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Microgravity Experiment on Flame Spread of a Fuel Droplet ArrayFlame spread phenomena in a suspended fuel droplet array were experimentally investigated for n-decane and n-hexadecane in microgravity and normal gravity. Seven droplets of the same size were arranged horizontally at equal spacings. Flame spread rates were measured based on OH emission histories detected by a high-speed video camera with an image intensifier for droplet diameters of 0.50, 0.75, and 1.0 mm at ambient pressure from 0.1 to about 2.0 MPa. Results show that, as droplet spacing becomes smaller, flame spread rate increases and has a maximum value at a certain spacing in both microgravity and normal gravity. A further decrease in droplet spacing causes the spread rate to decrease due to the large latent heat of vaporization. The flame spread rate in microgravity is larger than that in normal gravity. The spacing at the flame spread limit in microgravity is more than two times as large as that in normal gravity, but the spacing at the maximum flame spread rate in microgravity is only a little larger than that in normal gravity.
Document ID
19970020626
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Shinichiro Kato
(Tohoku University Sendai, Japan)
Hiroyuki Mizuno
(Tohoku University Sendai, Japan)
Hideaki Kobayashi
(Tohoku University Sendai, Japan)
Takashi Niioka
(Tohoku University Sendai, Japan)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Materials Processing
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21899
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
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