个人简介
面向空天科技国家重大需求和飞行器气动相关前沿背景，围绕高速流体力学中的关键科学问题，主要研究方向为流动稳定性及层流-湍流转捩、高速空气动力学、计算流体力学、直接数值模拟，代表性贡献为首次直接揭示了高超声速转捩“钝度反转”的流动机理、发现了飞行环境转捩新规律、提出了宽速域失稳统一解释和转捩预测模型及参数敏感度估算模型。已在流体力学顶级期刊Journal of Fluid Mechanics（9篇）、Journal of Computational Physics、AIAA Journal、Chinese Journal of Aeronautics等流体力学及航空航天领域顶级SCI期刊发表论文26篇。其中，Q1区25篇、近五年 23 篇，第一/通讯作者17篇；一篇入选PoF编辑推荐专辑，并在期刊官网首页报道，一篇入选CJA亮点文章。曾在香港理工大学任助理教授（研究）、独立PI，并以博士生第一作者、本人唯一通讯作者在JFM等SCI 期刊发表论文多篇；主持航天院所横向课题等项目共3项，总额149万港元；英文授课2门。授权高超声速飞行器设计相关的国家发明专利2项，参与国家重大专项项目等多项，提出的高超声速转捩预测模型已应用于航空航天院所相关工程项目研制中。曾受邀担任第35届国际激波会议等3个国际会议的分会场主席，并作邀请报告。担任JFM、AIAAJ等近十个国际期刊的审稿人。独立开发了适用于一般曲线坐标系的稳定性解算软件CHASES，已应用于标准构型的线性/非线性流动稳定性分析，成为开展相关研究的自主计算平台。成果获院士团队、JFM副主编、AIAA会士等引用与正面评价。个人主页见 https://peixuguo.github.io。
代表论著：
1.Guo, P.* (2025) Transition reversal over a blunt plate at Mach 5. Part 2. The role of free-stream-disturbance form. Journal of Fluid Mechanics, 1025: A54. (Q1, 5/41, IF = 3.9)
2.Guo, P., Hao, J., & Wen, C. Y. (2025) Transition reversal over a blunt plate at Mach 5. Journal of Fluid Mechanics, 1005: A5. (Q1, 5/41, IF = 3.9)
3.Guo, P., Hao, J., & Wen, C. Y. (2023) Interaction and breakdown induced by multiple optimal disturbances in hypersonic boundary layer. Journal of Fluid Mechanics, 974: A50. (Q1, 5/41, IF = 3.9)
4.Chen, Y., Guo, P.*, & Wen, C. Y. (2026) Role of acoustic metasurface in the nonlinear mode-mode interaction and breakdown of hypersonic boundary layer. Journal of Fluid Mechanics, 1026: A27. (Q1, 5/41, IF = 3.9)
5.Chen, Y., Guo, P.*, & Wen, C. Y. (2023) A unified explanation of energy growth sources for unstable modes in flat-plate boundary layers. Journal of Fluid Mechanics, 972: A5. (Q1, 5/41, IF = 3.9)
6.Xu, B., Sun, C., & Guo, P.* (2026) A Central differential flux with high-order dissipation for robust simulations of transcritical flows. Journal of Computational Physics, 550: 114653. (Q1, 2/61, IF = 3.8)
7.Guo, P.*, Hao, J., & Wen, C. Y. (2025) Understanding the instability-wave selectivity of hypersonic compression ramp laminar flow. AIAA Journal, 63(7): 2580–2593. (Q1, 12/55, IF = 2.8)
8.Guo, P., Gao, Z., Zhang, Z., Jiang, C., & Lee, C. H. (2019) Local-variable-based model for hypersonic boundary layer transition. AIAA Journal, 57(6): 2372–2383. (Q1, 12/55, IF = 2.8)
9.Cao, S., Wang, Q., Guo, P., Li, J., & You, Y. (2026) On the transition zone in shock wave/boundary layer interactions. Journal of Fluid Mechanics, 1035: A43. (Q1, 5/41, IF = 3.9)
10.Cao, S., Hao, J., & Guo, P. (2024) Transition to turbulence in hypersonic flow over a compression ramp due to upstream forcing. Journal of Fluid Mechanics, 999: A37. (Q1, 5/41, IF = 3.9)
11.Hao, J., Cao, S., Guo, P., & Wen, C-Y. (2023) Response of hypersonic compression corner flow to upstream disturbances. Journal of Fluid Mechanics, 964: A25. (Q1, 5/41, IF = 3.9)
12.Cao, S., Hao, J., Guo, P., Wen, C-Y., & Klioutchnikov I. (2023) Stability of hypersonic flow over a curved compression ramp. Journal of Fluid Mechanics, 957: A8. (Q1, 5/41, IF = 3.9)
13.Guo, P., Shi, F., Gao, Z., Jiang, C., Lee, C. H., & Wen, C. Y. (2022) Heat transfer and behavior of the Reynolds stress in Mach 6 boundary layer transition induced by first-mode oblique waves. Physics of Fluids, 34(10): 104116. (Q1, 3/41, IF = 4.3) (Editor’s pick)
