Dr. LI, Weihong
Assistant Professor
Contact InformationOffice:YEUNG-P6524
Phone:+(852)-3442 9601
Email:weihongli6@cityu.edu.hk
Web:Personal Homepage
Research InterestsAerospace Thermal Management
Heat and Mass Transfer
Interfacial Phenomena
Smart Windows

EducationB.S. in Thermal engineering from the Tsinghua University (2013)
Ph.D. in Energy and Power engineering from the Tsinghua University (2018)
Current PositionAssistant Professor in the Dept. of Mechanical Engineering of CityU
Professional ExperienceResearch Associate at University of Glasgow in UK (2019)
Research Assistant Professor of the Dept. of Mechanical and Aerospace Engineering in HKUST(2019-2021)
Selected Recent Journal PublicationW. Li#, C. Lin#, W. Ma, Y. Li, B. Huang*, S. Yao*, 2021, "Transparent Selective Photothermal Coatings for Antifogging Applications," Cell Reports Physical Science, 2(5), 100435.
W. Ma#, Y. Li#, C. Chao, C. Tso, B. Huang*, W. Li*, S. Yao*, 2021, "Solar-assisted icephobicity down to -60 'C with superhydrophobic selective surfaces," Cell Reports Physical Science, 2(3), p.100384.
W. Li, G. Yu, Z. Yu, 2020, "Bioinspired heat exchangers based on triply periodic minimal surfaces for supercritical CO2 cycles
On Improving Full-Coverage Effusion Cooling Efficiency by Varying Cooling Arrangements and Wall Thickness in Double Wall Cooling Application," ASME Transactions-Journal of Heat Transfer, 141(4), p. 042201.
W. Li, X. Lu, X. Li, J. Ren, H. Jiang, 2019, "Wall Thickness and Injection Direction Effects on Flat Plate Full-Coverage Film Cooling Arrays: Adiabatic Film Effectiveness and Heat Transfer Coefficient
Experimental Investigation of Wall Thickness and Hole Shape Variation Effects on Full-Coverage Film Cooling Performance for a Gas Turbine Vane
A Novel Method for Designing Fan-Shaped Holes with Short Length-To-Diameter Ratio in Producing High Film Cooling Performance for Thin-Wall Turbine Airfoil," ASME Transactions-Journal of Turbomachinery, 140(9), p. 091004
W. Li, W. Shi, X. Li, J. Ren, H. Jiang, 2017, "On the Flow Structures and Adiabatic Film Effectiveness for Simple and Compound Angle Hole with Varied Length-to-Diameter Ratio by Large Eddy Simulation and Pressure Sensitive Paint Techniques
Effect of Reynolds Number, Hole Patterns, and Hole Inclination on Cooling Performance of an Impinging Jet Array, Part I: Convective Heat Transfer Results and Optimization," ASME Transactions-Journal of Turbomachinery, 139(4), p. 041002.
W. Li, L. Yang, X. Li, J. Ren, H. Jiang, 2017, "Effect of Reynolds Number, Hole Patterns, Target Plate Thickness on Cooling Performance of an Impinging Jet Array, Part II: Conjugate Heat Transfer Results and Optimization," ASME Transactions-Journal of Turbomachinery, 139(10), p.101001.

Last modified on 30 Nov, 2021