The ignition of methane by laser spark in a small combustion chamber has been modelled using CFD-code ANSYS CFX. The numerical simulations were performed in a 2D axisymmetric geometry. Turbulence has been modelled using SST turbulence model while the combustion of methane has been modelled with the help of the combined Eddy Dissipation/Finite Rate Chemistry model and a one-step kinetic mechanism. The numerical results have been compared with the experiments by the pressure inside the combustion chamber. The filling of the combustion chamber with the propellants before the ignition and the stationary combustion in the chamber have been modelled accurately. However the numerical model predicts notably higher pressure peak immediately after th...
Currently, CFD simulations are an invaluable support of experimental researches and stands, especial...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...
Methane has never been used as rocket fuel in a flight mission up to now. However, for upper stage ...
This paper describes a numerical study of the laser-pulse ignition sequence occurring in the combust...
This paper describes a numerical study of the laser-pulse ignition sequence occurring in the combust...
A successful ignition is the consequence of corresponding conditions of fuel mass flow rates, mixtur...
Transient mixing and ignition mechanisms in a simplified pre-chamber/main-chamber system are investi...
The understanding of the ignition process is important for many practical and fundamental applicatio...
The influence of using different chemistry model and different chemical kinetics schemes on modeling...
The control of ignition in a rocket engine is a critical problem for combustion chamber design. Dela...
Methane supply in diesel engines operating in dual fuel mode has demonstrated to be effective for th...
This work presents the results of a numerical simulation of the combustion of natural gas (methane) ...
Methane supply in diesel engines operating in dual fuel mode has demonstrated to be effective for th...
In this study the combustion characteristics of the turbulent combustion of a gaseous fuel (methane)...
Currently, CFD simulations are an invaluable support of experimental researches and stands, especial...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...
Methane has never been used as rocket fuel in a flight mission up to now. However, for upper stage ...
This paper describes a numerical study of the laser-pulse ignition sequence occurring in the combust...
This paper describes a numerical study of the laser-pulse ignition sequence occurring in the combust...
A successful ignition is the consequence of corresponding conditions of fuel mass flow rates, mixtur...
Transient mixing and ignition mechanisms in a simplified pre-chamber/main-chamber system are investi...
The understanding of the ignition process is important for many practical and fundamental applicatio...
The influence of using different chemistry model and different chemical kinetics schemes on modeling...
The control of ignition in a rocket engine is a critical problem for combustion chamber design. Dela...
Methane supply in diesel engines operating in dual fuel mode has demonstrated to be effective for th...
This work presents the results of a numerical simulation of the combustion of natural gas (methane) ...
Methane supply in diesel engines operating in dual fuel mode has demonstrated to be effective for th...
In this study the combustion characteristics of the turbulent combustion of a gaseous fuel (methane)...
Currently, CFD simulations are an invaluable support of experimental researches and stands, especial...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...
The numerical simulation for the starting process of the ram accelerator in Hiroshima University (HU...