An investigation of one and half axial turbine stage configuration was carried out in a closed-loop wind tunnel. The investigation was addressed to that impact how the previous stage outlet flow field influences the flow structures in the next stator in steam multistage turbines. The stage - stator interaction has been studied in this work. The detailed measurement with a pneumatic probes and fast response pressure probes behind the rotor and the second stator were performed to gain the useful data to analyze the impact. The detailed flow field measurement was carried out in the nominal stage regime (given by the stage isentropic Mach number 0.3 and velocity ratio u/c 0.68). The clocking effect of the stators is discussed and detailed unste...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
An investigation of one and half axial turbine stage configuration was carried out in a closed-loop ...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
Abstract: The never ending process to increase the efficiency of turbine stages introduced an idea t...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
The unsteady nature of the flow in multi-stage turbomachines makes it possible for designers to impr...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
The contribution deals with analysis of unsteady pressure measurement in one and half axial turbine ...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
The contribution deals with analysis of unsteady pressure measurement in one and half axial turbine ...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
An investigation of one and half axial turbine stage configuration was carried out in a closed-loop ...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
Abstract: The never ending process to increase the efficiency of turbine stages introduced an idea t...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
The unsteady nature of the flow in multi-stage turbomachines makes it possible for designers to impr...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
The contribution deals with analysis of unsteady pressure measurement in one and half axial turbine ...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
The contribution deals with analysis of unsteady pressure measurement in one and half axial turbine ...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...
This work aims at investigating the impact of axial gap variation on aerodynamic performance of a hi...