Pre-integrated Nonequilibrium Combustion-Response Mapping for Gas Turbine Emissions
Author:
Korakianitis T.1, Dyer R.2, Subramanian N.2
Affiliation:
1. James Watt Professor of Mechanical Engineering, University of Glasgow, Glasgow G12 8QQ, Scotland 2. Mechanical Engineering Department, Washington University, Campus Box 1185, 1 Brookings Drive, St. Louis, MO 63130
Abstract
In gas turbine combustion the gas dynamic and chemical energy release mechanisms have comparable time scales, so that equilibrium chemistry is inadequate for predicting species formation (emissions). In current practice either equilibrium chemical reactions are coupled with experimentally derived empirical equations, or time-consuming computations are used. Coupling nonequilibrium chemistry, fluid dynamic, and initial and boundary condition equations results in large sets of numerically stiff equations; and their time integration demands enormous computational resources. The response modeling approach has been used successfully for large reaction sets. This paper makes two new contributions. First it shows how pre-integration of the heat release maps eliminates the stiffness of the equations. This is a new modification to the response mapping approach, and it performs satisfactorily for non-diffusion systems. Second the theoretical framework is further extended to predict species formation in cases with diffusion, which is applicable to gas turbine combustion systems and others. The methodology to implement this approach to reacting systems, and to gas turbine combustion, is presented. The benefits over other reaction-mapping techniques are discussed.
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference23 articles.
1. Lefebvre, A. H.
, 1995, “The Role of Fuel Preparation in Low-Emission Combustion,” ASME J. Eng. Gas Turbines Power, 117, pp. 617–654. 2. Rizk, N. K., and Mongia, H. C., 1994, “Emissions Predictions of different Gas Turbine Combustors,” AIAA Paper No. 94-0118. 3. Jones, W. P., and Priddin, C. H., 1978, “Predictions of the Flow Field and Local Gas Composition in Gas Turbine Combustors,” Proceedings of the 17th International Symposium on Combustion, The Combustion Institute, Pittsburgh, PA., pp. 399–409. 4. Smith, G. P., Golden, D. M., Frenklach, M., Moriarty, N. W., Eitcneer, B., Goldenberg, M., Bowman, C. T., Hanson, R. K., Song, S., Gardiner, W. C., Jr., Lissianski, V. V., and Qin, Z., GRI-Mech 3.0 http://www.me.berkeley.edu/gri_mech/ 5. Zeldovich, Ya. B., Sadovnikov, P. Ya., and Frank Kamnetskii, D. A., 1947, “Oxidation of Nitrogen in Combustion,” Academy of Sciences of the USSR, Moscow.
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