In previous work by the authors, a quantitative model based on a two‐stage oxidation mechanism was developed to describe the oxidation‐assisted crack growth behavior in alloy 718. This model is used here to predict the crack growth rate in this alloy at 650°C for two different loading conditions: one is a continuous cycle with a hold time duration of 300 s imposed at minimum load, the other is a continuous cycle without a hold time duration. The results obtained from applying the model to these loading profiles were then compared with those obtained experimentally. Good agreement was observed between the two data sets. Details of the model calculations are discussed, and suggestions to further extend the model capabilities are made in this ...
Prediction of oxidation-assisted crack growth has been carried out for a nickel-based superalloy at ...
Observations concerning the effects of the environment and material variables on the crack growth pr...
Inconel 718 is a frequently used material for gas turbine applications at temperatures up to 650 °C....
At frequencies below that of the transitional frequency, the elevated temperature fatigue crack grow...
This paper presents a new model to predict the high temperature, intergranular crack growth rate beh...
The elevated-temperture fatigue crack growth behavior in alloy 718, when subjected to a loading freq...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
The present investigation aims to clarify the mechanisms behind hold-time fatigue crack growth in Al...
Abstract: This paper deals with the prediction of fatigue crack growth at high temperatures in the N...
AbstractThe present investigation aims to clarify the mechanisms behind hold-time fatigue crack grow...
International audienceThe understanding o f hold time effects on the fatigue crack growth rate (FCGR...
This paper describes the use of a crack growth rate superposition model. In this model, the total cr...
International audienceUnderstanding and modeling hold time effects on fatigue crack growth rate (FCG...
In this paper observations concerning effects of mechanical, environmental, material variables on th...
The objective of the present study is to review the different phenomena responsible for crack growth...
Prediction of oxidation-assisted crack growth has been carried out for a nickel-based superalloy at ...
Observations concerning the effects of the environment and material variables on the crack growth pr...
Inconel 718 is a frequently used material for gas turbine applications at temperatures up to 650 °C....
At frequencies below that of the transitional frequency, the elevated temperature fatigue crack grow...
This paper presents a new model to predict the high temperature, intergranular crack growth rate beh...
The elevated-temperture fatigue crack growth behavior in alloy 718, when subjected to a loading freq...
This paper is concerned with the intergranular crack tip oxidation mechanism in alloy 718 at elevate...
The present investigation aims to clarify the mechanisms behind hold-time fatigue crack growth in Al...
Abstract: This paper deals with the prediction of fatigue crack growth at high temperatures in the N...
AbstractThe present investigation aims to clarify the mechanisms behind hold-time fatigue crack grow...
International audienceThe understanding o f hold time effects on the fatigue crack growth rate (FCGR...
This paper describes the use of a crack growth rate superposition model. In this model, the total cr...
International audienceUnderstanding and modeling hold time effects on fatigue crack growth rate (FCG...
In this paper observations concerning effects of mechanical, environmental, material variables on th...
The objective of the present study is to review the different phenomena responsible for crack growth...
Prediction of oxidation-assisted crack growth has been carried out for a nickel-based superalloy at ...
Observations concerning the effects of the environment and material variables on the crack growth pr...
Inconel 718 is a frequently used material for gas turbine applications at temperatures up to 650 °C....