Thermal and Reactive Flow Simulation on High-End Computers

高端计算机上的热流和反应流模拟

• 批准号: EP/J016381/1
• 负责人: Kai Luo
• 金额: $ 8.74万
• 依托单位: University of Southampton
• 依托单位国家: 英国
• 项目类别: Research Grant
• 财政年份: 2012
• 资助国家: 英国
• 起止时间: 2012 至 无数据
• 项目状态: 已结题
• 来源: https://gtr.ukri.org/projects?ref=EP%2FJ016381%2F1
• 关键词: Thermal; Reactive; Flow; Simulation; End

Thermal and reactive flows are cross-cutting fundamental disciplines that have found applications in technologies such as aerospace engineering, combustion engines for power generation and propulsion, geothermal energy, solar thermal energy, bioenergy, nanotechnology, chemical engineering and climate science, etc. Research in the field is a prime example where high-end computing (HEC) can have a crucial impact, as the reliability and accuracy of numerical prediction and diagnosis of thermal and reactive flows are directly linked to the computational grid resolution and the size of the time steps. The reason lies with the extremely wide range of time and length scales present in thermal and reactive flows, which are typically turbulent as well. There are 9 to 12 orders of magnitude change between the smallest and the largest length and time scales present in thermal and reactive flows of technical relevance, which should ideally be resolved by experimental measurement or numerical simulation. To study such complex phenomena by experiment alone would be prohibitively expensive and laborious if possible at all. Numerical simulation, on the other hand, offers non-intrusive, virtual "measurement" of all relevant quantities at desired resolution and accuracy, provided sufficient computing power is available. Over the past two decades, the world has first seen gigaflops supercomputers, then teraflops and more recently petaflops machines. The pace of development towards exa-scale HEC platforms has recently quickened. Only last autumn, Tianhe-1A caused a stir by reaching 2.566 petaflops maximum sustained calculation speed, but six months later the K computer achieved an astonishing 8.162 petaflops. At least two HEC machines with 20 petaflops are being built in the world and expected to enter service next year (http://www.top500.org/). The problem is that advance in supercomputing hardware and software, impressive as it appears, has barely kept pace with the research needs. Therefore, frontier research in computational thermal and reactive flows tends to be strongly associated with making use of the latest HEC available. We believe that HEC is a key enabler of cutting-edge research in thermal and reactive flow flows. The main purpose of this application is to secure HEC resources on HECToR and its successors to support funded research projects in the field. These include: (a) K H Luo (P.I.), EPSRC grant No. EP/I016570/1 (09/2011 - 08/2014), "Tackling Combustion Instability in Low-Emission Energy Systems: Mathematical Modelling. Numerical Simulations and Control Algorithms"; (b) K H Luo (P.I.) and R W Eason, EPSRC grant No. EP/I012605/1 (05/2011 - 05/2014), "Laser-Induced Forward Transfer Nano-Printing Process - Multiscale Modelling, Experimental Validation and Optimization"; and (c) N D Sandham (P.I.), on-going LAPCAT II EU/FP7, "Long-term advanced propulsion concepets and technologies". In addition, the widely used SBLI code first developed by the applicants will be extended to incorporate capabilities for reactive flow simulation. By making use of the world-class computing facility HECToR, the above projects will fulfil the objectives of producing significant, world-leading research results. Examples of world-first simulations will include: (a) largest direct numerical simulation of a turbulent premixed flame interacting with acoustic waves (b) lattice Boltzmann simulation of the complete Laser-Induced Forward Transfer (LIFT) process; and (c) large-eddy simulation of a complete nose-to-tail scramjet engine. These projects are of direct interest to large research communities in aerospace engineering, combustion, nanotechnology, high-performance computing and so on, and will involve a dozen UK and EU companies, which will ensure wide and timely dissemination of research results.

