The goal of this study is to assess current, commonly applied turbulence and combustion models with respect to their performance in gas-turbine combustion (GTC). Reynolds Averaged Navier-Stokes (RANS)-based turbulence and chemistry models are two primary factors influencing the uncertainty in predicting turbulent combustion characteristics, especially for GTC. RANS-based methods are the design tools of choice in the gas turbine industry due to the high computational costs of LES (Large Eddy Simulation). In this study, lean premixed combustion of methane was simulated using two different reduced mechanisms (ARM9 and ARM19) along with the Eddy Dissipation Concept (EDC) turbulent chemistry interaction model to calculate the CO and NOx emission...
In the current study, a comparative study is performed using Large Eddy Simulation (LES) and Reynold...
Turbulent reacting flows in a generic swirl gas turbine combustor are investigated numerically. Turb...
RANS simulation of a gas turbine combustor with complex geometry is performed. The turbulence is mod...
DoctorThis thesis describes simulation of a small stationary gas turbine combustor of a reverse flow...
Abstract: The paper reviews progress in the development of methods for calculating the properties of...
Global environmental concerns and the increasing amount of power generated using gas turbines have l...
ABSTRACT INTRODUCTION The three-dimensional, viscous, turbulent, reacting and non-reacting flow char...
CFD predictions of emissions using conventional RANS methods have been shown to be inaccurate, somet...
A universally applicable user-friendly tool has been developed for numerical simulations of turbulen...
Turbulence modelling is a major issue, affecting the precision of current numerical simulations, par...
Gas turbine pollutant emissions (especially NOx and CO) are limited to 25 ppmvd by the European legi...
Siemens SGT-800 gas turbine is the largest industrial gas turbine within Siemens medium gas turbine ...
In the current study, a comparative study is performed using Large Eddy Simulation (LES) and Reynold...
This paper presents a Computational Fluid Dynamics (CFD) study of a natural gas combustion burner fo...
This paper presents a Computational Fluid Dynamics (CFD) study of a natural gas combustion burner fo...
In the current study, a comparative study is performed using Large Eddy Simulation (LES) and Reynold...
Turbulent reacting flows in a generic swirl gas turbine combustor are investigated numerically. Turb...
RANS simulation of a gas turbine combustor with complex geometry is performed. The turbulence is mod...
DoctorThis thesis describes simulation of a small stationary gas turbine combustor of a reverse flow...
Abstract: The paper reviews progress in the development of methods for calculating the properties of...
Global environmental concerns and the increasing amount of power generated using gas turbines have l...
ABSTRACT INTRODUCTION The three-dimensional, viscous, turbulent, reacting and non-reacting flow char...
CFD predictions of emissions using conventional RANS methods have been shown to be inaccurate, somet...
A universally applicable user-friendly tool has been developed for numerical simulations of turbulen...
Turbulence modelling is a major issue, affecting the precision of current numerical simulations, par...
Gas turbine pollutant emissions (especially NOx and CO) are limited to 25 ppmvd by the European legi...
Siemens SGT-800 gas turbine is the largest industrial gas turbine within Siemens medium gas turbine ...
In the current study, a comparative study is performed using Large Eddy Simulation (LES) and Reynold...
This paper presents a Computational Fluid Dynamics (CFD) study of a natural gas combustion burner fo...
This paper presents a Computational Fluid Dynamics (CFD) study of a natural gas combustion burner fo...
In the current study, a comparative study is performed using Large Eddy Simulation (LES) and Reynold...
Turbulent reacting flows in a generic swirl gas turbine combustor are investigated numerically. Turb...
RANS simulation of a gas turbine combustor with complex geometry is performed. The turbulence is mod...