Lean perfectly premixed flame propagation in a swirling flow dump combustor is studied. The emphasis is on flame propagation in the Broken Reaction-Zone (BRZ), where the reaction zone thickness (δF) is larger than the Kolmogorov scale (η). The Linear-Eddy Mixing (LEM) model is used to simulate subgrid interactions between the flame structure and the unresolved turbulent structures within the framework of a large-eddy simulation (LES) approach. A real case scenario is studied: the propagation of a lean premixed flame in a dump combustion chamber where heat losses at the walls are taken into account via the use of a simple heat loss model. Results show flame lift-off, caused by flame quenching, for low equivalence ratio (Φ=0.45). The dynamics...
Large Eddy Simulations of an unconfined turbulent lean practical flame stabilised behind a bluff bod...
Large Eddy Simulation (LES) of bluff body stabilized premixed and partially premixed combustion clos...
This paper investigates flame and flow structure of a swirl-stabilized pilot combustor in convention...
The use of lifted flames presents some very promising advantages in terms of pollutant emissions and...
Premixed and partially premixed lean combustion is utilised in modern gas turbine systems, since an ...
This paper presents a joint experimental and large eddy simulation (LES) study of lean premixed low ...
Flame holding and its propagation characteristics in a lean premixed swirl stabilized combustor is s...
A swirl-stabilised flame close to blow-off conditions in a gas turbine model combustor is investigat...
The present study numerically investigates a low-swirl partially premixed lifted flame employing gas...
This thesis deals with numerical simulation of reactive flows. The numerical method is three dimensi...
This work examines the three main aspects of bluff-body stabilized flames: stationary combustion, le...
A premixed propane–air flame stabilised on a triangular bluff body in a model jet-engine afterburner...
The dynamics in a swirl-stabilized flame is studied using large eddy simulation (LES). We account fo...
Large-Eddy Simulation (LES) methodology has been used to model combustion dynamics in a real-istic s...
International audienceSwirl burners are widely used in aeronautical engines and industrial gas turbi...
Large Eddy Simulations of an unconfined turbulent lean practical flame stabilised behind a bluff bod...
Large Eddy Simulation (LES) of bluff body stabilized premixed and partially premixed combustion clos...
This paper investigates flame and flow structure of a swirl-stabilized pilot combustor in convention...
The use of lifted flames presents some very promising advantages in terms of pollutant emissions and...
Premixed and partially premixed lean combustion is utilised in modern gas turbine systems, since an ...
This paper presents a joint experimental and large eddy simulation (LES) study of lean premixed low ...
Flame holding and its propagation characteristics in a lean premixed swirl stabilized combustor is s...
A swirl-stabilised flame close to blow-off conditions in a gas turbine model combustor is investigat...
The present study numerically investigates a low-swirl partially premixed lifted flame employing gas...
This thesis deals with numerical simulation of reactive flows. The numerical method is three dimensi...
This work examines the three main aspects of bluff-body stabilized flames: stationary combustion, le...
A premixed propane–air flame stabilised on a triangular bluff body in a model jet-engine afterburner...
The dynamics in a swirl-stabilized flame is studied using large eddy simulation (LES). We account fo...
Large-Eddy Simulation (LES) methodology has been used to model combustion dynamics in a real-istic s...
International audienceSwirl burners are widely used in aeronautical engines and industrial gas turbi...
Large Eddy Simulations of an unconfined turbulent lean practical flame stabilised behind a bluff bod...
Large Eddy Simulation (LES) of bluff body stabilized premixed and partially premixed combustion clos...
This paper investigates flame and flow structure of a swirl-stabilized pilot combustor in convention...