Computation of the local flow structure, heat tranfer, and chemical species concentration in a two dimensional combustor of a gas turbine is described. The prediction is based on a modified TEACH computer program. A simulation of combustion of methne, the assumed fuel, is done in two major steps (C H4 ... C 0 + 2 H2 0 followed by C 0 + 1/2 02 ...C 02). In addition formation of other two dominant products, (NO) and (OH) is traced. Infleunce of some selected parameters, as air/fuel ratio, velocities ratio, diameters ratio on the performance of the combustor is demonstrated.
MOHAMED, S. (1984). A MODIFIED MATHEMATICAL MODELING IN GAS TURBINE COMBUSTORS. The International Conference on Applied Mechanics and Mechanical Engineering, 2(1st Conference on Applied Mechanical Engineering.), 123-133. doi: 10.21608/amme.1984.50333
MLA
SALAMA MOHAMED. "A MODIFIED MATHEMATICAL MODELING IN GAS TURBINE COMBUSTORS", The International Conference on Applied Mechanics and Mechanical Engineering, 2, 1st Conference on Applied Mechanical Engineering., 1984, 123-133. doi: 10.21608/amme.1984.50333
HARVARD
MOHAMED, S. (1984). 'A MODIFIED MATHEMATICAL MODELING IN GAS TURBINE COMBUSTORS', The International Conference on Applied Mechanics and Mechanical Engineering, 2(1st Conference on Applied Mechanical Engineering.), pp. 123-133. doi: 10.21608/amme.1984.50333
VANCOUVER
MOHAMED, S. A MODIFIED MATHEMATICAL MODELING IN GAS TURBINE COMBUSTORS. The International Conference on Applied Mechanics and Mechanical Engineering, 1984; 2(1st Conference on Applied Mechanical Engineering.): 123-133. doi: 10.21608/amme.1984.50333
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