Thermomechanical fatigue (TMF) experiments were conducted on polycrystalline MAR-M 200 over a cyclic temperature range of 500 to 1000 C. Inelastic strain ranges of 0.03 to 0.2 percent were imposed on the specimens. The TMF lives were found to be significantly shorter than isothermal low-cycle-fatigue (LCF) life at the maximum cycle temperature, and in-phase cycling was more damaging than out-of-phase cycling. Extensive crack tip oxidation appeared to play a role in promoting the severity of in-phase cycling. Carbide particle - matrix interface cracking was also observed after in-phase TMF cycling. The applicability of various life prediction models to the TMF results obtained was assessed. It was concluded that current life prediction model...
AbstractThermo-mechanical fatigue (TMF) is a critical damage process in gas turbine jet engines. Rel...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
A review is presented of thermal and thermomechanical fatigue (TMF) crack initiation life prediction...
AbstractThroughout the world, extensive low-cycle fatigue (LCF) data, which is traditionally used fo...
The combination of cyclic mechanical and cyclic thermal loading leads to thermomechanical fatigue (T...
The combination of cyclic mechanical and cyclic thermal loading leads to thermomechanical fatigue (T...
As gas turbine technology continues to advance, the need for advanced life prediction methods for ho...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
A major objective of the fatigue and fracture efforts under the NASA Hot Section Technology (HOST) p...
A major objective of the fatigue and fracture efforts under the Hot Section Technology (HOST) progra...
This program is designed to investigate fundamental damage processes, identify modeling strategies, ...
AbstractThroughout the world, extensive low-cycle fatigue (LCF) data, which is traditionally used fo...
Announced survey directs attention toward low cycle fatigue and thermal fatigue experienced at eleva...
Structural materials used in engineering applications routinely subjected to repetitive mechanical l...
AbstractThermo-mechanical fatigue (TMF) is a critical damage process in gas turbine jet engines. Rel...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
A review is presented of thermal and thermomechanical fatigue (TMF) crack initiation life prediction...
AbstractThroughout the world, extensive low-cycle fatigue (LCF) data, which is traditionally used fo...
The combination of cyclic mechanical and cyclic thermal loading leads to thermomechanical fatigue (T...
The combination of cyclic mechanical and cyclic thermal loading leads to thermomechanical fatigue (T...
As gas turbine technology continues to advance, the need for advanced life prediction methods for ho...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
A major objective of the fatigue and fracture efforts under the NASA Hot Section Technology (HOST) p...
A major objective of the fatigue and fracture efforts under the Hot Section Technology (HOST) progra...
This program is designed to investigate fundamental damage processes, identify modeling strategies, ...
AbstractThroughout the world, extensive low-cycle fatigue (LCF) data, which is traditionally used fo...
Announced survey directs attention toward low cycle fatigue and thermal fatigue experienced at eleva...
Structural materials used in engineering applications routinely subjected to repetitive mechanical l...
AbstractThermo-mechanical fatigue (TMF) is a critical damage process in gas turbine jet engines. Rel...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...
Non-isothermal conditions during flight cycles have long led to the requirement for thermo-mechanica...