14.Guo, P., Gao, Z., Jiang, C., & Lee, C. H. (2021) Sensitivity analysis on supersonic-boundary-layer stability subject to perturbation of flow parameters. Physics of Fluids, 33: 084111. (Q1, 3/41, IF = 4.3)
15.Guo, P., Gao, Z., Jiang, C., Lee, C. H. (2020) Linear stability analysis on the most unstable frequencies of supersonic flat-plate boundary layers. Computers & Fluids, 197: 104394. (Q2, 59/171, IF = 3.0)
16.Guo, P., Liu, X., Zhao, R., Hao, J., & Wen, C. Y. (2023) Effect of acoustic metasurface on hypersonic-boundary-layer wave packet. Physics of Fluids, 35(9): 094110. (Q1, 3/41, IF = 4.3)
17.Guo, P., Gao, Z., Wu, Z., Liu, H., Jiang, C., & Lee, C. H. (2019) Investigations on the accurate prediction of supersonic shear layers for detached eddy simulation. Aerospace Science and Technology, 89: 46–57. (Q1, 6/55, IF = 5.8)
18.Guo, P., Shi, F., Gao, Z., Jiang, C., Lee, C. H., & Wen, C. Y. (2022) Sensitivity analysis on supersonic-boundary-layer stability: Parametric influence, optimization, and inverse design. Physics of Fluids, 34(10): 104113. (Q1, 3/41, IF = 4.3)
19.Chen, Y., Ma, T., Guo, P.*, Hao, J. & Wen, C. Y. (2025) Optimal disturbances and growth patterns in hypersonic blunt-wedge flow, Chinese Journal of Aeronautics, 38(7): 103461. (Q1, 7/55, IF = 5.7) (Featured article)
20.Chen, Y., Guo, P.*, & Wen, C. Y. (2023) Consistent energy-based framework of amplification mechanisms for the second mode in hypersonic boundary layers. Physics of Fluids, 35(12): 124107. (Q1, 3/41, IF = 4.3)
21.Huang, Q., Sun, C., & Guo, P.* (2025) Effect of angle of attack on the instability-wave selectivity in hypersonic compression ramp laminar flow. Physics of Fluids, 37(12): 124126. (Q1, 3/41, IF = 4.3)
22.Zhao, G., Wang, C. C., Li, X., Liu, X., Chen, Z., Uy, C. K., Hao, J., Guo, P., Zhang, Z., & Wen, C. Y. (2026) Convective instabilities in hypersonic compression ramp flows. AIAA Journal, accepted. (Q1, 12/55, IF = 2.8)
23.Huang C., Cao S., Hao J., Guo P., & Wen, C. Y. (2025) Laminar-turbulent transition in a hypersonic compression ramp flow. Physics of Fluids, 37: 034110. (Q1, 3/41, IF = 4.3)
24.Shi F., Guo, P., Liu, H., & Wang, T. (2024) Effect of vibrational excitation on vorticity amplification and transportation in shock/isotropic turbulence interaction: a numerical investigation. Physics of Fluids, 36: 085140. (Q1, 3/41, IF = 4.3)
25.Long, T., Guo, P., Zhao, R., Wen, C. Y., & Ji, F. (2023) Energy growth of vortical, acoustic, and entropic components of the second-mode instability in the hypersonic boundary layer. Physics of Fluids, 35(5): 054104. (Q1, 3/41, IF = 4.3)
26.Liu, X., Ma, D., Yang, M., Xia, X., & Guo, P. (2022) Modified block A* planning method for hybrid-driven underwater gliders. IEEE Journal of Oceanic Engineering, 47(1): 20–31. (Q1, 4/65, IF = 5.3)
27.Shen, P., Niu, J., Guo, P., & Gu, S. (2026) A Modular Method of Characteristics Framework for Controllable-Length Hypersonic Nozzle Design. Advances in Aerodynamics, accepted. (Q2, 20/41, IF = 2.3)
