This dissertation deals with modeling of steam flow through the turbines stage with partial admission. Both methods, experimental and numerical, are described The mathematical model with different models of turbulence were developed, tested in CFD Fluent and compared with experimental result. the proper model of turbulence was chosen and described. Number of variants with different geometric and boundary conditions were computed. Special attention are given to detailed description of flow field in investigated area, with focus ob visualization of characteristic of variables, which could significantly influence the efficiency of turbine stage. In contrast to the experiment, numerical simulation gives us the possibility to monitor variables d...
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 steam flow past a last stage (the eleventh stage) of the high pressure part of the TK120 steam t...
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...
Topical problems of flow part of LP of steam turbines ere described. Developed numerical methods, ex...
Partial admission occurs in steam turbines operated under part load when one or more segments of the...
Diploma thesis named CFD simulation of the steam flow in the unregulated extraction of the steam tur...
This thesis deals with modelling of flow in rotating engines. The introduction of the thesis discuss...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
International audiencePartial admission is commonly used to control the power, especially of small s...
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...
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 steam flow past a last stage (the eleventh stage) of the high pressure part of the TK120 steam t...
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...
Topical problems of flow part of LP of steam turbines ere described. Developed numerical methods, ex...
Partial admission occurs in steam turbines operated under part load when one or more segments of the...
Diploma thesis named CFD simulation of the steam flow in the unregulated extraction of the steam tur...
This thesis deals with modelling of flow in rotating engines. The introduction of the thesis discuss...
The never ending process to increase the efficiency of turbine stages introduced an idea to create a...
International audiencePartial admission is commonly used to control the power, especially of small s...
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...
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...