周志宇｜北京航空航天大学｜学者主页

2026

Leaf venation-inspired novel method to develop cooling configurations for turbine blade trailing edge

Xilai Wang, Zhiyu Zhou, Haiwang Li, Gang Xie, Long Meng

Applied Thermal Engineering

DOI

2026

A numerical investigation of the coupled effects of casing purge flow and blade tip film cooling with various tip cooling parameters

Haiwang Li, Zhenzhen Xue, Zhiyu Zhou, Gang Xie, Long Meng, Xiaoyang Huang, Shilin Zhong

Aerospace Science and Technology

DOI

2026

Multi-objective optimizations of guide fins for pin fin cooling in the wedge channel of turbine blade trailing edge

Xilai Wang, Zhiyu Zhou, Haiwang Li, Gang Xie, Long Meng

Aerospace Science and Technology

DOI

2026

Leaf venation-inspired novel method for flow organization of impingement cooling on gas turbine blade

Xilai Wang, Zhiyu Zhou, Haiwang Li, Gang Xie, Long Meng

Aerospace Science and Technology

DOI

2026

Experimental investigation of film cooling characteristics in the supersonic region of a turbine blade suction surface

Yuzhu Lou, Haiwang Li, Gang Xie, Zhi Tao, Jinghan Zhang, Juqiang Lin, Zhiyu Zhou

Applied Thermal Engineering

DOI

2026

Experimental optimization of novel B-shaped and C-shaped holes on flat plate and linear cascade models

Haiwang Li, Yiming Luo, Zhiyu Zhou, Gang Xie, Long Meng, Yuzhu Lou

Aerospace Science and Technology

DOI

2025

Large eddy simulations and experimental study for the effect of hole exit filleted corners on film cooling effectiveness

Yan Hua Jiang, Xianyu Wang, Haiwang Li, Yi Huang, Gang Xie, Zhiyu Zhou

Aerospace Science and Technology

DOI

2025

Parametric modeling and thermal optimization of novel bionic heat sinks inspired by leaf venation

Xilai Wang, Zhiyu Zhou, Haiwang Li, Gang Xie, Long Meng

International Journal of Heat and Mass Transfer

DOI

2025

In-depth analysis of flow field aerodynamic mechanism in integrated combustor–turbine structure for heavy-duty gas turbine

Jinghan Zhang, Haiwang Li, Zhiyu Zhou, Yuzhu Lou, Gang Xie

Physics of Fluids

DOI

2025

Experimental investigation of film cooling effectiveness deviation on a transonic blade: Oxygen mixture correction for pressure sensitive paint measurement

Yuzhu Lou, Haiwang Li, Gang Xie, Zhi Tao, Jinghan Zhang, Jiaqing Wu, Zhiyu Zhou

Aerospace Science and Technology

DOI

2025

Programmed constructions of novel bionic heat sinks inspired by leaf venation pattern

Xilai Wang, Zhiyu Zhou, Haiwang Li, Gang Xie, Long Meng, Zhiqiang Zhang

International Journal of Heat and Mass Transfer

DOI

2024

高压涡轮导叶吸力面异型孔的对比研究

江艳，李海旺，陶智，周志宇

《风机技术》

2024

高压涡轮导叶压力面异型气膜孔特性

江艳，李海旺，谢刚，陶智，周志宇

《航空动力学报》

2024

冷却气进气角度对端壁泄漏流气膜冷却特性影响

唐润泽，李海旺，周志宇，谢刚

《航空动力学报》

2024

涡轮动叶吸力面气膜冷却径向差异对比

王磊，李海旺，谢刚，周志宇

《航空动力学报》

2024

椭圆锥孔对导叶前缘冷效的影响及优化

江艳，李海旺，谢刚，周志宇

《航空动力学报》

2024

涡轮动叶背侧不同叶高处异型孔气膜对比

王磊，李海旺，谢刚，周志宇

《航空动力学报》

2024

A comprehensive investigation of the effect of hole diameter and number on film cooling performance of rotating blade leading edge

Meng Gu, Haiwang Li, Zhiyu Zhou, Gang Xie, Song Liu, Yu-zhu Lou

Aerospace Science and Technology

DOI

2024

Experimental Investigation of the Film Cooling Effectiveness Deviation Using Pressure Sensitive Paint Measurement for Different Hole Structures

Yuzhu Lou, Zhi Tao, Haiwang Li, Zhiyu Zhou, Jinghan Zhang, Gang Xie

DOI

2024

Effects of Trench Structural Features on the Film Cooling Effectiveness and Particle Deposition Performances of a Fan-Shaped Hole

Siyu Chen, Haiwang Li, Gang Xie, Zhiyu Zhou, Long Meng

DOI

2024

Film Cooling Performance on Rotating Blade Leading Edge With Various Rotating Speed and Film Hole Structures

Yan Hua Jiang, Yi Jun Huang, Haiwang Li, Zhiyu Zhou, Gang Xie

DOI

2024

Numerical Study on the Console Hole Film Cooling Performance With Varied Hole Inlet Shape

Yiming Luo, Haiwang Li, Zhiyu Zhou, Gang Xie, Long Meng

DOI

2024

Effect of the Upstream Shroud Purge Flow on the Cooling Performances of Turbine Blade Tip

Zhenzhen Xue, Haiwang Li, Zhi Tao, Zhiyu Zhou, Long Meng, Gang Xie

DOI

2022

Shape Optimization of the Laidback Fan-Shaped Film Cooling Hole on Pressure Surface of Turbine Guide Vane

Yan Hua Jiang, Zhi Tao, Haiwang Li, Zhiyu Zhou

DOI

2022

Optimum cooling performance of a multiple-jets impingement cooling system by controlling the inlet flow condition

