High-Resolution One-Dimensional Modeling of a Gas Turbine Combustor Using Eulerian-Lagrangian Method

Autor: Reza Khodadadi, Nima Zamani Meymian
Rok vydání: 2019
Předmět:
bepress|Engineering|Aerospace Engineering|Propulsion and Power
engrXiv|Engineering|Mechanical Engineering|Computer-Aided Engineering and Design
bepress|Engineering
engrXiv|Engineering|Aerospace Engineering|Propulsion and Power
engrXiv|Engineering|Mechanical Engineering|Fluid Mechanics
engrXiv|Engineering|Chemical Engineering|Thermodynamics
bepress|Engineering|Chemical Engineering|Thermodynamics
bepress|Engineering|Mechanical Engineering
engrXiv|Engineering|Mechanical Engineering
bepress|Engineering|Chemical Engineering
bepress|Engineering|Aerospace Engineering
bepress|Engineering|Mechanical Engineering|Computer-Aided Engineering and Design
engrXiv|Engineering|Chemical Engineering
engrXiv|Engineering|Mechanical Engineering|Heat Transfer
engrXiv|Engineering|Aerospace Engineering
Physics::Fluid Dynamics
bepress|Engineering|Mechanical Engineering|Heat Transfer
Combustion

engrXiv|Engineering
bepress|Engineering|Computational Engineering
engrXiv|Engineering|Computational Engineering
engrXiv|Engineering|Automotive Engineering
bepress|Engineering|Aerospace Engineering|Aerodynamics and Fluid Mechanics
engrXiv|Engineering|Mechanical Engineering|Combustion
bepress|Engineering|Automotive Engineering
Popis: In this paper, a dynamic combustor model for inclusion into a one-dimensional full gas turbine engine simulation model, with high numerical accuracy is developed. Effects of dominant parameters, such as frequency and amplitude of the inlet air and fuel mass flow rate fluctuations, on outlet temperature of the combustion chamber, are investigated. The main goal of this research is to analyze the response of the gas turbine combustor to dynamic events that occur in the compressor. In the present work, for modeling combustion, the equations of chemical equilibrium (a second-law concept) are developed and applied to combustion-product mixtures. Thus the heat released from combustion is computed and used as a source term in the energy equation. Ignition effects either would be considered with a time lag equation as a source term in the energy equation. The combustor flammability limits are determined by using available experimental data for various gases and also Le Chatelier’s law. Source terms of governing equations are added using the operator splitting method. To operate this, the modified version of the PPM algorithm called PPMLR is used which solves the Euler equations in Lagrangian coordinates. At the end of each time step, results calculated in the Lagrangian coordinates would remap to the original Eulerian coordinate. The results revealed that to achieve a grid-independent solution, the accuracy of 0.002 m over the length of the combustion chamber should be applied. By reducing the accuracy of simulation, numerical diffusion causes a rise in flow temperature along with the combustion chamber. Through the dynamic modeling aspect, it is found that by increasing inlet fuel flow rate frequency up to 25 Hz, the amplitude of the fluctuations of outlet temperature, increases. Further increase in frequency up to 100 Hz, the amplitude of the fluctuations remains unchanged. However further increases in frequency from 100 Hz, causes amplitudes of outlet temperature fluctuations to decrease.
Databáze: OpenAIRE