Turbulent Premixed Combustion in a High-Pressure Environment up to 4.0MPa
高达4.0MPa高压环境下的湍流预混燃烧
基本信息
- 批准号:08455100
- 负责人:
- 金额:$ 2.5万
- 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:1996
- 资助国家:日本
- 起止时间:1996 至 1997
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
This research was aimed to conduct precise observations of the flame structure, to elucidate the relationship between ambient pressure and turbulence scale and intensities, and to explore the effects of ambient pressure on turbulent burning velocities. Turbulent premixed flames for CH_4-air, C_2H_4-air, and C_3H_8-air mixtures were stabilized by a nozzle burner installed in a high-pressure. The following results were obtained.1) Measured turbulence characteristics showed that turbulence intensities increatsed with increasing mean velocities. Nevertheless, at ordinary pressure, the increase was small in the region of small mean velocities because of an extensive dumping of turbulence. At high-pressures, turbulence intensity linearly increased with the mean velocities in the entire range of the mean velocities.2) At high-pressures, flame structure becomes fine and complicated. S_T/S_L increased rapidly with increasing u'/S_L particularly for weak turbulence regions (u'/S_L<l), indicating … More effects the hydrodynamic instability becomes extensive in a high-pressure environment. For CH_4-air flames, S_T/S_L increases with u'/S_L, up to 30 at 3. OMPa for the experimental conditions achieved.3) The rate of the increase in S_T/S_L for C_3H_8-air flames was smaller than that for C_2H_4-air flames. This is because the flame area increase due to the hydrodynamic instability at high pressures was restrained by diffusive-thermal effects because the larger Lewis number of C_3H_8-air mixtures.4) The data for awide range of turbulence intensities showed that the u'/S_L dependence of S_T/S_L for C_2H_4-air flames is almost the same as that for CH_4-air flames. Nevertheless, S_T/S_L for C_3H_8-air flame showed smaller S_T/S_L than in the cases of C_2H_4-air and CH_4-air flames.5) The applicability of existent correlation between S_T/S_L, u'/S_L, aud turbulence Reynolds number, R_L, to high-pressure flames were examined, and it was found that the data of our experiments had a similar tendency to the correlation by Abde1-Gayd but had larger S_T/S_L than their correlation. 1/4 power law of R_L was seen for S_T/S_L in the strong turbulence region (u'/SL>l.0), consistent with the fractal flamelet model of turbulent burning velocity proposed by Gouldin.6) The best general correlation which can express the experimental data for a whole range of u'/SL and pressure was in the for of S_T/S_L* [ (P/P_O) (u'/S_<1L>) ]^n and the exponent n was close to 0.4. Less
这项研究的目的是对火焰结构进行精确观测,阐明环境压力与湍流尺度和强度的关系,并探索环境压力对湍流燃烧速度的影响。用高压喷嘴燃烧器稳定了CH4-空气、C2H4-空气和C3H8-空气混合物的湍流预混火焰。结果表明:1)测量的湍流特性表明,湍流强度随平均速度的增大而增大。然而,在常压下,由于湍流的广泛倾倒,在平均速度较小的区域,增加的幅度很小。在高压下,湍流强度在整个平均速度范围内与平均速度成线性关系。2)高压下,火焰结构变得细小而复杂。S_T/S_L随u‘/S_L增大迅速增大,尤以弱湍流区(u’/S_L<;L)为甚,指示…在高压环境下,流体动力不稳定性的影响范围更广。对于CH_4-空气火焰,S_T/S_L随u‘/S_L的增大而增大,在3时达到30。在实验条件下获得了OMPA。3)对于C_3H_8-空气火焰,S_T/S_L的增加幅度小于C_2H_4-空气火焰。这是因为C_3H_8-空气混合物的刘易斯数较大,从而抑制了高压下流体动力不稳定性引起的火焰面积的增大。4)大范围的湍流强度数据表明,对于C_2H_4-空气火焰,S_T/S_L与甲烷-空气火焰的u‘/S_L关系基本相同。然而,对于C_3H_8-空气火焰,S_T/S_L比C_2H_4-空气和CH_4-空气火焰的S_T/S_L小。5)考察了S_T/S_L,u‘/S_L和湍流雷诺数R_L之间的现有关联式对高压火焰的适用性,发现我们的实验数据与Abde1-Gayd的关联式的趋势相似,但比它们的关联式大。在强湍流区(u‘/SL>;1.0),S_T/S_L的R_L符合1/4幂规律,与Gouldin提出的湍流燃烧速度的分形火焰面模型一致。6)S_T/S_L*[(P/P_O)(u’/S_<;1L>;)]^n的指数n接近0.4,能较好地描述u‘/SL与压力的整个实验数据。较少
