Spray Computations in a Centerbody Combustor

[+] Author and Article Information
M. S. Raju, W. A. Sirignano

Department of Mechanical Engineering, University of California, Irvine, Irvine, CA 92717

J. Eng. Gas Turbines Power 111(4), 710-718 (Oct 01, 1989) (9 pages) doi:10.1115/1.3240317 History: Received February 01, 1988; Online October 15, 2009


A hybrid Eulerian–Lagrangian method is employed to model the reactive flow field of a centerbody combustor. The unsteady two-dimensional gas-phase equations are represented in Eulerian coordinates and liquid-phase equations are formulated in Lagrangian coordinates. The gas-phase equations based on the conservation of mass, momentum, and energy are supplemented by turbulence and combustion models. The vaporization model takes into account the transient effects associated with the droplet heating and liquid-phase internal circulation. The integration scheme is based on the TEACH algorithm for gas-phase equations, the Runge-Kutta method for liquid-phase equations, and linear interpolation between the two coordinate systems. The calculations show that the droplet penetration and recirculation characteristics are strongly influenced by the gas- and liquid-phase interaction in such a way that most of the vaporization process is confined to the wake region of the centerbody, thereby improving the flame stabilization properties of the flow field.

Copyright © 1989 by ASME
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