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  • Influence of Sootshell Formation on Droplet Burning Rate and Radiative Heat Transfer in Microgravity Ethanol Droplet Combustion

    Paper number

    IAC-09.A2.2.8

    Author

    Dr. Seul Hyun Park, Drexel University, United States

    Coauthor

    Mr. Mun Young Choi, University of Connecticut, United States

    Year

    2009

    Abstract
    The influence of sootshell formed in microgravity ethanol droplet flames on the
    droplet burning rate and radiative heat transfer was investigated through various
    measurements including the burning rate, soot standoff ratio, soot volume fraction, soot
    temperature and radiative heat losses. Microgravity ethanol droplet combustion
    experiments were performed at the NASA 2.2 s droptower in Cleveland, OH U.S.A. To
    quantitatively analyze the influence of sootshell on the burning rate and radiative heat
    transfer, the sootshell location was varied by means of inert gas substitution (argon vs.
    nitrogen). These experiments demonstrated strong influence of inert gas substitution
    (that caused changes in the thermophysical properties and temperature) between argon
    and nitrogen. The experimentally measured soot standoff ratio (SSR) for the argon inert
    experiment was ~1.4, whereas the value for the nitrogen inert experiment was ~ 2.5. The
    † Corresponding Author: Email:seulpark@nist.gov ; +1-975-301-3908 (O); +1-975-301-4052 (F)\
    Current address: Building and Fire Research Laboratory (BFRL)
    National Institute of Standards and Technology (NIST)
    Gaithersburg, MD 20899-8662
    calculated SSR for each of inert experiments using balance among Stefan, thermophoretic,
    and diffusiophoretic fluxes are also in excellent agreement with the experimental
    measurements. These experiments clearly indicate that the sootshell location influences
    the radiative heat transfer from the flame to the droplet and to the surrounding
    environment and can modify the burning rate.
    Keywords: Ethanol, Sootshell, Droplet Combustion, Microgravity, Radiative Heat Loss
    Abstract document

    IAC-09.A2.2.8.pdf

    Manuscript document

    (absent)