When a metallic material is exposed to a high temperature in an ambient atmosphere, oxidation takes place on the metallic surface. The formed oxides (both surface and grain boundary oxides) are mechanically brittle so that if the stress is high enough the oxides will be cracked. The grain boundary oxide formation in TAZ-8A nickel-base superalloy was studied. The effect of oxide crack nucleus on low cycle fatigue life will be analyzed. The TAZ-8A was subjected to high temperature oxidation tests in air under the stress-free condition. The oxidation temperatures were 600, 800, and 1000 C. The oxidation time varies from 10 to 1000 hours
Fatigue crack initiation and propagation behaviour in subsolvus heat treated turbine disc alloy N18 ...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
The effects of preoxidation on subsequent fatigue life were studied. Surface oxidation and grain bou...
Fatigue life consists of fatigue crack nucleation and propagation periods. In order to predict fatig...
Fatigue lives at elevated temperatures are often shortened by creep and/or oxidation. Creep causes g...
Gas turbine materials are designed to work in extreme environments in high temperature with an oxidi...
As temperatures within the aero engine increase, oxidation will begin to have a greater effect on th...
The shortage of fossil fuels and the emergence of renewable energy technologies have increased the d...
Fatigue tests have been conducted on an advanced disc Ni-based superalloy [low solvus, high refracto...
A number of thermal exposures were undertaken to determine the effect oxidation has on the fatigue l...
The oxidation behaviour of RR1000 with different surface modifications has been well studied using d...
Fatigue crack growth rate at elevated temperatures can be accelerated by grain boundary oxidation. G...
Nickel-base superalloys are the most complex and the most widely used for high temperature applicati...
High-temperature intergranular crack tip oxidation under a single 600 s long sustained tensile load ...
Fatigue crack initiation and propagation behaviour in subsolvus heat treated turbine disc alloy N18 ...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
The effects of preoxidation on subsequent fatigue life were studied. Surface oxidation and grain bou...
Fatigue life consists of fatigue crack nucleation and propagation periods. In order to predict fatig...
Fatigue lives at elevated temperatures are often shortened by creep and/or oxidation. Creep causes g...
Gas turbine materials are designed to work in extreme environments in high temperature with an oxidi...
As temperatures within the aero engine increase, oxidation will begin to have a greater effect on th...
The shortage of fossil fuels and the emergence of renewable energy technologies have increased the d...
Fatigue tests have been conducted on an advanced disc Ni-based superalloy [low solvus, high refracto...
A number of thermal exposures were undertaken to determine the effect oxidation has on the fatigue l...
The oxidation behaviour of RR1000 with different surface modifications has been well studied using d...
Fatigue crack growth rate at elevated temperatures can be accelerated by grain boundary oxidation. G...
Nickel-base superalloys are the most complex and the most widely used for high temperature applicati...
High-temperature intergranular crack tip oxidation under a single 600 s long sustained tensile load ...
Fatigue crack initiation and propagation behaviour in subsolvus heat treated turbine disc alloy N18 ...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...