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采用稳态的和非稳态的火焰面模型同时对一个湍流甲烷射流扩散火焰进行了数值模拟,比较了两者对湍流平均火焰结构、活性自由基和污染物(氮氧化物)排放的模拟效果。速度场采用κ-ε模型计算,守恒标量混合物分数的分布通过其概率密度函数(PDF)输运方程的求解得到。稳态的火焰面结构由查询火焰面数据库得到,而非稳态的火焰面结构由火焰面方程和流场方程耦合求解来计算。采用详细的GRI—Mech 3.0机理描述甲烷的氧化和氮氧化物的形成。数值模拟结果和实验数据作了广泛的对比,验证了火焰面模型对湍流扩散燃烧的定量模拟能力。 相似文献
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为了考察湍流燃烧过程中的辐射热影响,数值模拟了Sanida火焰D,其中湍流流动采用多时间尺度(MTS)k-ε湍流模型模拟,燃烧过程采用概率密度函数(PDF)方法和拉格朗日火焰面模型(LFM)以及详细化学反应机理GRI3.0联合的方法模拟,辐射换热采用有限体积(FVM)联合关联k分布模型模拟。计算结果和实验数据的比较发现虽然相对于燃烧热,辐射热是一个小量,但是考虑了辐射热影响以后,模拟结果大有改进。针对该现象,我们给出的解释是由于在湍流燃烧过程中,湍流过程,燃烧过程以及辐射换热过程三者是强耦合的,湍流作用很可能会将辐射换热作用放大,因此,对于燃烧过程的详细数值模拟,建议考虑辐射换热的影响。 相似文献
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在开源计算流体软件OpenFOAM环境下,将基于欧拉方法的Σ-Y喷雾模型与非稳态火焰面/反应进度变量湍流燃烧模型相耦合,发展用于高温高压环境中液体燃料喷雾湍流燃烧高精度计算模型,分别对非燃烧和燃烧工况下的五种典型参比燃料(Primary Reference Fuel,PRF)的燃油喷射雾化与湍流燃烧过程开展数值研究。结果表明:该新型耦合模型能够准确的预测PRF燃料的喷雾和着火燃烧特性;所开发的重构数值喷雾纹影图像和燃烧OH*图像处理方法能够很好地捕捉到试验的滞燃期、火焰浮起长度及喷雾火焰结构;研究揭示了不同比例的PRF燃料对喷雾及着火燃烧过程的影响特性,为替代燃料在发动机上的高效应用提供了理论指导。 相似文献
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本文利用直接数值模拟方法对均质压燃(HCCI, Homogeneous Charge Compression Ignition)工况下氨氢混合物的着火和燃烧特性进行了研究。结果表明,着火首先从局部孤立区域处发生,随后发展到整个计算区域;最高燃烧温度和热释率随着掺氢比的增加而增加;通过与零维计算结果对比,发现湍流和热分层使得氨氢混合物着火提前。利用直接数值模拟数据计算了反应锋面的位移速度,并据此分析了自着火和火焰传播这两种燃烧模式。发现在低掺氢比的情况下,燃烧模式以自着火为主;而在高掺氢比的情况下,燃烧模式以火焰传播为主。 相似文献
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文章使用基于LES-PDF方法的AECSC两相程序,对模型燃烧室GTMC进行了数值模拟,以此验证AECSC程序对燃烧室模拟的可行性和可信度,并对旋流燃烧室的流动和燃烧特性进行分析.首先,分别用商用软件Fluent 18.1和AECSC程序的LES方法对GTMC的冷态工况进行了模拟.与实验结果相比,程序计算的轴向、径向、切向速度峰值的相对误差在大多数统计点上在20%以内,3个方向速度峰值位置的相对误差基本都在10%以内.同时发现,AECSC程序的计算结果在一定程度上比Fluent的计算结果更接近实验值.文章进一步使用AECSC程序对GTMC的热态工况进行了模拟.在计算结果中,整体的时间平均温度在数值和分布上和实验结果很接近,并很好地再现了实验的"V形"火焰和内外低温回流区,但是高温区出现的位置相比实验结果有些靠前.总体来说,热态结果和实验结果比较吻合,尤其在液雾的模拟方面,计算结果和实验结果相比有着很好的一致性.这说明将LES和PDF相结合的方法在模拟湍流燃烧方面有较强的优势,可以成为未来的研究和发展方向. 相似文献
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Wei Huang Mohamed Pourkashanian Lin Ma Derek B. Ingham Shi Bin Luo Zhen Guo Wang 《显形杂志》2011,14(1):63-74
Abstract
As effective devices to extend the fuel residence time in supersonic flow and prolong the duration time for hypersonic vehicles cruising in the near-space with power, the backward-facing step and the cavity are widely employed in hypersonic airbreathing propulsive systems as flameholders. The two-dimensional coupled implicit RANS equations, the standard k-ε turbulence model, and the finite-rate/eddy-dissipation reaction model have been used to generate the flow field structures in the scramjet combustors with the backward-facing step and the cavity flameholders. The flameholding mechanism in the combustor has been investigated by comparing the flow field in the corner region of the backward-facing step with that around the cavity flameholder. The obtained results show that the numerical simulation results are in good agreement with the experimental data, and the different grid scales make only a slight difference to the numerical results. The vortices formed in the corner region of the backward-facing step, in the cavity and upstream of the fuel injector make a large difference to the enhancement of the mixing between the fuel and the free airstream, and they can prolong the residence time of the mixture and improve the combustion efficiency in the supersonic flow. The size of the recirculation zone in the scramjet combustor partially depends on the distance between the injection and the leading edge of the cavity. Further, the shock waves in the scramjet combustor with the cavity flameholder are much stronger than those that occur in the scramjet combustor with the backward-facing step, and this causes a large increase in the static pressure along the walls of the combustor. 相似文献13.
