Study on the instability of near-critical-mixing surface jet and turbulent atomization for the purpose of high-pressure spray combustion control
Study on the instability of near-critical-mixing surface jet and turbulent atomization for the purpose of high-pressure spray combustion control
批准号:
14350510
负责人:
UMEMURA Akira
金额:
$8.51万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
2002
资助国家:
日本
项目状态:
已结题
起止时间:
2002 至 2005
中文摘要
由于喷雾在各个领域的应用,到目前为止已经进行了无数次的调查。然而,湍流雾化的基本物理原理仍然不为人所知。主要原因是这些现象细微而迅速地观察到其细节,因此很难产生对揭示湍流雾化机理有用的概念。在本研究中,我们提出了一种独特的方法来克服这一困难,利用微重力环境,这是一种新的实验手段,在传统的雾化研究中从未使用过。实验的一个关键点是,我们实现了一种液体射流,其表面接近SF6液体的临界混合状态,并在室温下以远超过液体临界压力的高压释放到静止的氮气中。由于近临界混合表面射流具有极小的表面张力和高的蒸汽密度,气体的韦伯数为…更重要的是,即使液体射流以低速喷出,射流也可能具有很大的价值。因此,我们可以使用低速、近临界混合的表面射流来研究湍流雾化过程中的不稳定现象。因此,本实验为同时解决(1)湍流雾化机理和(2)高压射流不稳定特性这两个问题提供了方法论。我们发展了基于微重力实验新发现的理论和数值模型。使传统的雾化理论发生了突破性的变化。特别是,我们发现,由射流解体产生的毛细管波变成了不稳定波,从而导致了随后的解体。我们还可以提出一种构建喷雾燃烧模拟器的策略,该模拟器包括雾化和液滴间火焰传播过程,而所有现有的模拟器都未能包括这些过程。较少
英文摘要
Since spray is used in a variety of fields, a numberless of investigation has been conducted by far. However, the underlying physics of turbulent atomization is still veiled. The main reason is that the phenomena are so fine and rapid to observe its details so that it was very hard to produce those concepts which are useful to reveal the turbulent atomization mechanism. In the present study, we made a unique approach to overcome this difficulty by utilizing the microgravity environment, a new experimental means which has been never used in the conventional style of atomization study. A key point of the experiment is that we realize a liquid jet which has its surface close to a critical mixing state for a SF6 liquid issued into an otherwise quiescent nitrogen gas at a high pressure far exceeding the critical pressure of the liquid and at a room temperature. Since the near-critical-mixing surface jet has a vanishingly small surface tension and a high vapor density, the gas Weber number o … More f the jet may take a large value even when the liquid jet is issued at a low speed. Therefore, we can use a low-speed, near-critical-mixing surface jet to examine the unstable phenomena involved in turbulent atomization processes. Thus, this experiment provides the methodology simultaneously to resolve the two problems of (1) turbulent atomization mechanism and (2) the characteristic properties of the high pressure jet instability.We developed the theories and numerical models which bases the new findings from the microgravity experiments. And lead to a breakthrough change in the conventional atomization theories. In particular, we found that the capillary waves which is generated by the disintegration of the jet turns into unstable waves which leads to the subsequent disintegration. We could also figure out a strategy to construct a spray combustion simulator which includes the processes of atomization and inter-droplet flame propagation which all existing simulator have failed to incorporate. Less
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Marangoni effect on droplet approached by a diffusion flame
马兰戈尼效应对扩散火焰接近的液滴的影响
DOI:
--
发表时间:
2006
期刊:
Combustion Theory and Modelling, 10
影响因子:
--
作者:
[Umemura, A., Nagase, Y., Ando, T.]
通讯作者:
T.
微小重力環境を利用した液体ジェットの不安定性の研究
微重力环境下液体射流不稳定性研究
DOI:
--
发表时间:
2004
期刊:
日本マイログラビティ応用学会誌 21
影响因子:
--
作者:
[梅村章]
通讯作者:
梅村章
ウォーターミストのダウンバーストとプール火炎基部との干渉に関する数値的研究
水雾下击暴流与水池火焰基底相互作用的数值研究
DOI:
--
发表时间:
2004
期刊:
日本燃焼学会誌 第46巻137号
影响因子:
--
作者:
[村松憲志郎, 梅村章]
通讯作者:
梅村章
New approach to elucidation of turbulent atomization mechanism by use of near-critical mixing surface jet in microgravity
利用微重力下近临界混合表面射流阐明湍流雾化机制的新方法
DOI:
--
发表时间:
2006
期刊:
Proceedings of The Combustion Institute Submitted
影响因子:
--
作者:
[Umemura, A., Kitagawa, T., Ihara, A.]
通讯作者:
A.
微小重力環境を利用して微粒化機構を探る
利用微重力环境探索雾化机制
DOI:
--
发表时间:
2005
期刊:
日本液体微粒化学会誌 (印刷中)
影响因子:
--
作者:
[牧田 雅之, Misao Nagahata, 梅村章]
通讯作者:
梅村章
共 20 条
Development of a new conceptual atomization simulator for liquid rocket engines
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批准号:21246125
-
项目类别:Grant-in-Aid for Scientific Research (A)
-
资助金额:$27.29万
-
财政年份:2009
-
负责人:UMEMURA Akira
-
依托单位:
Development of a genuine numerical simulator for spray combustion based on new concepts derived from microgravity experiments
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批准号:18360404
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$9.2万
-
财政年份:2006
-
负责人:UMEMURA Akira
-
依托单位:
Study on the Atomization Gasification, Mixing and Combustuin Processes of Liquid fuel Jets in Supercritical Enironments
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批准号:11650219
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.66万
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财政年份:1999
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负责人:UMEMURA Akira
-
依托单位:
Study on Themo-Fluiddynamic Coupling involved in Supercritical Droplet Combusion and Vaporization/Combustion Characteristics Prediction
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批准号:07650234
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.22万
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财政年份:1995
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负责人:UMEMURA Akira
-
依托单位:
Basic study for developing supercritical spray combustion simulator
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批准号:04650173
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.28万
-
财政年份:1992
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负责人:UMEMURA Akira
-
依托单位:
Supercritical Liquid Fuel Combustion Mechanism
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批准号:01550163
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.22万
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财政年份:1989
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负责人:UMEMURA Akira
-
依托单位: