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Forced ignition of turbulent spray flames

Accepted version
Peer-reviewed

Type

Article

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Authors

Mastorakos, Epaminondas  ORCID logo  https://orcid.org/0000-0001-8245-5188

Abstract

This paper reviews the current state of knowledge on the initiation of a flame in a spray through the action of a spark or through local deposition of heat, and the subsequent flame development, in uniform and non-uniform dispersions of droplets and in the presence of turbulent flow. These processes are of importance in various applications such as gas turbine ignition (relight) and safety related to flammable liquid mists. The review focuses on the initial kernel development, the evolution of a spherical or edge flame, and the ignition of the spray flame when viewed at the whole combustor scale. The factors that determine success or failure of the ignition process at the various phases of the overall burner ignition are discussed through experiments and Direct Numerical Simulations, while modelling efforts are also assessed. The fuel volatility, droplet size, overall fuel-to-air ratio, and the degree of pre-evaporation are the important factors that distinguish spray ignition from gaseous flame ignition, and the extra fluctuations introduced by the random droplet locations, and how this may affect modelling and flame evolution, are highlighted. The flame propagation mechanism in laminar and turbulent sprays is one of the key aspects determining overall ignition success. Suggestions for future research are discussed.

Description

Keywords

Forced ignition, Spark, Spray, Relight, Ignition probability

Journal Title

Proceedings of the Combustion Institute

Conference Name

Journal ISSN

1540-7489
1873-2704

Volume Title

36

Publisher

Elsevier BV
Sponsorship
Engineering and Physical Sciences Research Council (EP/K025791/1)
Engineering and Physical Sciences Research Council (EP/J021644/1)
European Commission (641453)
European Commission (211843)
European Commission FP6 Specific Targeted Research Projects (STReP) (AST5-CT-2006-030828)
European Commission, Engineering and Physical Sciences Research Council (Grant ID: EP/J021644/1), Rolls-Royce Group