Partial-Burning Regime for Quasi-Steady Droplet Combustion Supported by Cool Flames

被引：21
|
作者：
Nayagam, Vedha [1 ]
Dietrich, Daniel L. [2 ]
Williams, Forman A. [3 ]
机构：
[1] Case Western Reserve Univ, Dept Mech & Aerosp Engn, Cleveland, OH 44106 USA
[2] NASA, John H Glenn Res Ctr, Dept Mech & Aerosp Engn, Cleveland, OH 44135 USA
[3] Univ Calif San Diego, Dept Mech & Aerosp Engn, La Jolla, CA 92093 USA
来源：
AIAA JOURNAL | 2016年 / 54卷 / 04期
关键词：
N-HEPTANE; MICROGRAVITY; EXTINCTION;
D O I：
10.2514/1.J054437
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A simplified model for droplet combustion in the partial-burning regime is applied to the cool-flame regime observed in droplet-burning experiments performed in the International Space Station with normal-alkanes fuels resulting in expressions for the quasi-steady droplet burning rate and for the flame standoff ratio. The simplified predictions are found to produce reasonable agreement with the experimentally measured values of burning-rate constants but not with their apparent dependencies on pressure or on the initial droplet diameter. Good agreement is found, however, with newly measured and numerically calculated flame standoff ratios in this droplet combustion supported by cool flames.
引用
收藏
页码：1235 / 1239
页数：5
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