| 姓名： |
赵磊 |
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| 性别： |
男 |
| 英文名： |
Zhao Lei |
| 人才称号： |
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| 职称： |
副教授/博士生导师 |
| 职务： |
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专业： |
流体力学 |
| 所在机构： |
力学学科，高速空气动力学研究室 |
个人主页： |
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| 邮箱： |
lei_zhao@tju.edu.cn |
办公地点： |
36楼333 |
| 传真： |
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办公电话： |
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| 主要学历： |
2011.9-2017.1 天津大学 博士
2007.9-2011.7 天津大学 本科
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| 主要学术经历： |
2023.6-至今 天津大学 准聘副教授 博士生导师
2019.7-2023.5 天津大学 助理教授 硕士生导师（2020.8-至今）
2017.8-2019.7 中国空气动力研究与发展中心 博士后
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| 主要研究方向： |
主要从事与流动稳定性、转捩预测及控制相关的研究
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| 主要讲授课程： |
本科生课程《工程力学》、研究生课程《边界层理论》
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| 主要学术兼职： |
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| 主要学术成就： |
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| 主要科研项目： |
主持科研项目：
纵向课题：
1. 2024-2027，国家自然科学基金面上项目，头部激波和熵层对高超声速圆锥边界层感受性的影响及SF-HLNS预测方法。在研，负责人。
2. 2021-2024，国家自然科学基金企业联合基金重点项目，临近空间飞行器表面烧蚀形貌对边界层转捩影响的关键机理。在研，本单位负责人，项目由中科院力学所、天津大学、航天十一院联合承研。
3. 2021-2023，国家自然科学基金青年基金，高超声速边界层中条带对自由流扰动的感受性机理。已结题，负责人。
4. 2021-2024，基础加强项目子课题2项。总经费180万元，在研，负责人。
5. 2024-2025，领域基金。在研，本单位负责人，项目由航天十一院、航天一院、天津大学联合承研。
6. 2024-2024，基础研究项目。总经费25.7万元，在研，负责人。
横向项目：
7. 2021-2022，高超声速复杂曲面边界层流动稳定性分析研究。总经费60万元，已结题，负责人。
8. 2020-2020，考虑非平行性的流动稳定性分析方法。总经费20万元，已结题，负责人。
参与科研项目：
参与其它纵向课题、横向项目多项。
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| 代表性论著： |
2023年天津大学优秀硕士学位论文指导教师。
代表性论文： “*”表示通讯作者
[16] Zhao Lei, Zhou Wenqiang, Li Xinliang, Zhang Shaolong & Zhang Yongming*. 2024. Prediction of Transition Locations in Regions of the Minor Axis of Hypersonic Elliptic Cones Using the BiGlobal-eN Method. Advances in Applied Mathematics and Mechanics. 16 (4). 805-832.
[15] Song Runjie, Dong Ming* and Zhao Lei*. Principle of fundamental resonance in hypersonic boundary layers: an asymptotic viewpoint. Journal of Fluid Mechanics, 2024. 978: p. A30.
[14] Ji Xiaoyang, Dong Ming* and Zhao Lei*. Impact of compliant coating on Mack-mode evolution in hypersonic boundary layers. Journal of Fluid Mechanics, 2023. 974: p. A1.
[13] Song Runjie, Dong Ming* and Zhao Lei*. Effect of cone rotation on the nonlinear evolution of Mack modes in supersonic boundary layers. Journal of Fluid Mechanics, 2023. 971: p. A4.
[12] Zhao Lei, He Jianhong and Dong Ming*. Asymptotic theory of Mack-mode receptivity in hypersonic boundary layers due to interaction of heating/cooling sources and a freestream sound wave. Journal of Fluid Mechanics, 2023. 963: p. A34.
[11] Song Qinyang, Zhao Lei* and Dong Ming*. Effect of porous coatings on the nonlinear evolution of Mack modes in hypersonic boundary layers. Physics of Fluids, 2023. 35(5): p. 054115.
