Based on the critical velocity model, impact and capture efficiencies in an AGTB turbine cascade are investigated numerically under various inlet angles of mainstream, blowing ratios, particle sizes, and particle densities. The effect of hole configuration on deposition is analyzed based on comparisons of results from combined hole and cylindrical hole. The impact efficiency increases with the increase of particle size. Impact area on pressure side of blade surface expands with increasing of the mainstream inlet angle from 123 deg to 143 deg. The capture efficiency decreases with the increase of blowing ratio for 10 µm particles. For particles with densities of 1485 kg/m3, 1980 kg/m3, and 2475 kg/m3, the maximum capture efficiency is reache...
In this paper, the effect of seal clearance on the efficiency of a turbine with a shrouded rotor is ...
The consequences of particle deposition on gas turbine blade surface are studied since the first gas...
Solid particle ingestion is one of the principal degradation mechanisms in the turbine and compresso...
This study numerically investigates film-cooling performance and particle trajectories in AGTB (two ...
The work considered here represents the first part for the study of the effect of deposition on the ...
The work considered here represents the second part of a study for the effect of ash par-ticle depos...
This paper presents a review of erosion and deposition research in turbomachines and the associated ...
ii A numerical study of the physical mechanisms associated with the deposition of coal ash particula...
Many land-based gas turbine applications are conducive to the formation of rust in the supply piping...
Flow evolving in turbomachinery applications is turbulent and laden by particles, such as dust, ash,...
Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, ...
Fouling affects gas turbine operation and airborne or fuel contaminants, under certain conditions, b...
Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, ...
Particle deposition on turbine blade surfaces is studied in this work. The turbine blade geometry is...
In the present thesis a study of the erosion rates that blades from a typical radial inflow turbine ...
In this paper, the effect of seal clearance on the efficiency of a turbine with a shrouded rotor is ...
The consequences of particle deposition on gas turbine blade surface are studied since the first gas...
Solid particle ingestion is one of the principal degradation mechanisms in the turbine and compresso...
This study numerically investigates film-cooling performance and particle trajectories in AGTB (two ...
The work considered here represents the first part for the study of the effect of deposition on the ...
The work considered here represents the second part of a study for the effect of ash par-ticle depos...
This paper presents a review of erosion and deposition research in turbomachines and the associated ...
ii A numerical study of the physical mechanisms associated with the deposition of coal ash particula...
Many land-based gas turbine applications are conducive to the formation of rust in the supply piping...
Flow evolving in turbomachinery applications is turbulent and laden by particles, such as dust, ash,...
Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, ...
Fouling affects gas turbine operation and airborne or fuel contaminants, under certain conditions, b...
Fouling affects gas turbine operation, and airborne or fuel contaminants, under certain conditions, ...
Particle deposition on turbine blade surfaces is studied in this work. The turbine blade geometry is...
In the present thesis a study of the erosion rates that blades from a typical radial inflow turbine ...
In this paper, the effect of seal clearance on the efficiency of a turbine with a shrouded rotor is ...
The consequences of particle deposition on gas turbine blade surface are studied since the first gas...
Solid particle ingestion is one of the principal degradation mechanisms in the turbine and compresso...