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NASA NTRS ยท 19820023766

Flow process in combustors

Abstract

Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine combustors were investigated. Flow features of most interest were vorticity, especially swirl, and turbulence. Theoretical analyses, numerical calculations, and experiments were performed. The theoretical and numerical work focused on noncombusting flows, while the experimental work consisted of both reacting and nonreacting flow studies. An experimental data set, e.g., velocity, temperature and composition, was developed for a swirl flow combustor for use by combustion modelers for development and validation work.

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BibTeXRIS

Gouldin, F. C.. 1982-06-01. Flow process in combustors. https://ntrs.nasa.gov/citations/19820023766

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