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Thermal and Reactive Flow Simulation on High-End Computers

高端计算机上的热流和反应流模拟

基本信息

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

项目摘要

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。该领域的研究是高端计算(HEC)可以产生关键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直接与计算网格分辨率和时间步长的大小有关。原因在于热流和反应流中存在着非常广泛的时间和长度尺度，这两种流动通常也是湍流的。在与技术相关的热流和反应流中，最小和最大长度和时间尺度之间存在9到12个数量级的变化，理想情况下应该通过实验测量或数值模拟来解决。如果可能的话，仅仅通过实验来研究这种复杂的现象将是令人望而却步的昂贵和艰苦的。另一方面，如果有足够的计算能力，数值模拟提供了所有相关量的非侵入性的、虚拟的、以期望的分辨率和精度进行的“测量”。在过去的二十年里，世界上首先出现了千兆次浮点运算的超级计算机，然后是万亿次浮点运算的超级计算机，最近又出现了千万亿次浮点运算的机器。港灯向大型平台发展的步伐最近有所加快。就在去年秋天，天河一号的最大持续计算速度达到了2.566千万亿次，引起了轰动，但六个月后，K计算机达到了惊人的8.162千万亿次。世界上正在建造至少两台具有20千万亿次浮点运算能力的HEC机器，预计明年投入使用(http://www.top500.org/).问题是，超级计算硬件和软件的进步，尽管看起来令人印象深刻，但几乎跟不上研究需求。因此，计算热流和反应流的前沿研究往往与利用最新的HEC密切相关。我们相信，HEC是热流和反应流前沿研究的关键推动者。这项申请的主要目的是确保HEC在赫克托及其继任者身上的资源，以支持该领域的资助研究项目。这些资助包括：(A)罗启豪(P.I.)，EPSRC补助金编号EP/I016570/1(09/2011-08/2014)，“处理低排放能源系统中的燃烧不稳定性：数学模型。数值模拟和控制算法”；(B)罗启宏(P.I.)和R W Eason，EPSRC批准号。EP/I012605/1(05/2011-05/2014)，“激光诱导前向转移纳米印刷工艺--多尺度建模、实验验证和优化”；和(C)N D Sandham(P.I.)，正在进行的LAPCAT II EU/FP7，“长期先进推进设想和技术”。此外，由申请者首先开发的广泛使用的SBLI代码将被扩展，以包括反应流模拟功能。通过使用世界级的计算设施赫克托，上述项目将实现产生重要的、世界领先的研究成果的目标。世界首创的模拟实例将包括：(A)对湍流预混火焰与声波相互作用的最大直接数值模拟；(B)对整个激光诱导前向转移(LIFT)过程的格子Boltzmann模拟；以及(C)对整个机头到尾部超燃冲压发动机的大涡模拟。这些项目直接关系到航空航天工程、燃烧、纳米技术、高性能计算等领域的大型研究社区，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。