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NASA NTRS · 19790016838

Stabilization of premixed combustors

Abstract

In order to attain a sufficiently good insight into the fluid mechanical processes taking place in combustors operating on premixed, prevaporized, and preheated gases, an experimental facility was developed where the flow field is tractable both experimentally and analytically. The configuration adopted for the initial stage of the study is based on the use of a step to stabilized the combustion zone. The primary purpose of the experimental apparatus is to provide a facility for studying the effects of the elementary fluid mechanical processes on the stability of a model combustion system in order to further the understanding of the intrinsic mechanism of nonsteady phenomena, rather than to provide criteria for unstable operation of combustors, as expressed by overall performance parameters, such as the blowout and flashback limits.

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BibTeXRIS

Sawyer, R. F., Daily, J. W., Oppenheim, A. K.. 1979-01-01. Stabilization of premixed combustors. https://ntrs.nasa.gov/citations/19790016838

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