Prediction of the Three-Dimensional Reacting Two-Phase Flow Within a Jet-Stabilized Combustor

Author:

Kurreck M.1,Willmann M.1,Wittig S.1

Affiliation:

1. Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), Karlsruhe, Federal Republic of Germany

Abstract

Numerical calculations of the two-phase flow in an experimentally well-investigated research combustor are presented. The comparison between measurements and calculations demonstrates the capabilities of the state-of-the-art Euler/Lagrange method for calculating two-phase flows, when applied to a complex reacting liquid-fueled combustor. The governing equations for gaseous and liquid phase are presented, with special emphasis on the control of the coupling process between the two phases. The relaxation method employed, together with a convergence history, shows a suitable way to achieve a fast and accurate solution for the strongly coupled two-phase flow under investigation. Furthermore, methods are presented to simulate the stochastic behavior of the atomization process caused by an air-blast atomizer. In addition to the numerical methods, experimental techniques are presented that deliver detailed information about droplet starting conditions.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference14 articles.

1. Abramovich, G. H., 1963, The Theory of Turbulent Jets, The M.I.T. Press, Mass. Inst. for Techn., Cambridge, MA.

2. Bauer, H. J., Eigenmann, L., Scherrer, B., and Wittig, S., 1995, “Local Measurements in a Three Dimensional Jet Stabilized Model Combustor,” ASME Paper No. 95-GT-71.

3. Gosman A. D. , and IoannidesE., 1983, “Aspects of Computer Simulation of Liquid-Fueled Combustors,” Journal of Energy, Vol. 7, No. 6, pp. 482–490.

4. Jeckel R., and Wittig S., 1993, “Time-Resolved Measurements in a Three Dimensional Model Combustor,” presented at the AGARD-PEP 81st Symposium on Fuel and Combustion Technology for Advanced Aircraft Engines, Colleferro, Roma, Italy, May 10–14.

5. Jeckel, R., Noll, B., and Wittig, S., 1992, “Three Dimensional Time-Resolved Velocity Measurements in a Model Combustor,” presented at the 6th International Symposium on the Application of Laser Techniques to Fluid Mechanics; Lisbon, Portugal, July 20–23.

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