项目成果
期刊论文数量(10)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Hideaki, Kobayashi: "Turbulence Measurements and Observations of Turbulent Premixed Flames at Elevated Pressures up to 3.0MPa" Combust.Flame. 108. 104-117 (1997)
Hideaki, Kobayashi:“压力高达 3.0MPa 时湍流预混火焰的湍流测量和观察”Combust.Flame。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Hideaki Kobayashi: "Experimental Study on General Correlation of Turbulent Burning Velocity at High Pressure" 27th Symp. (Int.) on Combust. (submitted). (1998)
小林秀明:《高压湍流燃烧速度一般相关性的实验研究》第 27 期 Symp.
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Hideaki, Kobayashi: "Burning Velocity of Turbulent Premixed Flames in a High-Pressure Environment" 26th Symp.(Int.)on Combust. 389-396 (1996)
Hideaki, Kobayashi:“高压环境中湍流预混火焰的燃烧速度”第 26 届 Symp.(Int.) 燃烧。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Hideaki, Kobayashi: "Experimental Study on General Corre lation of Turbulent Burning Velocity at High Pressure" 27th Symp.(Int.)on Combust. Submitted. (1998)
Hideaki, Kobayashi:“高压下湍流燃烧速度一般相关性的实验研究”第 27 届 Symp.(Int.) 燃烧。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Hideaki Kobayashi: "Turbulence Measurements and Observations of Turbulent Premixed Flames at Elevated Pressures up to 3.0 MPa" Combust.Flame. Vol.108. 104-117 (1997)
Hideaki Kobayashi:“压力高达 3.0 MPa 时湍流预混火焰的湍流测量和观察”Combust.Flame。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
{{
item.title }}
{{ item.translation_title }}
- DOI:
{{ item.doi }} - 发表时间:
{{ item.publish_year }} - 期刊:
- 影响因子:{{ item.factor }}
- 作者:
{{ item.authors }} - 通讯作者:
{{ item.author }}
数据更新时间:{{ journalArticles.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ monograph.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ sciAawards.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ conferencePapers.updateTime }}
{{ item.title }}
- 作者:
{{ item.author }}
数据更新时间:{{ patent.updateTime }}
KOBAYASHI Hideaki其他文献
KOBAYASHI Hideaki的其他文献
{{
item.title }}
{{ item.translation_title }}
- DOI:
{{ item.doi }} - 发表时间:
{{ item.publish_year }} - 期刊:
- 影响因子:{{ item.factor }}
- 作者:
{{ item.authors }} - 通讯作者:
{{ item.author }}
{{ truncateString('KOBAYASHI Hideaki', 18)}}的其他基金
Spectroscopic development of laser-induced fluorescence method using higher energy band excitation for rocket combustion diagnostics
利用高能带激发进行火箭燃烧诊断的激光诱导荧光方法的光谱发展
- 批准号:
15K14244 - 财政年份:2015
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Challenging Exploratory Research
Turbulent combustion mechanism and emission characteristics of next-generation C4-biofuel isomers in a high-pressure and high-temperature environment
高压高温环境下下一代C4生物燃料异构体湍流燃烧机理及排放特性
- 批准号:
26289043 - 财政年份:2014
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Flame structure and flame stabilization mechanism of oxygen jet diffusion flame in a high-pressure environment
高压环境下氧气射流扩散火焰的火焰结构及火焰稳定机制
- 批准号:
24656133 - 财政年份:2012
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Challenging Exploratory Research
Turbulent combustion mechanism of isomer bio-fuels in a high-pressure, high-temperature environment
异构生物燃料在高压高温环境下的湍流燃烧机理