热流和反应流是交叉的基础学科，已在航空航天工程、发电和推进用内燃机、地热能、太阳热能、生物能源、纳米技术、化学工程和气候科学等技术中得到应用。该领域是高端计算 (HEC) 可以产生至关重要影响的一个典型例子，因为热流和反应流数值预测和诊断的可靠性和准确性与计算网格分辨率和时间步长直接相关。原因在于热流和反应流中存在极其广泛的时间和长度尺度，这些流通常也是湍流。技术相关的热流和反应流中存在的最小和最大长度和时间尺度之间存在 9 至 12 个数量级的变化，理想情况下应通过实验测量或数值模拟来解决。如果可能的话，仅通过实验来研究如此复杂的现象将是极其昂贵和费力的。另一方面，只要有足够的计算能力，数值模拟就可以以所需的分辨率和精度对所有相关量进行非侵入式虚拟“测量”。在过去的二十年里，世界首先出现了千兆浮点运算的超级计算机，然后是万亿次浮点运算，最近又出现了千万亿次浮点运算的计算机。亿级 HEC 平台的开发步伐最近加快了。就在去年秋天，天河一号A因达到2.566 petaflops的最大持续计算速度而引起轰动，但六个月后，K计算机达到了惊人的8.162 petaflops。世界上至少有两台 20 petaflops 的 HEC 机器正在建造中，预计明年投入使用 (http://www.top500.org/)。问题在于，超级计算硬件和软件的进步虽然看起来令人印象深刻，但几乎跟不上研究需求的步伐。因此，计算热流和反应流的前沿研究往往与最新可用的 HEC 的使用密切相关。 我们相信 HEC 是热流和反应流尖端研究的关键推动者。此应用程序的主要目的是确保 HECToR 及其后续产品上的 HEC 资源，以支持该领域资助的研究项目。其中包括：(a) K H Luo (P.I.)，EPSRC 拨款号 EP/I016570/1 (09/2011 - 08/2014)，“解决低排放能源系统中的燃烧不稳定性：数学建模。数值模拟和控制算法”; (b) K H Luo (P.I.) 和 R W Eason，EPSRC 拨款号 EP/I012605/1 (05/2011 - 05/2014)，“激光诱导正向转印纳米打印工艺 - 多尺度建模、实验验证和优化” ; (c) N D Sandham（P.I.），正在进行的 LAPCAT II EU/FP7，“长期先进推进概念和技术”。此外，申请人首先开发的广泛使用的SBLI代码将被扩展以纳入反应流模拟的功能。通过利用世界一流的计算设施HECToR，上述项目将实现产生重大、世界领先的研究成果的目标。世界首创的模拟示例包括：(a) 湍流预混火焰与声波相互作用的最大直接数值模拟 (b) 完整激光诱导前向传递 (LIFT) 过程的晶格玻尔兹曼模拟； (c) 完整的从头到尾的超燃冲压发动机的大涡模拟。这些项目与航空航天工程、燃烧、纳米技术、高性能计算等领域的大型研究团体直接感兴趣，并将涉及十几家英国和欧盟公司，这将确保研究成果的广泛和及时传播。

项目成果

Thermodynamic consistency of the pseudopotential lattice Boltzmann model for simulating liquid-vapor flows

模拟液汽流动的赝势格子玻尔兹曼模型的热力学一致性

• DOI: http://dx.10.1016/j.applthermaleng.2014.03.030
• 发表时间: 2014
• 期刊: Applied Thermal Engineering
• 影响因子: 6.4
• 作者: Li Q

Effect of the forcing term in the pseudopotential lattice Boltzmann modeling of thermal flows.

热流赝势晶格玻尔兹曼模型中的强迫项的影响。

• DOI: http://dx.10.1103/physreve.89.053022
• 发表时间: 2014
• 期刊: Physical review. E, Statistical, nonlinear, and soft matter physics
• 作者: Li Q

Simultaneous planar and volume cross-LIF imaging to identify out-of-plane motion

同时进行平面和体积交叉 LIF 成像以识别平面外运动

• DOI: http://dx.10.1016/j.proci.2014.07.042
• 发表时间: 2015
• 期刊: Proceedings of the Combustion Institute
• 影响因子: 3.4
• 作者: Meares S

Effects of pressure on cellular flame structure of high hydrogen content lean premixed syngas spherical flames: A DNS study

压力对高氢含量贫预混合成气球形火焰蜂窝火焰结构的影响：DNS 研究

• DOI: http://dx.10.1016/j.ijhydene.2016.09.181
• 发表时间: 2016
• 期刊: International Journal of Hydrogen Energy
• 影响因子: 7.2
• 作者: Ranga Dinesh K

Receptivity to Freestream Acoustic Noise in Hypersonic Flow over a Generic Forebody

通用前体对高超声速流中自由流声学噪声的感受性

• DOI: http://dx.10.2514/1.a34283
• 发表时间: 2019
• 期刊: Journal of Spacecraft and Rockets
• 影响因子: 1.6
• 作者: Cerminara A