Experimental research on the phenomenon of reverse transition in the boundary layer under a heated plate is presented, and the mechanism of reverse transition is also explained.

Nonlinear dynamics parameters, such as correlation dimension, maximum Lyapunov exponent and Kolmogorov entropy, which reflect the chaos characteristics of flow field are calculated with the time series of instantaneous velocity during reverse transition.

In the two-dimensional wind tunnel, systematic experimental researches were carried out on the phenomenon of reverse transition on a heated plane with stable density stratification.

Visualization study on the flow structures in the transitional boundary layer under an adverse pressure gradient;

Study of bypass transition mechanisms in the boundary layer of blunt bodies;

Improving the aerodynamic performance of low Reynolds number airfoils in oscillating freestream with forced transition method;

Application of gamma-theta transition model to flows around airfoils

Based on Menter s SST k-ω turbulence model coupled with Langtry-Menter transition model,the control mechanism of jet-flap,an active flow control method for PAK-B low-pressure turbine blade profile,was numerically investigated under different flow conditions including different cascade inlet Reynolds numbers,free stream turbulence levels,and cascade outlet Mach numbers.

The M-L transition model can somewhat accurately predict the generation and developm.

Improving the aerodynamic performance of low Reynolds number airfoils in oscillating freestream with forced transition method;

The way to introduce controlled disturbance into supersonic boundary-layer in transition experiments;