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基于欧拉-拉格朗日模型的内燃机燃油喷雾数值模拟 被引量:4
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作者 李亮 解茂昭 贾明 《燃烧科学与技术》 EI CAS CSCD 北大核心 2019年第4期317-323,共7页
目前,关于内燃机燃油喷雾的研究通常采用拉格朗日模型,欧拉模型则相对较少.本文利用构建的欧拉-拉格朗日模型对ECN喷雾实验进行数值模拟研究.结果显示,在150MPa喷射压力下,喷嘴附近存在明显的连续欧拉液相.然而,在液核的下游,离散相液... 目前,关于内燃机燃油喷雾的研究通常采用拉格朗日模型,欧拉模型则相对较少.本文利用构建的欧拉-拉格朗日模型对ECN喷雾实验进行数值模拟研究.结果显示,在150MPa喷射压力下,喷嘴附近存在明显的连续欧拉液相.然而,在液核的下游,离散相液滴的破碎、碰撞、融合及聚集等均对界面面积密度、粒子直径的分布产生明显影响.由定量分析可知,在LES湍流模型下,除轴距6mm附近的狭窄区间燃料体积分数存在较大偏差外,其对整个喷雾的空间分布以及粒径分布均实现了很好的预测. 展开更多
关键词 欧拉-拉格朗日 燃料喷雾 LES 界面面积密度 多相流
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环境压力对超临界流体喷雾特性影响的数值分析 被引量:5
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作者 韦武 解茂昭 贾明 《内燃机学报》 EI CAS CSCD 北大核心 2018年第3期237-244,共8页
基于大涡模拟方法对超临界喷射进行数值分析,使用真实气体状态方程SRK计算流体的热物性和输运特性.研究对象是定容弹内低温液氮超临界喷射,假定初始入口条件不变,重点考察了不同环境压力对超临界喷雾特性的影响.结果表明:由于射流流体... 基于大涡模拟方法对超临界喷射进行数值分析,使用真实气体状态方程SRK计算流体的热物性和输运特性.研究对象是定容弹内低温液氮超临界喷射,假定初始入口条件不变,重点考察了不同环境压力对超临界喷雾特性的影响.结果表明:由于射流流体与周围流体之间存在较大密度比,射流表面形成显著的密度分层,并起到限制射流流体向径向扩展的作用.随着环境压力的提高,由于射流和周围环境的密度比降低,射流表面不稳定增加,比较容易形成不稳定涡,从而更有利于射流与周围气体的混合,因而液核长度也比较短,表明随着压力的增大,射流与周围气体的混合效果更好.进一步分析发现,环境压力对热物性和输运特性的影响较大,而对湍动能和速度场的影响不大. 展开更多
关键词 超临界 大涡模拟 喷雾 状态方程
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有序堆积床内预混气体燃烧特性实验研究 被引量:2
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作者 岳猛 解茂昭 +1 位作者 史俊瑞 刘宏升 《热科学与技术》 CAS CSCD 北大核心 2021年第1期48-53,共6页
为研究预混气体在多孔介质燃烧器中的火焰燃烧特性,设计了一种新型多孔介质燃烧器,其中多孔介质区域由氧化铝圆柱体有序堆积而成。分别研究了当量比和入口速度对甲烷/空气预混气体在多孔介质燃烧器中的火焰温度分布、火焰最高温度以及... 为研究预混气体在多孔介质燃烧器中的火焰燃烧特性,设计了一种新型多孔介质燃烧器,其中多孔介质区域由氧化铝圆柱体有序堆积而成。分别研究了当量比和入口速度对甲烷/空气预混气体在多孔介质燃烧器中的火焰温度分布、火焰最高温度以及火焰传播速度的影响。结果表明:在当量比0.162~0.324、入口速度0.287~0.860 m/s的实验工况下火焰均可以稳定向前传播,并且都发生了超绝热燃烧;当量比越大,入口速度越大,火焰最高温度越高;当入口速度为0.430 m/s时,贫可燃极限的当量比可以扩展到0.162;火焰传播速度随着入口速度的增加和当量比的减小而增大,其数量级为0.100 mm/s,属于一种十分典型的低速过滤燃烧。 展开更多
关键词 多孔介质 预混燃烧 火焰温度 火焰传播速度
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Large eddy simulation and proper orthogonal decomposition analysis of turbulent flows in a direct injection spark ignition engine:Cyclic variation and effect of valve lift 被引量:11
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作者 QIN WenJin xie maozhao +2 位作者 JIA Ming WANG TianYou LIU DaMing 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第3期489-504,共16页
Large eddy simulation(LES)is used to calculate the in-cylinder turbulent flow field in a direct injection spark ignition(DISI)engine.The computations are carried out for three different maximum valve lifts(MVL)and thr... Large eddy simulation(LES)is used to calculate the in-cylinder turbulent flow field in a direct injection spark ignition(DISI)engine.The computations are carried out for three different maximum valve lifts(MVL)and throughout 100 consecutive engine cycles.The simulated results as well as corresponding particle image velocimetry(PIV)measurement database are analyzed by the proper orthogonal decomposition(POD)method.Through a new developed POD quadruple decomposition the instantaneous in-cylinder flow fields are decomposed into four parts,named mean field,coherent field,transition field and turbulent field,respectively.Then the in-cylinder turbulent flow characteristics and cycle-to-cycle variations(CCV)are studied separately upon the four part flow fields.Results indicate that each part exhibits its specific characteristics and has close connection with others.The mean part contains more than 50%of the total kinetic energy and the energy cascade phenomenon occurs among the four part fields;the coherent field part possesses the highest CCV level which dominates CCV of the bulk flow.In addition,it is observed that a change in MVL affects significantly the in-cylinder flow behavior including CCV,especially for the coherent part.Furthermore,the POD analysis demonstrates that at least 25 sample cycles for the mean velocity and 50 sample cycles for the RMS velocity are necessary for obtaining converged and correct results in CCV. 展开更多
关键词 火花点火发动机 正交分解 大涡模拟 湍流流场 气门升程 直接喷射 循环 缸内流场
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Experimental study on combustion characteristics of Chinese RP-3 kerosene 被引量:9
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作者 Ma Hongan xie maozhao +1 位作者 Zeng Wen Chen Baodong 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2016年第2期375-385,共11页