- 批准号:
23360090 - 财政年份:2011
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
On the mechanism of turbulent premixed combustion in a porous pebble bed at high pressure and high temperature
多孔球石床高压高温湍流预混燃烧机理研究
- 批准号:
22656052 - 财政年份:2010
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Challenging Exploratory Research
A Study of Turbulent Combustion Mechanism in a High-Pressure, High-temperature and High Water-vapor Environment
高压高温高水汽环境下湍流燃烧机理研究
- 批准号:
17360090 - 财政年份:2005
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
A Study of Turbulent Combustion Mechanism in a High Temperature, High-Pressure, and Low-Oxygen Environment
高温高压低氧环境下湍流燃烧机理研究
- 批准号:
15360105 - 财政年份:2003
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Elucidation and Modeling of Turbulent Premixed Combustion Phenomena in a High-Pressure and High-Temperature Environment
高压高温环境中湍流预混燃烧现象的阐明和建模
- 批准号:
12450080 - 财政年份:2000
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Development of a Simultaneous Measurement Method of Velocity, Temperature, and Concentration using a Diode Laser in a Supersonic Combustion Flow
超音速燃烧流中使用二极管激光器同时测量速度、温度和浓度的方法的开发
- 批准号:
11555254 - 财政年份:1999
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B).
Investigation and Application of Fundamental Phenomena of Turbulent Premixed Combustion in a High-Pressure Environment
高压环境下湍流预混燃烧基本现象的研究与应用
- 批准号:
10450079 - 财政年份:1998
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
相似海外基金
A study on numerical simulation of turbulent combustion inside the combustor of an aircraft engine
航空发动机燃烧室内湍流燃烧数值模拟研究
- 批准号:
23KJ0035 - 财政年份:2023
- 资助金额:
$ 2.5万 - 项目类别:
Grant-in-Aid for JSPS Fellows
High-fidelity simulations of turbulent combustion relevant to gas turbines and compression ignition engines
与燃气轮机和压燃式发动机相关的湍流燃烧的高保真模拟
- 批准号:
RGPIN-2019-04309 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual
Turbulent combustion modelling for conditions relevant to industrial applications
工业应用相关条件的湍流燃烧建模
- 批准号:
RGPIN-2018-03965 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual
CAREER: Efficient Uncertainty Quantification in Turbulent Combustion Simulations: Theory, Algorithms, and Computations
职业:湍流燃烧模拟中的高效不确定性量化:理论、算法和计算
- 批准号:
2143625 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Continuing Grant
EAGER: Experimental investigation of physical-space scalar structure and unresolved mixing to improve large-eddy simulation of turbulent combustion
EAGER:物理空间标量结构和未解决的混合的实验研究,以改进湍流燃烧的大涡模拟
- 批准号:
2208136 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Standard Grant
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual
Adaptive Physics-informed Machine Learning Strategies for Turbulent Combustion Modeling
用于湍流燃烧建模的自适应物理学机器学习策略
- 批准号:
2201297 - 财政年份:2022
- 资助金额:
$ 2.5万 - 项目类别:
Standard Grant
High-fidelity simulations of turbulent combustion relevant to gas turbines and compression ignition engines
与燃气轮机和压燃式发动机相关的湍流燃烧的高保真模拟
- 批准号:
RGPIN-2019-04309 - 财政年份:2021
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual
Turbulent combustion modelling for conditions relevant to industrial applications
工业应用相关条件的湍流燃烧建模
- 批准号:
RGPIN-2018-03965 - 财政年份:2021
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2021
- 资助金额:
$ 2.5万 - 项目类别:
Discovery Grants Program - Individual














{{item.name}}会员




