On the Mechanism of Rapid Flame Propagation in a Rotating Flow
On the Mechanism of Rapid Flame Propagation in a Rotating Flow
批准号:
03650172
负责人:
ISHIZUKA Satoru
金额:
$1.28万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (C)
财政年份:
1991
资助国家:
日本
项目状态:
已结题
起止时间:
1991 至 1992
中文摘要
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英文摘要
The rapid flame propagation in a rotating flow is explained on the vortex bursting mechanism, in which it is considered that the hot burned gas of low density is forcibly involved into the unburned gas mixture of high density. In the first year, the relation between the flame speed and the rotating gas speed was examined and it was pointed out that quantitatively the theory could not explain the results.In the next year, the pressure distribution across the flame front was exaimed to substantiate the theory in which the pressure ahead of the flame is assumed to be lower than that behind the flame, because the centrifugal force is weak in the hot burned gas of low density, and hence, the pressure on the axis of rotation cannot be decreased much as compared with the ambient pressure, whereas the centrifugal force is strong in the unburned gas of high density, and hence, the pressure on the axis of rotation becomes much lower than the ambient pressure. Resultingly, the pressure behind the flame becomes higher than the pressure ahead of the flame.Using a high-response, micro-diffential manometer and a transient memory, the pressure distribution was measured for the flame propagating in a rotating mixture. For comparison, the pressure distribution was also measured for the flames propagating in a quiescent combustible mixture and in a non-rotating mixture stream. The results show that, as the theory predicts, the predicts, the pressure ahead of the flame is lower than the pressure behind the flame. However, it is shown that the flame apeed is only one half or one third the predicted speed. This is confirmed by the additonal experiments this year. The results obtained in the first year have been published in Progress in Astronautics and Aeronautics, and those in the last year will appear in Combustion Science and Technolgy.
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Satoru ISHIZUKA and Toshisuke HIRANO: "Behavior of Propagating Flame in a Rotating Flowfield" Progress in Astronautics and Aeronautics. Vol.151, AIAA. 284-306 (1993)
Satoru ISHIZUKA 和 Toshisuke HIRANO:“旋转流场中传播火焰的行为”航天与航空进展。
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Satoru ISHIZUKA: "Flame Propagation in a Vortex Flow" Proceedings of the Russian-Japanese Symposium on Combustion, Khabarovsk Polytechnical Institute. 15-20 (1992)
Satoru ISHIZUKA:“涡流中的火焰传播”俄日燃烧研讨会论文集,哈巴罗夫斯克理工学院。
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Satoru ISHIZUKA and Toshisuke HIRANO: "Behavior of Propagating Flame in a Rotating Flowfield" Progress in Astronautics and Aeronautics, AIAA. 151. 284-306 (1993)
Satoru ISHIZUKA 和 Toshisuke HIRANO:“旋转流场中传播火焰的行为”航天与航空进展,AIAA。
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Ishizuka,S.: "VortexーInduced Flame Propagation" Book of Abstracts,XIth International Workshop on Mathematical Methods in Combustion. 58-60 (1991)
Ishizuka, S.:“涡流诱导火焰传播”摘要,第十一届燃烧数学方法国际研讨会 58-60 (1991)。
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Satoru ISHIZUKA: "Vortex-Induced Flame Propagation" Book of Abstracts of the XIth International Workshop on Mathematical Methods in Combustion, Tukuba, July 26-27. 58-60 (1991)
Satoru ISHIZUKA:第 XI 届燃烧数学方法国际研讨会的“涡旋火焰传播”摘要集,图库巴,7 月 26-27 日。
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共 14 条
Realization of a ultra low NOx burner with using continuously varying multi-step combustion and self-recirculation
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批准号:23656150
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项目类别:Grant-in-Aid for Challenging Exploratory Research
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资助金额:$2.41万
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财政年份:2011
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负责人:ISHIZUKA Satoru
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依托单位:
Elucidation of Combustion Induced Vortex Breakdown Phenomena
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批准号:16360106
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$9.09万
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财政年份:2004
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负责人:ISHIZUKA Satoru
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依托单位:
海外基金