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Analysis of Two-Phase Cavitating Flow with Two-Fluid Model Using Integrated Boltzmann Equations 下载免费PDF全文
Shuhong Liu Yulin Wu Yu Xu & Hua-Shu Dou 《advances in applied mathematics and mechanics.》2013,5(5):607-638
In the present work, both computational and experimental methods are employed
to study the two-phase flow occurring in a model pump sump. The two-fluid
model of the two-phase flow has been applied to the simulation of the three-dimensional
cavitating flow. The governing equations of the two-phase cavitating flow
are derived from the kinetic theory based on the Boltzmann equation. The isotropic
RNG$k-\epsilon-k_{ca}$ turbulence model of two-phase flows in the form of cavity number instead
of the form of cavity phase volume fraction is developed. The RNG $k-\epsilon-k_{ca}$ turbulence
model, that is the RNG$k-\epsilon$ turbulence model for the liquid phase combined
with the $k_{ca}$model for the cavity phase, is employed to close the governing turbulent
equations of the two-phase flow. The computation of the cavitating flow through a
model pump sump has been carried out with this model in three-dimensional spaces.
The calculated results have been compared with the data of the PIV experiment. Good
qualitative agreement has been achieved which exhibits the reliability of the numerical
simulation model. 相似文献
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DSM-LPDF两相湍流模型及旋流两相流动的模拟 总被引:2,自引:0,他引:2
本文由流体-颗粒速度的拉氏联合概率密度函数(PDF)输运方程出发,用Simonin建议的Langevin模型封闭颗粒所遇到流体瞬时速度的条件期望项,并用Monte Carlo方法直接求解 PDF输运方程,将其和求解流体雷诺应力方程模型的有限差分方法结合,建立了雷诺应力-拉氏PDF(DSM-LPDF,简称DL)两相湍流模型.用此模型模拟了旋流数为0.47的突扩旋流气粒两相流动,并与文献中PDPA实验和用类似于单相流动湍流模型封闭方法的时平均统一二阶矩(USM)模型的预报进行了对比. 相似文献
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颗粒湍流扩散的数值模拟 总被引:3,自引:0,他引:3
1引言颗粒湍流扩散是气固两相流中的一个重要的研究课题,近年来,国外有大量文献报道这方面的工作。因为颗粒的湍流扩散的研究的一个基本问题就是湍流的描述,它一方面可以来检验湍流描述的正确性;另一方面,该问题是气固两相流理论中,特别是颗粒群轨道模型中一个难点。描述湍流大体上可分为两种方法。一是直接数值模拟方法(DNS),J.B.Mclaughlin对管流内颗粒沉降的研究就基于直接数值模拟山,K.D.squires和J.K.Eaton对颗粒扩散的研究也基于DNS[2],DNS一般只适用于低Reynolds数。另一方面,用随机方法来模拟湍流,该… 相似文献
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基于计算流体动力学软件ANSYS CFX,利用非均相流欧拉-欧拉模型耦合RPI(伦斯勒理工大学)沸腾模型开展超汽化冷却结构的过冷沸腾两相流模拟,比较不同翅片结构对超汽化结构换热性能的影响。研究发现在高热流量条件下三角形翅片结构的换热性能优于矩形翅片结构:其中顺流4×3 三角形翅片结构总体换热性能最好;矩形4×3 翅片结构受流速影响较大,由于翅片的阻碍作用使得流速越来越低,换热性能越来越差;逆流4×3 三角形翅片结构由于其翅片间的腔小,并且逆流翅片对主流的破坏使得腔内流体保持着很大的湍度,所以翅片区有很好的换热性能,但由于逆流翅片对流体阻碍作用大,小槽内流体速度越来越低,使得远离翅片区的侧边换热性能逐渐变差。 相似文献
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�� ����ë����������ΰ���������Ҷ���� 《核聚变与等离子体物理》2006,39(1):48-54
Based on the computational fluid dynamic code ANSYS CFX, the inhomogeneous Eulerian- Eulerian multiphase model coupled with RPI (Rensselaer Polytechnic Institute) boiling model is adopted to simulate the subcooled boiling two-phase flow of hypervapotron structure, and the effects of different fin structures on the heat transfer performance of hypervapotron structures are compared. The results show that under high heat flux conditions, the heat transfer performance of the triangular fin structure is better than the rectangular fin structure. Triangular 4×3 to the flow geometry has the best heat transfer performance. Rectangular 4×3 geometry is greatly affected by the flow rate due to the obstruction of the fins making the flow rate to be lower and the heat transfer performance will be getting worse. Triangular 4×3 against the flow geometry make the fluid in the cavity to maintain a large degree of turbulence due to the small cavity between the fins and the adverse effects of counter-flow fins on the mainstream, so the fin area has a good heat transfer performance, but due to the impeding effect of the counter-flow fin on the fluid, the fluid velocity in the slot is getting lower and lower, as the result, the heat transfer performance on the sidewall far away from the fin area is getting worse. 相似文献