Two-dimensional numerical simulation study have been conducted on flow and heat transfer of cooling configuration for trailing edge of turbine vane, the effects of the length of trailing edge (L/H), outlet air angle (a), the ratio of the coolant to mainstream mass flow (M) and the coolant Reynolds number (Re) on cooling efficiency were investigated.

Effect of different clapboards structure in turbine blade trailing edge complex passages on heat transfer characteristics;

Different structure diaphragm plates in complex passages of turbine blade trailing edge;

The experiment mainly aimed at to investigate the effect of different aperture in different clapboard structure in the turbine blade trailing edge complex passages on heat transfer and pressure drop characteristics.

Parametric design of turbine blades based on feature modeling;

Research on Fatigue Life of Large Gas Turbine Blades;

The single crystal Ni-base superalloys were widely used for manufacturing advance gas turbine blades,but the ignored weakness of these alloys to date is that the extent of primary creep at intermediate temperature is much higher than that at high temperature.

Error Analysis on Turbine Blade;

Displacement transfer with the mesh deformation method in multidisciplinary optimization of turbine blades;

Turbine blade design and optimization based on the combination means of parametric-Bezier curve;