Alexandra Baumgart, Matthew X. Yao, Guillaume Blanquart
{"title":"爆炸模拟的表化化学方法","authors":"Alexandra Baumgart, Matthew X. Yao, Guillaume Blanquart","doi":"10.1016/j.combustflame.2024.113878","DOIUrl":null,"url":null,"abstract":"<div><div>Chemistry modeling in detonations typically relies on two broad approaches: simplified models with one- or two-step chemistry, and detailed chemistry. These approaches require choosing between computational efficiency or physical accuracy. To reduce the cost of chemistry while maintaining accurate physics, tabulated chemistry has been used extensively for flames/deflagrations in the low Mach number framework. In the simplest tabulated chemistry model for premixed flames, a progress variable, describing the progress of reactions in the system, is transported in the simulation. This progress variable is then used to look up all other species, transport properties, and thermodynamic variables from a pre-computed table. The present work extends the tabulated chemistry method to detonations. Even in non-reacting compressible flow simulations, the enthalpy and specific heat capacity are required; to describe these thermodynamic variables, the temperature is selected as a second table coordinate. The two table coordinates are able to capture virtually all variations in the progress variable source term. The Zel’dovich–von Neumann–Döring (ZND) model is found to be the most appropriate one-dimensional problem for generation of the table. The ZND tabulation approach is validated for both one-dimensional stable and pulsating and two-dimensional regular and irregular detonations in various <span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span>-<span><math><msub><mrow><mi>O</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span> mixtures. The tabulated chemistry simulations are able to reproduce the detailed chemistry results in terms of propagation speed, cellular structures, and source term statistics. For hydrogen detonations, the computational cost of scalar transport is reduced by a factor of 9 and the cost of the chemistry is reduced by a factor of 17. More substantial computational savings are expected for hydrocarbon fuels.</div><div><strong>Novelty and significance statement</strong></div><div>Detonations are often challenging to simulate due to the significant cost of integrating accurate chemical models. In deflagrations, this cost has been reduced by pre-computing the chemistry and collecting the information into a lookup table to be used at runtime. Although chemistry tabulation has been adapted recently for supersonic combustion, such as in scramjets, the typical assumptions of these approaches do not apply to detonations. We propose a new tabulated chemistry approach, valid for detonations and reproducing critical parameters such as induction zone length and detonation velocity. The key novelty lies in (1) the use of progress variable and temperature as the coordinates for tabulation, and (2) the selection of one-dimensional Zel’dovich–von Neumann–Döring detonations as the relevant physical problem to be tabulated. The new model significantly reduces the cost of simulations.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"272 ","pages":"Article 113878"},"PeriodicalIF":5.9000,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Tabulated chemistry approach for detonation simulations\",\"authors\":\"Alexandra Baumgart, Matthew X. Yao, Guillaume Blanquart\",\"doi\":\"10.1016/j.combustflame.2024.113878\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Chemistry modeling in detonations typically relies on two broad approaches: simplified models with one- or two-step chemistry, and detailed chemistry. These approaches require choosing between computational efficiency or physical accuracy. To reduce the cost of chemistry while maintaining accurate physics, tabulated chemistry has been used extensively for flames/deflagrations in the low Mach number framework. In the simplest tabulated chemistry model for premixed flames, a progress variable, describing the progress of reactions in the system, is transported in the simulation. This progress variable is then used to look up all other species, transport properties, and thermodynamic variables from a pre-computed table. The present work extends the tabulated chemistry method to detonations. Even in non-reacting compressible flow simulations, the enthalpy and specific heat capacity are required; to describe these thermodynamic variables, the temperature is selected as a second table coordinate. The two table coordinates are able to capture virtually all variations in the progress variable source term. The Zel’dovich–von Neumann–Döring (ZND) model is found to be the most appropriate one-dimensional problem for generation of the table. The ZND tabulation approach is validated for both one-dimensional stable and pulsating and two-dimensional regular and irregular detonations in various <span><math><msub><mrow><mi>H</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span>-<span><math><msub><mrow><mi>O</mi></mrow><mrow><mn>2</mn></mrow></msub></math></span> mixtures. The tabulated chemistry simulations are able to reproduce the detailed chemistry results in terms of propagation speed, cellular structures, and source term statistics. For hydrogen detonations, the computational cost of scalar transport is reduced by a factor of 9 and the cost of the chemistry is reduced by a factor of 17. 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引用次数: 0
