractory metal alloy
The Department of Homeland Security (DHS) funded National Transportation Security Center of Excellen...
The Department of Homeland Security (DHS) funded National Transportation Security Center of Excellen...
Grain size and annealing temperature effects on creep properties of dispersion strengthened tantalum...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The notched-tensile, tensile, and bend properties of GTA welds in T-111 and ASTAR-811C sheet were de...
The metallurgical factors influencing the ductility of T-111 (Ta-8W-2Hf) alloy following long-time e...
Metallurgical condition was shown to have a significant effect on the creep properties of ASTAR-811C...
Low cycle fatigue tests have been performed on the tantalum base alloys T-111 and ASTAR 811C with sy...
Mechanical properties determined for precipitation hardened tantalum base alloy /ASTAR-811C/ for pot...
Elevated temperature tensile and stress rupture properties were evaluated for forged TDNiCr (Ni-20Cr...
Four separate studies of various aspects of the vacuum creep behavior of two tantalum alloys (T-111 ...
Ultrahigh vacuum creep tests were conducted on tantalum, tungsten, and molybdenum alloys to develop ...
Creep tests were conducted on two tantalum alloys (ASTAR 811C and T-111 alloy), on a molybdenum allo...
Two tantalum base alloys, Ta-12W-1.0Re-0.7Hf-0.025C(ASTAR-1211C) and Ta-15W-1.0Re-0.7Hf-0.025C(ASTAR...
Determination of weldability and elevated temperature stability of refractory metal alloy
The Department of Homeland Security (DHS) funded National Transportation Security Center of Excellen...
The Department of Homeland Security (DHS) funded National Transportation Security Center of Excellen...
Grain size and annealing temperature effects on creep properties of dispersion strengthened tantalum...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...