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Characterization of Liquid Fuel Evaporation of a Lifted Methanol Spray Flame in a Vitiated Coflow BurnerAn experimental investigation of lifted spray flames in a coflow of hot, vitiated gases is presented. The vitiated coflow burner is a spray flame that issues into a coaxial flow of hot combustion products from a lean, premixed H2/Air flame. The spray flame in a vitiated coflow emulates the combustion that occurs in many advanced combustors without the detailed fluid mechanics. Two commercially available laser diagnostic systems are used to characterize the spray flame and to demonstrate the vitiated coflow burner's amenability to optical investigation. The Ensemble Particle Concentration and Size (EPCS) system is used to measure the path-average droplet size distribution and liquid volume fraction at several axial locations while an extractive probe instrument named the Real-time Fuel-air Analyzer (RFA) is used to measure the air to fuel ratio downstream of the spray nozzle with high temporal and spatial resolution. The effect of coflow conditions (stoichiometry) and dilution of the fuel with water was studied with the EPCS optical system. As expected, results show that water retards the evaporation and combustion of fuels. Measurements obtained by the RFA extractive probe show that while the Delavan manufactured nozzle does distribute the fuel over the manufacturer specified spray angle, it unfortunately does not distribute the fuel uniformly, providing conditions that may result in the production of unwanted NOx. Despite some limitations due to the inherent nature of the experimental techniques, the two diagnostics can be readily applied to spray flames in the vitiated coflow environment.
Document ID
20030014738
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Cabra, Ricardo
(California Univ. Berkeley, CA United States)
Dibble, Robert W.
(California Univ. Berkeley, CA United States)
Chen, Jyh-Yuan
(California Univ. Berkeley, CA United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2002
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-13736
NASA/CR-2002-212083
NAS 1.26:212083
Report Number: E-13736
Report Number: NASA/CR-2002-212083
Report Number: NAS 1.26:212083
Funding Number(s)
CONTRACT_GRANT: NAG3-2103
PROJECT: RTOP 708-90-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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