AbstractFatigue crack growth testing of Inconel 718 has been carried out at the temperatures 550°C and 650°C. The tests were conducted using a mix of hold times and pure cyclic loading, referred to as block tests. From the test results, the existence of an embrittled volume or damaged zone in the vicinity of the crack tip has been revealed. It has been found that the evolution of this damaged zone can be sufficiently well described using a power law function with an exponent n=0.25
Thermo-mechanical fatigue crack propagation in Inconel 718 has been studied with different methods. ...
Abstract— In this paper observations concerning the effects of mechanical variables on the crack gro...
The crack growth behaviour of materials for application in turbines at temperatures of 500- 750 C ha...
High temperature fatigue crack growth in Inconel 718 has been studied at the temperatures 450 \ub0C,...
AbstractIn this work, fatigue crack growth measurements have been made on center-cracked tension spe...
In this work, fatigue crack growth measurements have been made on center-cracked tension specimens o...
Inconel 718 is a frequently used material for gas turbine applications at temperatures up to 650 °C....
In-phase TMF crack growth testing with different lengths of the hold time at the maximum temperature...
The present investigation aims to clarify the mechanisms behind hold-time fatigue crack growth in Al...
AbstractThe present investigation aims to clarify the mechanisms behind hold-time fatigue crack grow...
Gas turbine operating cycles at high temperatures often consist of load reversals mixed with hold ti...
The following contribution deals with the growth of cracks in low-cycle fatigue (LCF) and thermomech...
In this thesis an investigation and modelling of the fatigue crack propagation in the nickel based s...
The techniques of linear-elastic fracture mechanics were used to characterize the effect of several ...
The effect of isothermal exposure on elevated-temperature time-dependent fatigue crack propagation (...
Thermo-mechanical fatigue crack propagation in Inconel 718 has been studied with different methods. ...
Abstract— In this paper observations concerning the effects of mechanical variables on the crack gro...
The crack growth behaviour of materials for application in turbines at temperatures of 500- 750 C ha...
High temperature fatigue crack growth in Inconel 718 has been studied at the temperatures 450 \ub0C,...
AbstractIn this work, fatigue crack growth measurements have been made on center-cracked tension spe...
In this work, fatigue crack growth measurements have been made on center-cracked tension specimens o...
Inconel 718 is a frequently used material for gas turbine applications at temperatures up to 650 °C....
In-phase TMF crack growth testing with different lengths of the hold time at the maximum temperature...
The present investigation aims to clarify the mechanisms behind hold-time fatigue crack growth in Al...
AbstractThe present investigation aims to clarify the mechanisms behind hold-time fatigue crack grow...
Gas turbine operating cycles at high temperatures often consist of load reversals mixed with hold ti...
The following contribution deals with the growth of cracks in low-cycle fatigue (LCF) and thermomech...
In this thesis an investigation and modelling of the fatigue crack propagation in the nickel based s...
The techniques of linear-elastic fracture mechanics were used to characterize the effect of several ...
The effect of isothermal exposure on elevated-temperature time-dependent fatigue crack propagation (...
Thermo-mechanical fatigue crack propagation in Inconel 718 has been studied with different methods. ...
Abstract— In this paper observations concerning the effects of mechanical variables on the crack gro...
The crack growth behaviour of materials for application in turbines at temperatures of 500- 750 C ha...