Analyze of the properties of the submerged triangle wing for adjusting shallow supercritical flow;

Numerical simulation of unsteady flows past a delta wing using a 3-D vortex method;

Effects of free stream local disturbance on delta wing aerodynamics;

Numerical simulation to effects of trailing edge jet on delta wing vortices;

The effects of Gurney flap on double delta wing aerodynamic performance in low speed wind-tunnel tests;

Experimental investigation of the vortex characteristic over 75°/45°double delta wing;

Compared with a delta wing aircraft, the double delta wing configuration has better aerodynamic performance at high angles of attack.

Experimental study on pressure measurement distribution of double-delta wings;

The vortex visualization and surface pressure distribution for a 75°/45°double-delta wing were carried out in the water tunnel and in the low speed wind tunnel of BUAA.

The vortex visualization and surface pressure distribution measurement for a 75°/60° double-delta wing were carried out in the water tunnel and in the low speed wind tunnel of BUAA.