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Ensemble Diffraction Measurements of Spray Combustion in a Novel Vitiated Coflow Turbulent Jet Flame BurnerAn experimental investigation is presented of a novel vitiated coflow spray flame burner. The vitiated coflow emulates the recirculation region of most combustors, such as gas turbines or furnaces; additionally, since the vitiated gases are coflowing, the burner allows exploration of the chemistry of recirculation without the corresponding fluid mechanics of recirculation. As such, this burner allows for chemical kinetic model development without obscurations caused by fluid mechanics. The burner consists of a central fuel jet (droplet or gaseous) surrounded by the oxygen rich combustion products of a lean premixed flame that is stabilized on a perforated, brass plate. The design presented allows for the reacting coflow to span a large range of temperatures and oxygen concentrations. Several experiments measuring the relationships between mixture stoichiometry and flame temperature are used to map out the operating ranges of the coflow burner. These include temperatures as low 300 C to stoichiometric and oxygen concentrations from 18 percent to zero. This is achieved by stabilizing hydrogen-air premixed flames on a perforated plate. Furthermore, all of the CO2 generated is from the jet combustion. Thus, a probe sample of NO(sub X) and CO2 yields uniquely an emission index, as is commonly done in gas turbine engine exhaust research. The ability to adjust the oxygen content of the coflow allows us to steadily increase the coflow temperature surrounding the jet. At some temperature, the jet ignites far downstream from the injector tube. Further increases in the coflow temperature results in autoignition occurring closer to the nozzle. Examples are given of methane jetting into a coflow that is lean, stoichiometric, and even rich. Furthermore, an air jet with a rich coflow produced a normal looking flame that is actually 'inverted' (air on the inside, surrounded by fuel). In the special case of spray injection, we demonstrate the efficacy of this novel burner with a methanol spray in a vitiated coflow. As a proof of concept, an ensemble light diffraction (ELD) optical instrument was used to conduct preliminary measurements of droplet size distribution and liquid volume fraction.
Document ID
20000112945
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cabra, R.
(California Univ. Berkeley, CA United States)
Hamano, Y.
(California Univ. Berkeley, CA United States)
Chen, J. Y.
(California Univ. Berkeley, CA United States)
Dibble, R. W.
(California Univ. Berkeley, CA United States)
Acosta, F.
(Process Metrix, LLC San Ramon, CA United States)
Holve, D.
(Process Metrix, LLC San Ramon, CA United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2000
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2000-210466
E-12462
NAS 1.26:210466
Report Number: NASA/CR-2000-210466
Report Number: E-12462
Report Number: NAS 1.26:210466
Funding Number(s)
PROJECT: RTOP 523-90-13
CONTRACT_GRANT: NAG3-2103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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