Combustion flows with different fuels as heptane and pyrolysis gas in a dual-fuel-combustor of gas turbine were simulated by a CFD(computational fluid dynamics) method.The RNG(renormalization group) k-ε turbulence model
single chemistry reaction system
infinite-rate reaction velocity
discrete phase modeling for liquid fuel
upwind discretization scheme and the SIMPLE algorithm were applied.Some performances of combustor such as: combustion efficiency
temperature uniformity at outlet
temperature distribution of walls
distribution of air mass flow and the first air excess coefficient
were also analyzed.Some results show that: 1) the distribution of mass flow rate is consistent with different fuels
2) there is a 1% higher combustion efficiency and lower temperature uniformity at outlet with pyrolysis gas than that of oil fuel
3) the average temperature at outlet with pyrolysis gas is 20~40K lower than that of oil fuel with the same chemical enthalpy injected in the combustor
and 4) the first air excess coefficient α of pyrolysis gas is higher than that of oil fuel.
Analysis of matching characteristic of transonic tandem stator airfoil and its optimization
Numerical simulation of a novel turbine inter-vane burner
Numerical simulation and design improvement of leading-edge film cooling in an inlet guide vane
Numerical simulation of jet impingement cooling of turbine steam-cooling vane
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Related Author
TAO Yuan
YU Xian-jun
LIU Bao-jie
LI Ming
TANG Hao
ZHANG Chao
CHENG Ben-lin
MO Da
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Institute of Engineering Thermophysics, Chinese Academy of Science
Department of Thermal Engineering, Tsinghua University
School of Power and Energy,Northwestern Polytechnical University