In order to illustrate the combustion characteristics of RP-3 kerosene which is widely used in Chinese aero-engines, the combustion characteristics of RP-3 kerosene were experimentally inves- tigated in a constant vol... In order to illustrate the combustion characteristics of RP-3 kerosene which is widely used in Chinese aero-engines, the combustion characteristics of RP-3 kerosene were experimentally inves- tigated in a constant volume combustion chamber. The experiments were performed at four different pressures of 0.1 MPa, 0.3 MPa, 0.5 MPa and 0.7 MPa, and three different temperatures of 390 K, 420 K and 450 K, and over the equivalence ratio range of 0.6-1.6. Furthermore, the laminar combus- tion speeds of a surrogate fuel for RP-3 kerosene were simulated under certain conditions. The results show that increasing the initial temperature or decreasing the initial pressure causes an increase in the laminar combustion speed of RP-3 kerosene. With the equivalence ratio increasing from 0.6 to 1.6, the laminar combustion speed increases initially and then decreases gradually. The highest laminar combustion speed is measured under fuel rich condition (the equivalence ratio is 1.2). At the same time, the Markstein length shows the same changing trend as the laminar com- bustion speed with modification of the initial pressure. Increasing the initial pressure will increase the instability of the flame front, which is established by decreased Markstein length. However, different from the effects of the initial temperature and equivalence ratio on the laminar combustion speed, increasing the equivalence ratio will lead to a decrease in the Markstein length and the stability of the flame front, and the effect of the initial temperature on the Markstein length is unclear. Further- more, the simulated laminar combustion speeds of the surrogate fuel agree with the corresponding experimental datas of RP-3 kerosene within ~10% deviation under certain conditions. 展开更多
关键词 Combustion mechanism Combustion stability Laminar combustion speed Markstein length RP-3 kerosene
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Numerical Investigation on Porous Media Quenching Behaviors of Premixed Deflagrating Flame using RANS/LES Model 被引量:4
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作者 WEN Xiaoping SU Tengfei +3 位作者 LIU Zhigang xie maozhao WANG Fahui LIU Zhichao 《Journal of Thermal Science》 SCIE EI CAS CSCD 2019年第4期780-788,共9页
To understand the mechanism of premixed flame quenching by porous media,a zonal hybrid RANS/LES model was employed,in which the LES flow solver was used to resolve the large turbulent structures within the non-porous ... To understand the mechanism of premixed flame quenching by porous media,a zonal hybrid RANS/LES model was employed,in which the LES flow solver was used to resolve the large turbulent structures within the non-porous region,while RANS was applied to porous media zone.The predicted results were compared with previous experimental data.And it was evident that the premixed flame propagation rates and structure as well as quenching behaviors were reproduced by this numerical approach with a better accuracy.Due to the inherently higher heat transfer coefficients between the solid and gas phases in porous media,the gas phase temperature has been decreased rapidly.However,upstream obstacles can cause the flame propagating faster and thus reduce the axial gas temperature gradients,resulting in the invalidity of the operation of premixed flame quenching.By comparison with the case without upstream obstacle,the values of reaction rate attained in the case with three pairs of obstacles are higher,which makes a positive impact on the flame passing through the porous medium.In addition,the porous media with greater pore density has an excellent flame quenching property mainly owing to both the larger volumetric heat transfer and higher quenching temperature. 展开更多
关键词 RANS/LES MODEL porous media QUENCHING FLAME propagation
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跨/超临界下真实燃料喷射模型的构建及模拟
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作者 马杰 刘宏升 +1 位作者 解茂昭 李亮 《工程热物理学报》 EI CAS CSCD 北大核心 2022年第11期3103-3109,共7页
本研究以开源软件OpenFOAM为平台,基于真实流体状态方程与高压修正的热动力学输运模型,通过修改PIMPLE算法,构建出一个新的多组分跨/超临界射流模型,并通过一维对流问题考察了模型有效性;在此基础上,结合RANS模型对跨/超临界下正庚烷/... 本研究以开源软件OpenFOAM为平台,基于真实流体状态方程与高压修正的热动力学输运模型,通过修改PIMPLE算法,构建出一个新的多组分跨/超临界射流模型,并通过一维对流问题考察了模型有效性;在此基础上,结合RANS模型对跨/超临界下正庚烷/氮气的喷射和混合过程进行了数值模拟。结果表明:在跨临界工况下,尤其在伪沸点附近,射流对温度的变化非常敏感,伪沸腾现象维持着气液界面出现连续的高密度梯度区,其对跨临界射流的演变起着决定性作用;在超临界工况下,伪沸腾现象的消失导致射流与周围流体的混合更加充分。 展开更多
