4.6 Article

Effect of non-zero relative velocity on the flame speed of two-phase laminar flames

Journal

PROCEEDINGS OF THE COMBUSTION INSTITUTE
Volume 37, Issue 3, Pages 3393-3400

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.proci.2018.07.100

Keywords

Direct numerical simulation; Lagrangian particle tracking; Laminar flame; Spray flame

Funding

  1. Safran Helicopter Engines
  2. ANRT/CIFRE
  3. GENCI-CINES [Dari A0012B10157]

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A numerical study of one-dimensional n-heptane/air spray flames is presented. The objective is to evaluate the flame propagation speed in the case where droplets evaporate inside the reaction zone with possibly non-zero relative velocity. A Direct Numerical Simulation approach for the gaseous phase is coupled to a discrete particle Lagrangian formalism for the dispersed phase. A global two-step n-heptane/air chemical mechanism is used. The effects of initial droplet diameter, overall equivalence ratio, liquid loading and relative velocity between gaseous and liquid phases on the laminar spray flame speed and structure are studied. For lean premixed cases, it is found that the laminar flame speed decreases with increasing initial droplet diameter and relative velocity. On the contrary, rich premixed cases show a range of diameters for which the flame speed is enhanced compared to the corresponding purely gaseous flame. Finally, spray flames controlled by evaporation always have lower flame speeds. To highlight the controlling parameters of spray flame speed, approximate analytical expressions are proposed, which give the correct trends of the spray flame propagation speed behavior for both lean and rich mixtures. (C) 2018 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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