This paper presents analysis of stress intensity factors at blade mounting locations of steam turbine rotor system. General expressions for the stresses induced in a rotating disc are derived and these equations are applied to steam turbine rotor disc. It is observed that the radial stress increases instantly at blade mounting location which indicates the probability of crack initiation and growth. A semi elliptical crack is considered at that location and weight function approach is used to determine the stress intensity factors. The results are validated with the influence coefficient approach. The differences of present approach with influence coefficient approach are less than 3 %. Hence the present approach is suitable for determinatio...
LecturePg. 31-44The disks and shafts of large steam turbines are subject to cracking from a variety ...
The steam turbine blade had failed by fatigue. The fatigue crack had initiated at the blade root T-...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...
This paper presents analysis of stress intensity factors at blade mounting locations of steam turbin...
This paper presents weight function approach with piece wise polynomial interpolation function to de...
One of the most common incipient losses of integrity in mechanical structures is the development and...
One of the most common incipient losses of integrity in mechanical structures is the development and...
An attention in this paper is focused on the stress analysis and the determination of fracture mecha...
This study based on a new fracture mechanics parameter is concerned with assessing the integrity of ...
This paper presents evaluation fracture mechanics parameters in low pressure turbine components. Cri...
Heavy loaded rotating additives of numerous machines (which include steam and fuel turbine, pumps, g...
Rotational components of aero engine turbine are the most important components. It operates at high ...
The fast-moving rotary components of various machines (such as steam turbines, gas, pumps, generator...
This paper presents results of the stress intensity factor calculations for the compressor blade inc...
This paper presents the results of the crack propagation analysis of an aircraft engine turbine disc...
LecturePg. 31-44The disks and shafts of large steam turbines are subject to cracking from a variety ...
The steam turbine blade had failed by fatigue. The fatigue crack had initiated at the blade root T-...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...
This paper presents analysis of stress intensity factors at blade mounting locations of steam turbin...
This paper presents weight function approach with piece wise polynomial interpolation function to de...
One of the most common incipient losses of integrity in mechanical structures is the development and...
One of the most common incipient losses of integrity in mechanical structures is the development and...
An attention in this paper is focused on the stress analysis and the determination of fracture mecha...
This study based on a new fracture mechanics parameter is concerned with assessing the integrity of ...
This paper presents evaluation fracture mechanics parameters in low pressure turbine components. Cri...
Heavy loaded rotating additives of numerous machines (which include steam and fuel turbine, pumps, g...
Rotational components of aero engine turbine are the most important components. It operates at high ...
The fast-moving rotary components of various machines (such as steam turbines, gas, pumps, generator...
This paper presents results of the stress intensity factor calculations for the compressor blade inc...
This paper presents the results of the crack propagation analysis of an aircraft engine turbine disc...
LecturePg. 31-44The disks and shafts of large steam turbines are subject to cracking from a variety ...
The steam turbine blade had failed by fatigue. The fatigue crack had initiated at the blade root T-...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...