.Surrogate-model-driven optimization of gas–solid boundary parameters for hypersonic nonequilibrium flows using experimental data:In preparation (*通讯作者)
.Aerodynamic impact of a random icing leading edge on thick aerofoil performance:in preparation (*通讯作者)
.Aerodynamic impact of a random eroded leading edge on thick aerofoil performance:in preparation (*通讯作者)
.Guiyu Cao, Christopher Vogel. Aerodynamic impact of a highly-eroded leading edge on FFA-W3-241 aerofoil performance:in revision
.Bayesian calibration of γ-Reθt transition model for hypersonic boundary layer:Chinese Journal of Aeronautics, accepted (*通讯作者)
.High-order gas-kinetic scheme for numerical simulations of wind turbine with nacelle and tower using ALM and IBM:Advances in Aerodynamics, accepted. (*通讯作者)
.Guiyu Cao, Zheni Fei, Christopher Vogel. Uncertainty quantification analysis in the blade element momentum method:Renewable Energy(2025): 123181.
.Guiyu Cao, Liang Pan, Kun Xu, Shiyi Chen. Double time-relaxation kinetic model for compressible turbulence modeling:Advances in Aerodynamics(2025) 7:19.
.Guiyu Cao, Liang Pan, Kun Xu, Shiyi Chen. High-order gas-kinetic scheme in general curvilinear coordinate for iLES of compressible wall-bounded turbulent flows:Journal of Scientific Computing, 101.2(2024): 1-27.
.Wenjin Zhao, Guiyu Cao*, Jianchun Wang*, Kun Xu. High-order gas-kinetic schemes with non-compact and compact reconstruction for implicit large eddy simulation:Computers and Fluids 256(2023) 105846. (*通讯作者)
