教育及工作经历：

2021年9月-2025年9月 浙江大学 工学博士

2025年11月-至今 山东交通学院 学术副教授

研究方向：

围绕飞行器总体设计、旋翼空气动力学、智能流体力学等学科方向，拟开展新构型垂直起降飞行器总体设计；复杂气动布局（分布式螺旋桨/机翼/机身）气动干扰机理；涡动力学；智能/数据驱动流体力学方法等研究。

发表文章：

2026

1. Yue H, Gao Z, Liu P, et al. Transition planning and control methods for a tilt-wing VTOL UAV: From hardware design to flight validation[J]. Aerospace Science and Technology, 2026, 168: 111265.

2025

1. Gao Z, Luo H, Shao X, et al. Meshless simulation of multi-propeller/wing interactions in typical distributed electric propulsion configurations[J]. Aerospace Science and Technology, 2025, 163: 110287.

2. Gao Z, Zheng S, Zhang S, et al. Aerodynamic characteristics study on multiple propellers in distributed electric propulsion configurations[J]. Physics of Fluids, 2025, 37(1): 15131. (Editor’s Pick)

3. 高泽明, 邵雪明, 王家鼎, 等. 垂直下降状态下螺旋桨气动特性及涡环特征[J]. 空气动力学学报, 2025, 43(1): 1-11.

2024

1. Gao Z, Yue H, Shao X, et al. Aerodynamic interaction mechanisms in typical wingtip-mounted tractor propeller configurations[J]. Physics of Fluids, 2024, 36(12): 125126.

2. Gao Z, Shao X, Zeng L, et al. Hybrid aerodynamic optimization of a propeller based on the reformulated blade element momentum theory[J]. Journal of Aerospace Engineering, 2024, 37(2): 4023112.

3. Zhang S, Lin Z, Gao Z, et al. Wind tunnel experiment and numerical simulation of secondary flow systems on a supersonic wing[J]. Aerospace, 2024, 11(8): 618.

4. Zeng L, Gao Z, Xu T, et al. Mechanism analysis of the vortex ring and its effects on an axial descending rotor[J]. International Journal of Fluid Engineering, 2024, 1(2).

授权发明专利：

1.一种模块化的交叉式纵列无人直升机及其工作方法:ZL 2019 1 0547327.3.

2.一种尾座式三涵道垂直起降飞行器及其控制方法：ZL 2022 1 1649322.X.

3.一种变结构多涵道垂直起降飞行器及其控制方法：ZL 2023 1 1551140.3.