Add to ORKGThis paper deals with low cycle life estimation of a turbine blisk. The turbine blisk operates at extreme conditions; hence it is subjected to aerodynamic loads and high centrifugal loads. The loads on the turbine blisk vary due to the mission profile of the vehicle that includes takeoff, cruise and landing. An elasticplastic finite element analysis is carried out. The life at the obtained stress and strain values is estimated using nCode DesignLife tool. Strain life approach is followed to estimate the life and Smith Watson Topper's approach is followed to carry out the mean stress correction
GKN Aerospace in Trollhättan don’t use the latest ANSYS version and need to upgrade their life analy...
This article deals with the description of an approximate numerical estimation approach of a low cyc...
The paper analyses the possibility of using analytical methods of notch stress-strain correction in ...
This paper deals with low cycle life estimation of a turbine blisk. The turbine blisk operates at ex...
The present paper deals with fatigue analysis of a turbine blisk (integrated blade and dis...
AbstractThis work is primarily focused in utilising a technique to assess low cycle fatigue life of ...
AbstractA more accurate life prediction for gas turbine blade takes into account the material behavi...
The present paper deals with the low cycle fatigue analysis of the low pressure (LP) steam turbine b...
This paper represents the fatigue life Prediction of aircraft turbine disk. Low-cycle fatigue of rem...
This dissertation presents an approach to use blade tip timing measurements with finite element anal...
A consideration is given to the problem of determining remaining operational life of steam turbine r...
The present paper deals with the low cycle fatigue analysis of the low pressure (LP) steam turbine b...
In this thesis a test rig for blade life assessment has been designed. The test article is a blade f...
In view of the problem that the gas turbine blades rely more on the long-term test of the whole mach...
To assess of the lifetime extension (LTE) of wind turbines, the remaining fatigue budget of differen...
GKN Aerospace in Trollhättan don’t use the latest ANSYS version and need to upgrade their life analy...
This article deals with the description of an approximate numerical estimation approach of a low cyc...
The paper analyses the possibility of using analytical methods of notch stress-strain correction in ...
This paper deals with low cycle life estimation of a turbine blisk. The turbine blisk operates at ex...
The present paper deals with fatigue analysis of a turbine blisk (integrated blade and dis...
AbstractThis work is primarily focused in utilising a technique to assess low cycle fatigue life of ...
AbstractA more accurate life prediction for gas turbine blade takes into account the material behavi...
The present paper deals with the low cycle fatigue analysis of the low pressure (LP) steam turbine b...
This paper represents the fatigue life Prediction of aircraft turbine disk. Low-cycle fatigue of rem...
This dissertation presents an approach to use blade tip timing measurements with finite element anal...
A consideration is given to the problem of determining remaining operational life of steam turbine r...
The present paper deals with the low cycle fatigue analysis of the low pressure (LP) steam turbine b...
In this thesis a test rig for blade life assessment has been designed. The test article is a blade f...
In view of the problem that the gas turbine blades rely more on the long-term test of the whole mach...
To assess of the lifetime extension (LTE) of wind turbines, the remaining fatigue budget of differen...
GKN Aerospace in Trollhättan don’t use the latest ANSYS version and need to upgrade their life analy...
This article deals with the description of an approximate numerical estimation approach of a low cyc...
The paper analyses the possibility of using analytical methods of notch stress-strain correction in ...