关键词 跨/超临界工况 伪沸腾 真实流体状态方程 热动力学模型
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Numerical study on the compression ignition of a porous medium engine 被引量:2
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作者 ZHAO ZhiGuo xie maozhao 《Science China(Technological Sciences)》 SCIE EI CAS 2008年第3期277-287,共11页
Homogeneous and stable combustion can be realized in a porous medium (PM) engine where a chemically inert PM is mounted in the combustion chamber. To understand the mechanism of the PM engine, we simulated the working... Homogeneous and stable combustion can be realized in a porous medium (PM) engine where a chemically inert PM is mounted in the combustion chamber. To understand the mechanism of the PM engine, we simulated the working process of a PM engine fueled with natural gas (CH4) using an improved version of KIVA-3V and investigated the effects of the initial PM temperature, the PM structure as well as the fuel injection timing on the compression ignition of the engine. The im- proved version of KIVA-3V was verified by simulating the experiment of Zhdanok et al. for the superadiabatic combustion of CH4-air mixtures under filtration in a packed bed. The numerical results are in good agreement with experimental data for the speed of combustion wave. Computational results for the PM engine show that the initial PM temperature is the key factor in guaranteeing the onset of com- pression ignition of the PM engine at a given compression ratio. The PM structure affects greatly both convective heat transfer between the gas and solid phase in the PM and the dispersion effect of the PM. Pore diameter of the PM is a crucial factor in determining the realization of combustion in the PM engine. Over-late fuel injec- tion timing (near TDC) cannot assure a compression ignition of the PM engine. 展开更多
关键词 PM ENGINE CH4 KIVA-3V compression IGNITION NUMERICAL simulation
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液体推进燃料着火特性影响因子与活化能分析
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作者 马洪安 解茂昭 +1 位作者 曾文 陈保东 《航空动力学报》 EI CAS CSCD 北大核心 2018年第10期2385-2391,共7页
采用反射激波管实验台,对液体推进燃料RP-3着火特性进行了实验研究,并分析了燃料的表观活化能。采用了最大OH-光谱斜率倒推法确定着火终点,判定得到了液体推进燃料的着火特性,并对不同燃料体积分数下的着火延迟进行了归一化处理。结果表... 采用反射激波管实验台,对液体推进燃料RP-3着火特性进行了实验研究,并分析了燃料的表观活化能。采用了最大OH-光谱斜率倒推法确定着火终点,判定得到了液体推进燃料的着火特性,并对不同燃料体积分数下的着火延迟进行了归一化处理。结果表明:推进燃料的表观活化能差异不大,约为154~171kJ/mol;对各参数影响因子进行分析,着火延迟时间与当量比成正比关系,与燃料体积分数和混合气压力成反比关系;与JP-10比较发现,着火特性数据受燃料体积分数、当量比的影响因子几乎相等。 展开更多
关键词 液体推进燃料 激波管 当量比 燃料体积分数 表观活化能
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Numerical study on turbulent two-phase flow in porous medium combustion chamber
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作者 DONG Ming xie maozhao LI SuFen 《Science China(Technological Sciences)》 SCIE EI CAS 2009年第6期1511-1520,共10页
To understand the working mechanism of the porous medium(PM)internal combustion engine,effects of a porous medium heat regenerator inserted into a combustion chamber on the turbulent flow char-acteristics and fuel-air... To understand the working mechanism of the porous medium(PM)internal combustion engine,effects of a porous medium heat regenerator inserted into a combustion chamber on the turbulent flow char-acteristics and fuel-air mixture formation are studied by numerical simulation.The cylindrical chamber has a constant volume,in which a disk-shaped PM insert is fixed.A simplified model for the random structure of the PM is presented,in which the PM is represented by an assembly of a great number of randomly distributed solid units.To simulate flows in the PM a microscopic approach is employed,in which computations are performed on a pore-scale mesh and based on the standard k-ε turbulence model.A spray model,in which the effects of drop breakup,collision and coalescence are taken into account,is introduced to describe spray/wall interactions.Numerical computations are performed for the turbulent flows induced by a fuel spray outside and inside of the PM with different structure parameters.Calculation results show that the spray/PM interaction has substantial and positive influ-ences on the fuel-air mixture formation and homogenization in the combustion chamber,which could be very advantageous in engine applications. 展开更多
关键词 POROUS media TURBULENCE fuel SPRAY numerical simulation spray/PM interaction
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