浸入式边界方法的研究及应用进展

王卓; 杜林; 成龙; 孙晓峰

doi:10.6052/1000-0992-23-026

浸入式边界方法的研究及应用进展

doi: 10.6052/1000-0992-23-026

王卓¹,
杜林¹,
成龙²,
孙晓峰^3, ,

1.
北京航空航天大学航空发动机研究院, 北京 100191
2.
华为技术有限公司, 编译器与编程语言实验室, 北京 100094
3.
北京航空航天大学能源与动力工程学院, 北京 100191

基金项目: 国家自然科学基金(52022009)资助项目.

详细信息

作者简介:
孙晓峰, 1988年在北京航空航天大学获博士学位后留校工作, 并于1993年3月晋升为北航动力系教授、1994年任博士生导师. 近年来, 在叶轮机三维可压缩旋转失速稳定性理论、叶轮机亚/超音速叶片气动弹性稳定性的主/被动控制、航空发动机声学设计技术等方面做出了有意义的学术贡献. 具体来说, 他不仅比较系统地发展了航空推进系统三维流动, 燃烧不稳定性理论和控制方法, 还据于此提出了一种完全不同于国际上任何方案的叶轮机非定常流壁面控制方法, 实验上成功地实现了对压气机旋转失速的混合控制. 他还提出了一种计算运动边界问题的谱方法, 在气动声学, 气动弹性流固耦合问题中得到应用. 此外, 在波涡相互作用以及多空板声阻抗模型方面做了系统性的研究工作, 所发展的波涡相互作用模型对国际同类研究有显著影响, 并被国际同行用他和合作者的名字命名. 其主要研究成果均发表在《Physics of Fluids》《AIAA Journal》《Journal of The Acoustical Society of America》《Journal of Propulsion and Power》以及《Journal of Sound and Vibration》等本领域的国际著名杂志上. 此外, 自九十年代以来, 作为访问科学家或访问教授, 曾先后应邀在日本京都大学、东京大学, 德国宇航院柏林流体所, 英国剑桥大学工程系, 美国宾州州立大学, 麻省理工学院以及法国中央理工大学从事合作研究. 孙晓峰现任中国工程热物理学会常务理事, 中国航空学会动力分会总干事, 日本燃气轮机学会 (GTSJ) 国际顾问委员会 (IAC) 成员, 《航空学报》中文, 英文刊主编. 1996年获中国青年科技奖, 1999年获国家杰出青年, 同年入选国家人事部百千万工程. 2005年担任美国《AIAA Journal of Propulsion and Power》顾问编委 (Editorial Advisory Board) . 孙晓峰教授现任中国工程热物理学会常务理事, 中国航空学会动力分会总干事, 日本燃气轮机学会 (GTSJ) 国际顾问委员会 (IAC) 成员. 此外, 同年批准为国家人事部“百千万人才工程”第一、第二层次人选. 2012年, 任973计划项目“大型客机主要气动噪声机理及先进控制方法研究”首席科学家. 2016—2022年任中国航空发动机集团公司外部董事

通讯作者:
sunxf@buaa.edu.cn

中图分类号: V231
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出版历程
- 收稿日期: 2023-07-12
- 录用日期: 2023-09-11
- 网络出版日期: 2023-09-13
- 刊出日期: 2023-12-30

Advances in the investigations and applications of the immersed boundary method

1.
Aeroengine Research Institute, Beihang University, Beijing 100191, China
2.
Compilers & Programming Languages Lab, Huawei Technologies Co. Ltd, Beijing 100094, China
3.
School of Energy and Power Engineering, Beihang University, Beijing 100191, China

More Information

Corresponding author: sunxf@buaa.edu.cn

摘要

摘要: 本文总结了浸入式边界方法 (immersed bundary method, IB method) 中的力源建模研究进展, 并且对该方法在诸如生物体绕流及流固耦合等典型的复杂边界以及运动边界问题中的应用进行了介绍. 边界精度低是IB方法主要特征之一, 但该方法目前在计算气动声学等高精度计算中同样有所应用. 最后本文对IB方法在处理高雷诺数流动问题上所面临的挑战以及目前研究进展和未来发展方向进行了介绍.
- 浸入式边界方法 /
- 生物体绕流 /
- 流固耦合 /
- 计算气动声学 /
- 高雷诺数流动
Abstract: This paper summarizes the advances in the modelling of force source for the immersed boundary (IB) method. Introductions have been given to the applications of this method in the fields of flow around biological structures and fluid-structure interaction, which are representatives of problems with complex and moving geometries, respectively. Although low accuracy at boundary is one main feature of the IB method, it has also been applied to these computational aeroacoustic problems which requires high-order accuracy. Finally, the challenges, advances and future expects of the IB method in dealing with high-Reynolds-number flow are also reviewed.
- immersed boundary method /
- flow around biological structures /
- fluid-structure interaction /
- computational aeroacoustics /
- high-reynolds-number flow

HTML全文

图 1 用于研究心脏血液流动的模型示意图

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图 2 笛卡尔网格上边界对流场的影响通过力源来刻画

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图 3 (a) 固壁边界虚拟弹簧力示意图, (b) 锐利界面的浸入式边界方法

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图 4 蝙蝠鱼示意图(Huang et al. 2020, Zhang et al. 2022b)

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图 5 鱼类群体游泳数值模拟中不同个体的尾迹互相干涉(Peng et al. 2018)

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图 6 基于IB方法的叶轮机械转静干涉计算. (a) 转静叶片排模型, (b) 流场瞬时涡量分布(Du et al, 2016a, 2016b)

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图 7 (a) 二维柔性细丝示意图, (b) 刚性/柔性细丝组合体

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图 8 长度对刚性/柔性细丝组合体流固耦合响应及尾迹的影响(Ni et al. 2023)

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图 9 多个圆柱散射下的声场压力分布(Sun et al. 2012)

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图 10 叶栅声共振所对应的流场特征. (a) 压力云图, (b) 涡量云图(Cheng et al. 2021a)

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图 11 开式转子流致发声直接数值模拟结果. (a) 瞬时压力纹影图, (b) 马赫数云图分布

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图 12 采用自适应网格加密生成的多层网格系统(Wang et al. 2020)

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图 13 基于SA显式壁面模型的湍流边界层速度分布与壁面律对比(Chen et al. 2023)

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图 14 (a) 内流问题示意图, (b) 采用笛卡尔网格结合自适应加密所生成的网格系统, (c) 流道贴体网格结合自适应加密生成的网格系统(Wang et al. 2023)

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图 15 三维亚声速平面叶栅叶片表面压力分布数值模拟结果及其与实验的对比(Wang et al. 2023)

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