Hongzhou Xu

TurbineVane Endwall Film Cooling Comparison From Five Film-Hole Design Patterns and Three UpstreamInjection Angles

Chao-Cheng Shiau, İzzet Şahin, Nian Wang et al. · Journal of Thermal Science and Engineering Applications · 2018 · 46 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effects of Upstream Step Geometry on Axisymmetric Converging Vane Endwall Secondary Flow and Heat Transfer at Transonic Conditions

Zhigang Li, Luxuan Liu, Jun Li et al. · Journal of Turbomachinery · 2018 · 24 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effects of tip gap on transonic turbine blade heat transfer characteristics with pressure side film cooling

Hallie Collopy, Phillip M. Ligrani, Hongzhou Xu et al. · International Journal of Heat and Mass Transfer · 2022 · 24 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection

Nian Wang, Chao-Cheng Shiau, Je-Chin Han et al. · International Journal of Heat and Mass Transfer · 2018 · 19 citations

Engineering, Mechanical Engineering, Computational Fluid Dynamics +11

Effects of pressure side film cooling hole placement and condition on adiabatic film cooling effectiveness characteristics of a transonic turbine blade tip

Hallie Collopy, Phillip M. Ligrani, Hongzhou Xu et al. · International Journal of Heat and Mass Transfer · 2022 · 19 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17