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Large Diameter, Radiative Extinction Experiments with Decane Droplets in MicrogravityThe extinction of a diffusion flame is of fundamental interest in combustion science. Linan, Law, and Chung and Law analytically and experimentally determined an extinction boundary in terms of droplet diameter and pressure for a single droplet due to Damkohler, or blowoff, extinction. More recently, other researchers demonstrated extinction due to finite rate kinetics in reduced gravity for free droplets of heptane. Chao modeled the effect of radiative heat loss on a quasi-steady spherically symmetric single droplet burning in the absence of buoyancy. They determined that for increasing droplet diameter, a second limit can be reached such that combustion is no longer possible. This second, larger droplet diameter limit arises due to radiative heat loss, which increases with increasing droplet and flame diameter. This increase in radiative heat loss arises due to an increase in the surface area of the flame. Recently, Marchese modeled fuel droplets with detailed chemistry and radiative effects, and compared the results to other work. The modeling also showed the importance of radiative loss and radiative extinction Experiments examined the behavior of a large droplet of decane burning in reduced gravity onboard the NASA Lewis DC-9 aircraft, but did not show a radiative extinction boundary due to g-jitter (Variations in gravitational level and direction) effects. Dietrich conducted experiments in the reduced gravity environment of the Space Shuttle. This work showed that the extinction diameter of methanol droplets increased when the initial diameter of the droplets was large (in this case, approximately 5 mm). Theoretical results agreed with these experimental results only when the theory included radiative effects . Radiative extinction was experimentally verified by Nayagam in a later Shuttle mission. The following work focuses on the combustion and extinction of a single fuel droplet. The goal is to experimentally determine a large droplet diameter limit that arises due to radiative heat loss from the flame to the surroundings.
Document ID
20000007141
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Easton, John
(Case Western Reserve Univ. Cleveland, OH United States)
Tien, James
(Case Western Reserve Univ. Cleveland, OH United States)
Dietrich, Daniel
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Inorganic, Organic And Physical Chemistry
Meeting Information
Meeting: 1st Joint Meeting of the U.S. Sections of the Combustion Institute
Location: Washington, DC
Country: United States
Start Date: March 14, 1999
End Date: March 17, 1999
Sponsors: Combustion Inst., George Washington Univ.
Funding Number(s)
PROJECT: RTOP 962-22-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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