An extensive test program was undertaken to understand the roles of microstructure and environment on the elevated temperature, strain controlled, low cycle fatigue (HTLCF) behavior of two classes of recently developed high temperature alloy systems. The first of these classes consisted of three near-alpha titanium alloys, Ti-5524S (Ti-5Al-5Sn-2Zr-4Mo-0.25Si), Ti-685 (Ti-6Al-5Zr-0.5Mo-0.25Si) and Ti-6242S (Ti-6Al-2Sn-4Zr-2Mo-0.1Si). A wide variety of processing sequences were used to produce sixteen different microstructural conditions for both Ti-5524S and Ti-685. Two different microstructural conditions were examined for the Ti-6242S alloy. The different microstructural conditions for all of these alloys may be divided into two basic grou...
From service point of view effect of two important parameters, namely, temperature and frequency on...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...
An extensive test program was undertaken to understand the roles of microstructure and environment o...
One of the important criteria for selection titanium alloys for discs and blades of turbine engine c...
TIMETAL®407 (Ti-407) is a medium strength (~650MPa 0.2%YS) titanium alloy, recently developed by TIM...
Titanium alloys are increasingly used for structural applications in transportation engineering (aer...
Component failure due to cold dwell fatigue of titanium and its alloys is a long-standing problem wh...
Timetal 407 (Ti-407) is a novel titanium alloy formulated as a lower strength, more malleable alloy ...
Tensile properties of titanium alloys are known to be strongly dependent on their microstructures an...
The mechanisms of low-cycle, fatigue crack nucleation and early growth were investigated at room tem...
Titanium alloys are equipped with impressive high strength and low density, along with other notable...
This work seeks to integrate temperature dependence into a microstructure-sensitive fatigue model fo...
The high cycle and very high cycle fatigue properties of the titanium alloy Ti-6Al-4V with a duplex ...
TIMETAL®407 (Ti-407) is a novel titanium alloy formulated as a medium strength, highly ductile alloy...
From service point of view effect of two important parameters, namely, temperature and frequency on...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...
An extensive test program was undertaken to understand the roles of microstructure and environment o...
One of the important criteria for selection titanium alloys for discs and blades of turbine engine c...
TIMETAL®407 (Ti-407) is a medium strength (~650MPa 0.2%YS) titanium alloy, recently developed by TIM...
Titanium alloys are increasingly used for structural applications in transportation engineering (aer...
Component failure due to cold dwell fatigue of titanium and its alloys is a long-standing problem wh...
Timetal 407 (Ti-407) is a novel titanium alloy formulated as a lower strength, more malleable alloy ...
Tensile properties of titanium alloys are known to be strongly dependent on their microstructures an...
The mechanisms of low-cycle, fatigue crack nucleation and early growth were investigated at room tem...
Titanium alloys are equipped with impressive high strength and low density, along with other notable...
This work seeks to integrate temperature dependence into a microstructure-sensitive fatigue model fo...
The high cycle and very high cycle fatigue properties of the titanium alloy Ti-6Al-4V with a duplex ...
TIMETAL®407 (Ti-407) is a novel titanium alloy formulated as a medium strength, highly ductile alloy...
From service point of view effect of two important parameters, namely, temperature and frequency on...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...
A key design consideration for material selection in the aerospace industry is weight reduction; wit...