[10] Song Runjie, Dong Ming* and Zhao Lei*. Revisit of the oblique-breakdown regime in supersonic boundary layers and mechanism of the extra amplification of streak modes. Physics of Fluids, 2022. 34(10): p. 104110.
[9] Song Qinyang and Zhao Lei*. Scattering of Mack modes by solid-porous junctions in hypersonic boundary layers. Physics of Fluids, 2022. 34(8): p. 084104.
[8] Zhao Lei and Dong Ming*. Effect of surface temperature strips on the evolution of supersonic and hypersonic Mack modes: Asymptotic theory and numerical results. Physical Review Fluids, 2022. 7(5): 053901.
[7] 孙培成, 赵磊*, 董明, 基于HLNS方法对高超声速边界层中非模态扰动演化的研究. 力学进展, 2022. 52(1): p. 180-195.
[6] Dong Ming* and Zhao Lei. An asymptotic theory of the roughness impact on inviscid Mack modes in supersonic/hypersonic boundary layers. Journal of Fluid Mechanics, 2021, 913: A22.
[5] Zhao Lei, Dong Ming*. Effect of suction on laminar-flow control in subsonic boundary layers with forward-/backward-facing steps. Physics of Fluids. 2020;32(5):054108.
[4] Zhao Lei, Dong Ming, Yang Yan-guang*. Harmonic linearized Navier-Stokes equation on describing the effect of surface roughness on hypersonic boundary-layer transition. Physics of Fluids. 2019;31(3):034108.（Editor’s Pick）
[3] Song Run-jie#, Zhao Lei#, Huang Zhang-feng*. Conservation relation of generalized growth rate in boundary layers. Applied Mathematics and Mechanics. 2018;39(12):1755-68
[2] Zhao Lei, Yu Gao-tong, Luo Ji-sheng*. Extension of e N method to general three-dimensional boundary layers. Applied Mathematics and Mechanics. 2017;38(7):1007-18.
[1] Zhao Lei, Zhang Cun-bo, Liu Jian-xin *, Luo Ji-sheng. Improved algorithm for solving nonlinear parabolized stability equations. Chinese Physics B. 2016;25(8):084701.
其它学术论文：
[9] 刘洋,赵磊*.高速平板边界层中定常条带的前缘感受性.空气动力学学报,2024,42(04):14-26.
[8] 黄加昊, 赵磊*, 赵瑞, 基于调和线性化Navier-Stokes方程的局部感受性. 空气动力学学报, 2024. 42(03): p. 69-82.
[7] Xiong, Youde, Zhao Lei and Wu Jie*. Characterization of Disturbance Resonance in Postshock of Blunt Body in Hypersonic Flow. AIAA Journal, 2023: p. 1-8.
[6] Song Run-jie, Zhao Lei, Huang Zhang-feng*(a). Improvement of the parabolized stability equation to predict the linear evolution of disturbances in three-dimensional boundary layers based on ray tracing theory. Physical Review Fluids. 2020;5(3):033901.
[5] Song Run-jie, Zhao Lei, Huang Zhang-feng*(b). Secondary instability of stationary Görtler vortices originating from first/second Mack mode. Physics of Fluids. 2020;32(3):034109.
[4] 李强, 赵磊, 陈苏宇, 江涛, 庄宇, 张扣立*. 展向凹槽及泄流孔对高超声速平板边界层转捩影响的试验研究. 物理学报. 2020;69(02):195-202.
[3] Zhao Jin-shan*, Liu Sen, Zhao Lei, Zhang Zhi-gang. Numerical study of total temperature effect on hypersonic boundary layer transition. Physics of Fluids. 2019;31(11):114105.
[2] 陈杰*, 赵磊. 高超声速流存在局部稀薄效应的一个判据及相应的流动特性. 空气动力学学报. 2018;36(01):4-11.
[1] Chen Jie*, Zhao Lei. Numerical analysis of locally rarefied effects in hypersonic shear flow, 2nd International Workshop on Aerodynamics Covering Flow Regimes, Mianyang, 2017.
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