摘要
爆炸的化学建模通常依赖于两种广泛的方法:采用一步或两步化学的简化模型和详细化学。这些方法需要在计算效率和物理精度之间做出选择。为了在保持精确物理的同时降低化学的成本,表化化学已被广泛用于低马赫数框架下的火焰/爆燃。在最简单的预混合火焰表化化学模型中,在模拟中传递了描述系统中反应过程的进程变量。然后使用这个进度变量从预先计算的表中查找所有其他物种、输运性质和热力学变量。本工作将表化化学方法扩展到爆轰。即使在非反应可压缩流动模拟中,也需要焓和比热容;为了描述这些热力学变量,选择温度作为第二个表坐标。这两个表坐标能够捕获进度变量源项中的几乎所有变化。发现Zel 'dovich-von Neumann-Döring (ZND)模型是生成表的最合适的一维问题。ZND制表方法在各种H2-O2混合物中的一维稳定和脉动爆轰以及二维规则和不规则爆轰中都得到了验证。制表化学模拟能够在传播速度、细胞结构和源项统计方面再现详细的化学结果。对于氢爆炸,标量传输的计算成本减少了9倍,化学成本减少了17倍。碳氢化合物燃料有望节省更多的计算量。新颖性和重要性声明由于整合精确的化学模型的巨大成本,模拟爆炸通常具有挑战性。在爆燃中,通过预先计算化学成分并将信息收集到运行时使用的查找表中,可以降低该成本。虽然化学制表法最近被用于超音速燃烧,例如超燃冲压发动机,但这些方法的典型假设并不适用于爆轰。我们提出了一种新的表格化学方法,适用于爆炸和再现关键参数,如感应区长度和爆速。关键的新颖之处在于:(1)使用进度变量和温度作为制表坐标,(2)选择一维Zel ' ovich - von Neumann-Döring爆炸作为要制表的相关物理问题。新模型显著降低了仿真成本。
Tabulated chemistry approach for detonation simulations
Chemistry modeling in detonations typically relies on two broad approaches: simplified models with one- or two-step chemistry, and detailed chemistry. These approaches require choosing between computational efficiency or physical accuracy. To reduce the cost of chemistry while maintaining accurate physics, tabulated chemistry has been used extensively for flames/deflagrations in the low Mach number framework. In the simplest tabulated chemistry model for premixed flames, a progress variable, describing the progress of reactions in the system, is transported in the simulation. This progress variable is then used to look up all other species, transport properties, and thermodynamic variables from a pre-computed table. The present work extends the tabulated chemistry method to detonations. Even in non-reacting compressible flow simulations, the enthalpy and specific heat capacity are required; to describe these thermodynamic variables, the temperature is selected as a second table coordinate. The two table coordinates are able to capture virtually all variations in the progress variable source term. The Zel’dovich–von Neumann–Döring (ZND) model is found to be the most appropriate one-dimensional problem for generation of the table. The ZND tabulation approach is validated for both one-dimensional stable and pulsating and two-dimensional regular and irregular detonations in various - mixtures. The tabulated chemistry simulations are able to reproduce the detailed chemistry results in terms of propagation speed, cellular structures, and source term statistics. For hydrogen detonations, the computational cost of scalar transport is reduced by a factor of 9 and the cost of the chemistry is reduced by a factor of 17. More substantial computational savings are expected for hydrocarbon fuels.
Novelty and significance statement
Detonations are often challenging to simulate due to the significant cost of integrating accurate chemical models. In deflagrations, this cost has been reduced by pre-computing the chemistry and collecting the information into a lookup table to be used at runtime. Although chemistry tabulation has been adapted recently for supersonic combustion, such as in scramjets, the typical assumptions of these approaches do not apply to detonations. We propose a new tabulated chemistry approach, valid for detonations and reproducing critical parameters such as induction zone length and detonation velocity. The key novelty lies in (1) the use of progress variable and temperature as the coordinates for tabulation, and (2) the selection of one-dimensional Zel’dovich–von Neumann–Döring detonations as the relevant physical problem to be tabulated. The new model significantly reduces the cost of simulations.
期刊介绍:
The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on:
Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including:
Conventional, alternative and surrogate fuels;
Pollutants;
Particulate and aerosol formation and abatement;
Heterogeneous processes.
Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including:
Premixed and non-premixed flames;
Ignition and extinction phenomena;
Flame propagation;
Flame structure;
Instabilities and swirl;
Flame spread;
Multi-phase reactants.
Advances in diagnostic and computational methods in combustion, including:
Measurement and simulation of scalar and vector properties;
Novel techniques;
State-of-the art applications.
Fundamental investigations of combustion technologies and systems, including:
Internal combustion engines;
Gas turbines;
Small- and large-scale stationary combustion and power generation;
Catalytic combustion;
Combustion synthesis;
Combustion under extreme conditions;
New concepts.