The study of droplet ignition in hot convective environment
碩士 === 國立成功大學 === 航空太空工程學系 === 81 === The fuel droplets spout from injector nozzle contains several different sizes of diamete, and the life time of these droplets is an important factor in combustion chamber and sprayer design . Therefore...
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ndltd-TW-081NCKU02950292016-07-20T04:11:34Z http://ndltd.ncl.edu.tw/handle/41253607093844099092 The study of droplet ignition in hot convective environment 燃油滴於熱流場之點火研究 Chir-Shyong Lin 林琦雄 碩士 國立成功大學 航空太空工程學系 81 The fuel droplets spout from injector nozzle contains several different sizes of diamete, and the life time of these droplets is an important factor in combustion chamber and sprayer design . Therefore , it is an important study to understand the vaporization / combustion situation of a single fuel droplet in a high temperature and oxidizing environment with external flow. Especially , the study of droplet ignition plays an important role to understand the droplet combustion phenomena. In a real fuel spray combustor , the combustion of fuel droplets occure in a convective , high temperature , oxidizing environment and the relative motion of neighboring air turns the problems into two dimensional or more . Due to the complex chemical reaction and fluid interaction with combustion , the droplet combustion becomes an extremely difficult phenomenon to solve . This research of simple ignition model is to understand the effects of the fuel droplets and of the external environment on the ignition delay . Threeply - period concept is introduced to interpret the dominant factors that govern the ignition process . Numerical technique is applied to get an insight of transient behavior of a fuel droplet to ignition . A special hybird numerical scheme ICED-ALE is used to circumvent the difficulties arising from the rapid transition of ignition and regression offuel droplet . The results indicated the droplet in smaller dimension is easier to be be ignited in most cases . But in higher temperature enviroment , the dimension of fuel droplet affects the delay times less .At enviroment temperature of 1050 k , the ignition delay time difference between large and small fuel droplet is 7.7% . Basically , it saves 34.6% time for fuel droplet ignition in convective enviroment than one in stagnant which coincides the real physical situation . J. M. Char 、S. M. Liang 賈澤民 、梁勝明 1993 學位論文 ; thesis 67 zh-TW |
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碩士 === 國立成功大學 === 航空太空工程學系 === 81 === The fuel droplets spout from injector nozzle contains several
different sizes of diamete, and the life time of these droplets
is an important factor in combustion chamber and sprayer design
. Therefore , it is an important study to understand the
vaporization / combustion situation of a single fuel droplet in
a high temperature and oxidizing environment with external
flow. Especially , the study of droplet ignition plays an
important role to understand the droplet combustion phenomena.
In a real fuel spray combustor , the combustion of fuel
droplets occure in a convective , high temperature , oxidizing
environment and the relative motion of neighboring air turns
the problems into two dimensional or more . Due to the complex
chemical reaction and fluid interaction with combustion , the
droplet combustion becomes an extremely difficult phenomenon to
solve . This research of simple ignition model is to understand
the effects of the fuel droplets and of the external
environment on the ignition delay . Threeply - period concept
is introduced to interpret the dominant factors that govern the
ignition process . Numerical technique is applied to get an
insight of transient behavior of a fuel droplet to ignition . A
special hybird numerical scheme ICED-ALE is used to circumvent
the difficulties arising from the rapid transition of ignition
and regression offuel droplet . The results indicated the
droplet in smaller dimension is easier to be be ignited in most
cases . But in higher temperature enviroment , the dimension of
fuel droplet affects the delay times less .At enviroment
temperature of 1050 k , the ignition delay time difference
between large and small fuel droplet is 7.7% . Basically , it
saves 34.6% time for fuel droplet ignition in convective
enviroment than one in stagnant which coincides the real
physical situation .
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author2 |
J. M. Char 、S. M. Liang |
author_facet |
J. M. Char 、S. M. Liang Chir-Shyong Lin 林琦雄 |
author |
Chir-Shyong Lin 林琦雄 |
spellingShingle |
Chir-Shyong Lin 林琦雄 The study of droplet ignition in hot convective environment |
author_sort |
Chir-Shyong Lin |
title |
The study of droplet ignition in hot convective environment |
title_short |
The study of droplet ignition in hot convective environment |
title_full |
The study of droplet ignition in hot convective environment |
title_fullStr |
The study of droplet ignition in hot convective environment |
title_full_unstemmed |
The study of droplet ignition in hot convective environment |
title_sort |
study of droplet ignition in hot convective environment |
publishDate |
1993 |
url |
http://ndltd.ncl.edu.tw/handle/41253607093844099092 |
work_keys_str_mv |
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