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NASA NTRS · 19930038655

Two and three-dimensional prediffuser combustor studies with air-water mixture

Abstract

Two- and three-dimensional gas turbine prediffuser-combustor sectors were experimentally studied under a number of mixture and flow conditions in a tunnel operating with a two-phase, air-liquid film-droplet mixture. It is concluded that water vaporization in the combustor causes changes in both local gas temperature and state of vitiation and reduces reaction rates. Substantial accumulation of water and water vapor takes place in pocket over the combustor volume, even when the air-water mixture is steady in time. The accuracy of determining combustor performance changes increases with a better knowledge of the state of the air-water mixture in the primary zone. To establish flame-out conditions it is considered to be necessary to combine the prediction of detailed flowfield and chemical activity with that of flame stability and motion characteristics.

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BibTeXRIS

Laing, Peter, Ehresman, C. M., Murthy, S. N. B.. 1993-01-01. Two and three-dimensional prediffuser combustor studies with air-water mixture. https://ntrs.nasa.gov/citations/19930038655

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