Predicting the ignition sequences in a separated stratified swirling spray flame with stochastic flame particle tracking

Author:

Xie Qing1,Yang Siheng2,Cheng Hao2,Zhang Chi3,Ren Zhuyin1

Affiliation:

1. Institute for Aero Engine, Tsinghua University, Beijing, 100084, China

2. National Key Laboratory of Science and Technology on Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing, 100191, China

3. National Key Laboratory of Science and Technology on Aero-Engine, Research Institute of Aero-Engine, Beihang University, Beijing 100191, China

Abstract

Stochastic flame particle tracking in conjunction with non-reacting combustor simulations can offer insights into the ignition processes and facilitate the combustor optimization. In this study, this approach is employed to simulate the ignition sequences in a separated dual-swirl spray flame, in which the newly proposed pairwise mixing-reaction model is used to account for the mass and energy transfer between the flame particle and the surrounding shell layer. Based on the flame particle temperature, the particle state can be classified in to burnt, hot gas, and extinguished. The additional state of hot gas is introduced to allow the flame particles with high temperature to survive from nonflammable region and then potentially to ignite the nearby favourable regions. The simulations of the separated stratified swirl spray flame reveal two different ignition pathways for flame stabilization. The first showed that some flame particles from the spark would directly enter the main recirculation zone resulting from the velocity randomness and then ignite both sides of the combustor simultaneously. The second showed that flame particles from the spark would ignite the traversed regions following the swirl motion inside the combustor. The predicted ignition sequences were compared with the evolution of flame morphology recorded by high-speed imaging from experiments, showing qualitative agreement.

Publisher

Global Power and Propulsion Society

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering

Reference27 articles.

1. Droplet vaporization model for spray combustion calculations

2. Spark ignition of turbulent nonpremixed bluff-body flames

3. Ahmed S., Bahena I., Ledezma I. A., and Mastorakos E. (2009). Spark ignition in a turbulent shearless fuel-air mixing layer: average flame growth rates. In: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, USA, Janurary, p. 238.

4. Numerical investigation of edge flame propagation characteristics in turbulent mixing layers

5. A statistical model to predict ignition probability

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