Long Meng, Haiwang Li, Xie Gang, Zhiyu Zhou

Proceedings

DOI

2020

The cooling performance of three-row compound angle holes on the suction surface of a rotating turbine blade

Zhiyu Zhou, Haiwang Li, Gang Xie, Shuangzhi Xia, Jianjun Zhou

Propulsion and Power Research

DOI

2020

The cooling performance of multiple rows of film holes on the suction surface of a turbine blade under rotating conditions

Haiwang Li, Zhiyu Zhou, Gang Xie, Shuangzhi Xia, Zhi Tao

Applied Thermal Engineering

DOI

2020

Film Cooling Performance on Turbine Blade Suction Side With Various Film Cooling Hole Arrangements

Zhiyu Zhou, Haiwang Li, Gang Xie, Ruquan You

DOI

2019

Film cooling of cylindrical holes on turbine blade suction side near leading edge

Zhiyu Zhou, Haiwang Li, Haichao Wang, Gang Xie, Ruquan You

International Journal of Heat and Mass Transfer

DOI

2019

A study for the film cooling performance on the turbine blade suction side tip region under rotating conditions

Haichao Wang, Zhi Tao, Zhiyu Zhou, Huimin Zhou, Yiwen Ma, Haiwang Li

International Journal of Heat and Mass Transfer

DOI

2019

Experimental and numerical study of the film cooling performance of the suction side of a turbine blade under the rotating condition

Haichao Wang, Zhi Tao, Zhiyu Zhou, Feng Bo Han, Haiwang Li

International Journal of Heat and Mass Transfer

DOI

2019

An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition

Haichao Wang, Zhi Tao, Zhiyu Zhou, Guoqin Zhao, Feng Bo Han, Haiwang Li

Applied Thermal Engineering

DOI

2018

Rotating Film Cooling Performance of the Hole Near the Leading Edge on the Suction Side of the Turbine Blade

Zhiyu Zhou, Haiwang Li, Hai-chao Wang, Guoqin Zhao, Feng Bo Han, Min Wu

DOI

2018

Experimental investigation on the effects of rotation and the blowing ratio on the leading-edge film cooling of a twist turbine blade

Haiwang Li, Feng Bo Han, Yiwen Ma, Hai-chao Wang, Zhiyu Zhou, Zhi Tao

International Journal of Heat and Mass Transfer

DOI

2018

Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade

Haiwang Li, Feng Bo Han, Zhiyu Zhou, Yiwen Ma, Zhi Tao

International Journal of Heat and Mass Transfer

DOI

周志宇

精选作品

期刊论文

Leaf venation-inspired novel method to develop cooling configurations for turbine blade trailing edge

A numerical investigation of the coupled effects of casing purge flow and blade tip film cooling with various tip cooling parameters

Multi-objective optimizations of guide fins for pin fin cooling in the wedge channel of turbine blade trailing edge

Leaf venation-inspired novel method for flow organization of impingement cooling on gas turbine blade

Experimental investigation of film cooling characteristics in the supersonic region of a turbine blade suction surface

Experimental optimization of novel B-shaped and C-shaped holes on flat plate and linear cascade models

Large eddy simulations and experimental study for the effect of hole exit filleted corners on film cooling effectiveness

Parametric modeling and thermal optimization of novel bionic heat sinks inspired by leaf venation

In-depth analysis of flow field aerodynamic mechanism in integrated combustor–turbine structure for heavy-duty gas turbine

Experimental investigation of film cooling effectiveness deviation on a transonic blade: Oxygen mixture correction for pressure sensitive paint measurement

Programmed constructions of novel bionic heat sinks inspired by leaf venation pattern

高压涡轮导叶吸力面异型孔的对比研究

高压涡轮导叶压力面异型气膜孔特性

冷却气进气角度对端壁泄漏流气膜冷却特性影响

涡轮动叶吸力面气膜冷却径向差异对比

椭圆锥孔对导叶前缘冷效的影响及优化

涡轮动叶背侧不同叶高处异型孔气膜对比

A comprehensive investigation of the effect of hole diameter and number on film cooling performance of rotating blade leading edge

Experimental Investigation of the Film Cooling Effectiveness Deviation Using Pressure Sensitive Paint Measurement for Different Hole Structures

Effects of Trench Structural Features on the Film Cooling Effectiveness and Particle Deposition Performances of a Fan-Shaped Hole

Film Cooling Performance on Rotating Blade Leading Edge With Various Rotating Speed and Film Hole Structures

Numerical Study on the Console Hole Film Cooling Performance With Varied Hole Inlet Shape

Effect of the Upstream Shroud Purge Flow on the Cooling Performances of Turbine Blade Tip

Shape Optimization of the Laidback Fan-Shaped Film Cooling Hole on Pressure Surface of Turbine Guide Vane

Optimum cooling performance of a multiple-jets impingement cooling system by controlling the inlet flow condition

The cooling performance of three-row compound angle holes on the suction surface of a rotating turbine blade

The cooling performance of multiple rows of film holes on the suction surface of a turbine blade under rotating conditions

Film Cooling Performance on Turbine Blade Suction Side With Various Film Cooling Hole Arrangements

Film cooling of cylindrical holes on turbine blade suction side near leading edge

A study for the film cooling performance on the turbine blade suction side tip region under rotating conditions

Experimental and numerical study of the film cooling performance of the suction side of a turbine blade under the rotating condition

An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition

Rotating Film Cooling Performance of the Hole Near the Leading Edge on the Suction Side of the Turbine Blade

Experimental investigation on the effects of rotation and the blowing ratio on the leading-edge film cooling of a twist turbine blade

Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade

研究方向