Abstract- The aim of this paper is to examine the stress and displacement for pico turbine blades. The engineer’s work is to design blades that can operate safely in harsh environments and be able to avoid failure and deformation of blades. This requires in-depth finite element modeling and structural analysis. Due to shape of the blade it is not possible to calculate the stresses of rotor blade using analytical method. Hence ANSYS, a solid modeling & a finite element package is used to calculate the stresses for rotor blades. The results were analyzed for runner and found location of several critical sections subjected to high stress concentration at hub section. Analysis shows that the maximum stress is produced at hub and blade joint...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...
This paper presents the failure analysis of the turbine blade of a gas turbine engine 9E GE type, in...
AbstractThe gas turbine is the heart of all modern aircraft. The power derived from the gas turbine ...
Abstract: One of the major sources of stress arising in turbomachinery blades are the centrifugal lo...
With the development of wind power generation technology, the wind turbine blade is becoming more an...
One of the major sources of stress arising in turbo machinery blades are centrifugal loads acting at...
The problem of turbine engines blades stress-strain state has been studied. All calculations have be...
The intent of this thesis is to study stresses in high speed turbo machine. A turbo machine used for...
Abstract—This paper borders around analysis of turbine blade. The blade is a rotating part which con...
In this work, the analysis is done on a blade of length 66.5cm which is designed for AIR X- 400W hor...
In this paper, the failure analysis of the air engine's turbine disk has been established in a certa...
Gas turbine works under high stress and high temperature. The stress is distributed over the whole t...
New installations of unregulated power to the electrical grid have led to more fluctuations in the g...
Abstract- Modal analysis has been important to the designers and operators since the inception of th...
The present research work describes the development of Turgo turbine blades on the Solidworks softwa...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...
This paper presents the failure analysis of the turbine blade of a gas turbine engine 9E GE type, in...
AbstractThe gas turbine is the heart of all modern aircraft. The power derived from the gas turbine ...
Abstract: One of the major sources of stress arising in turbomachinery blades are the centrifugal lo...
With the development of wind power generation technology, the wind turbine blade is becoming more an...
One of the major sources of stress arising in turbo machinery blades are centrifugal loads acting at...
The problem of turbine engines blades stress-strain state has been studied. All calculations have be...
The intent of this thesis is to study stresses in high speed turbo machine. A turbo machine used for...
Abstract—This paper borders around analysis of turbine blade. The blade is a rotating part which con...
In this work, the analysis is done on a blade of length 66.5cm which is designed for AIR X- 400W hor...
In this paper, the failure analysis of the air engine's turbine disk has been established in a certa...
Gas turbine works under high stress and high temperature. The stress is distributed over the whole t...
New installations of unregulated power to the electrical grid have led to more fluctuations in the g...
Abstract- Modal analysis has been important to the designers and operators since the inception of th...
The present research work describes the development of Turgo turbine blades on the Solidworks softwa...
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. ...
This paper presents the failure analysis of the turbine blade of a gas turbine engine 9E GE type, in...
AbstractThe gas turbine is the heart of all modern aircraft. The power derived from the gas turbine ...