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Theoretical and Experimental Investigations on Droplet Evaporation and Droplet Ignition at High PressuresThe evaporation of fuel droplets under high ambient pressure and temperature in normal gravity and microgravity has been investigated experimentally. For subcritical ambient conditions, droplet evaporation after a heat-up period follows the d(exp 2)-law. For all data the evaporation constant increases as the ambient temperature increases. At identical ambient conditions the evaporation constant under microgravity is smaller compared to normal gravity. This effect can first be observed at 1 bar and increases with ambient pressure. Preliminary experiments on ignition delay for self-igniting fuel droplets have been performed. Above a 1 s delay time, at identical ambient conditions, significant differences in the results of the normal and microgravity data are observed. Self-ignition occurs within different temperature ranges due to the influence of gravity. The time dependent behavior of the droplet is examined theoretically. In the calculations two different approaches for the gas phase are applied. In the first approach the conditions at the interface are given using a quasi steady theory approximation. The second approach uses a set of time dependent governing equations for the gas phase which are then evaluated. In comparison, the second model shows a better agreement with the drop tower experiments. In both cases a time dependent gasification rate is observed.
Document ID
19950031215
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ristau, R.
(University Bremen Bremen, Germany)
Nagel, U.
(University Bremen Bremen, Germany)
Iglseder, H.
(University Bremen Bremen, Germany)
Koenig, J.
(University Bremen Bremen, Germany)
Rath, H. J.
(University Bremen Bremen, Germany)
Normura, H.
(Nihon University Chiba, Japan)
Kono, M.
(Univ. of Tokyo Tokyo, Japan)
Tanabe, M.
(Univ. of Tokyo Tokyo, Japan)
Sato, J.
(IHI Research Institute Tokyo, Japan)
Date Acquired
August 29, 2013
Publication Date
December 1, 1993
Publication Information
Publication: Microgravity Science and Technology
Volume: 6
Issue: 4
ISSN: 0938-0108
Subject Category
Propellants And Fuels
Accession Number
95A62814
Funding Number(s)
PROJECT: RTOP 656-61-23
Distribution Limits
Public
Copyright
Other

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