非绝热湍流反应流中烟尘演化的原位自适应流形

IF 5.2 2区 工程技术 Q2 ENERGY & FUELS
Matthew X. Yao, Israel J. Bonilla, S. Trevor Fush, Michael E. Mueller
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引用次数: 0

摘要

为了减少紊流反应流模拟的计算成本,通常采用基于流管的燃烧模型。在这些模型中,热化学状态被投射到一个低维流形上,它可以与流求解器分开计算。传统上,该模型涉及一组流形方程的解的预制式,这些解是先验获得的。由于辐射热损失的重要性,烟尘和排放物的包含引入了额外的物理。为了考虑热损失的影响,表尺寸的数量必然增加。因此,这些表可能会占用大量内存,并且包含许多在模拟过程中甚至可能无法访问的热化学状态。为了减少这种内存负担,最近提出了原位自适应流形(ISAM)的概念。在这个框架内,必要的流形解被实时计算并存储,以便使用原位自适应制表(ISAT)进行查找。在这项工作中,ISAM与基于混合矩量法(HMOM)模型的煤烟模型相耦合。为了考虑热损失,流形方程中增加了热损失参数H的方程,该方程也在LES流求解器中演化。流形方程是基于准稳定假设而制定的,模型热损失源项乘以常数Ω来考虑气相和煤烟辐射热损失的变化幅度。在运行期间,来自LES的H场必须与ISAM匹配以产生正确的热化学状态。为了保证LES和ISAM热损失参数的一致性,建立了求解Ω的迭代过程。该模型在桑迪亚煤烟火焰上进行了验证。与传统的预计算表相比,ISAM在计算成本小幅增加的情况下提供了显著的内存节省,这对匹配H的迭代方法的初始猜测很敏感。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
In-Situ Adaptive Manifolds for soot evolution in non-adiabatic turbulent reacting flows
To reduce the computational cost of simulations of turbulent reacting flows, manifold-based combustion models are often employed. In these models, the thermochemical state is projected onto a low-dimensional manifold, which can be computed separately from the flow solver. Traditionally, the model involves the pretabulation of solutions to a set of manifold equations, which are obtained a priori. The inclusion of soot and emissions introduces additional physics due to the importance of radiation heat losses. To account for the effects of heat loss, the number of table dimensions necessarily increases. Consequently, these tables can become very memory intensive and include many thermochemical states that may not even be accessed during the simulation. To reduce this memory burden, the concept of In-Situ Adaptive Manifolds (ISAM) has recently been proposed. Within this framework, necessary manifold solutions are computed on-the-fly and stored for lookup using In-Situ Adaptive Tabulation (ISAT). In this work, ISAM is coupled to a soot model based on the Hybrid Method of Moments (HMOM) model. To incorporate heat losses, the manifold equations are augmented with an equation for the heat loss parameter H, which is also evolved in the LES flow solver. The manifold equations are formulated based on a quasi-steady assumption, and a model heat loss source term is multiplied by a constant Ω to account for varying magnitudes of radiation heat losses from the gas-phase and soot. During runtime, the H field from the LES must be matched by ISAM to produce the correct thermochemical state. An iterative procedure is developed to obtain the correct value of Ω to ensure consistency of the heat loss parameter between LES and ISAM. The model is demonstrated on the Sandia Sooting Flame. Compared to traditional precomputed tables, ISAM is shown to provide significant memory savings at a minor increase in the computational cost, which is sensitive to the initial guesses for the iterative approach for matching H.
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来源期刊
Proceedings of the Combustion Institute
Proceedings of the Combustion Institute 工程技术-工程:化工
CiteScore
7.00
自引率
0.00%
发文量
420
审稿时长
3.0 months
期刊介绍: The Proceedings of the Combustion Institute contains forefront contributions in fundamentals and applications of combustion science. For more than 50 years, the Combustion Institute has served as the peak international society for dissemination of scientific and technical research in the combustion field. In addition to author submissions, the Proceedings of the Combustion Institute includes the Institute''s prestigious invited strategic and topical reviews that represent indispensable resources for emergent research in the field. All papers are subjected to rigorous peer review. Research papers and invited topical reviews; Reaction Kinetics; Soot, PAH, and other large molecules; Diagnostics; Laminar Flames; Turbulent Flames; Heterogeneous Combustion; Spray and Droplet Combustion; Detonations, Explosions & Supersonic Combustion; Fire Research; Stationary Combustion Systems; IC Engine and Gas Turbine Combustion; New Technology Concepts The electronic version of Proceedings of the Combustion Institute contains supplemental material such as reaction mechanisms, illustrating movies, and other data.
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