Characterizing the low cycle fatigue (LCF) properties of each alloy used in a gas turbine is expensive and time consuming. As such, each material is typically characterized over only the necessary cyclic range to insure safe, reliable component design. If it is desired to understand properties outside of that range, the accepted procedure is to acquire additional LCF test data. The objective of this project is to test the validity of several extrapolation methods versus acquiring additional test data for a particular alloy. Several models are developed by the following techniques: a monotonic test data anchor point, a strain-compatibility derived anchor point, and temperature independence of the Coffin-Manson relation. Predictions are made ...
In this contribution the mechanical behaviour of the Ni-based superalloy Haynes 282, developed for h...
Abstract: This work was focused on the material parameter extraction for the isothermal cyclic defor...
<p>Critical jet engine components are exposed to high temperatures. These components are also requir...
Characterizing the low cycle fatigue (LCF) properties of each alloy used in a gas turbine is expensi...
This thesis describes innovative methods used to predict high-stress amplitude, low cycle fatigue (L...
A combination of extrapolation and estimation techniques from both prior and current studies has bee...
A combination of extrapolation and estimation techniques from both prior and current studies has bee...
In the aviation industry today there is a trend of increasing operating temperatures in turbine engi...
To calculate the durability of gas turbine engine parts damaged by low-cycle fatigue (LCF), accordin...
In gas turbine engines for aerospace propulsion, the assessment of the fatigue damage mechanisms due...
This Excel file contains a compilation of low cycle fatigue (LCF) and thermomechanical fatigue (TMF)...
The article describes a new approach to the processing of experimental data coming from low-cycle fa...
Gas turbine components, such as blades and vanes, are routinely subjected to non-isothermal fatigue ...
\ua9 2016 Elsevier Ltd. In this paper, the high temperature cyclic and relaxation behaviour of Ni-ba...
A method of low-cycle fatigue equivalent tests based on the application of test specimens whose stre...
In this contribution the mechanical behaviour of the Ni-based superalloy Haynes 282, developed for h...
Abstract: This work was focused on the material parameter extraction for the isothermal cyclic defor...
<p>Critical jet engine components are exposed to high temperatures. These components are also requir...
Characterizing the low cycle fatigue (LCF) properties of each alloy used in a gas turbine is expensi...
This thesis describes innovative methods used to predict high-stress amplitude, low cycle fatigue (L...
A combination of extrapolation and estimation techniques from both prior and current studies has bee...
A combination of extrapolation and estimation techniques from both prior and current studies has bee...
In the aviation industry today there is a trend of increasing operating temperatures in turbine engi...
To calculate the durability of gas turbine engine parts damaged by low-cycle fatigue (LCF), accordin...
In gas turbine engines for aerospace propulsion, the assessment of the fatigue damage mechanisms due...
This Excel file contains a compilation of low cycle fatigue (LCF) and thermomechanical fatigue (TMF)...
The article describes a new approach to the processing of experimental data coming from low-cycle fa...
Gas turbine components, such as blades and vanes, are routinely subjected to non-isothermal fatigue ...
\ua9 2016 Elsevier Ltd. In this paper, the high temperature cyclic and relaxation behaviour of Ni-ba...
A method of low-cycle fatigue equivalent tests based on the application of test specimens whose stre...
In this contribution the mechanical behaviour of the Ni-based superalloy Haynes 282, developed for h...
Abstract: This work was focused on the material parameter extraction for the isothermal cyclic defor...
<p>Critical jet engine components are exposed to high temperatures. These components are also requir...