In the asymmetric flow field of typhoon A(typhoon B),the azimuthal phase of asymmetric gyres due to the linear beta effect is opposite to (the same with) that of .

Now it was generalized to nonaxisymmetric vortices case.

Then asymmetrical vortex breakdown flows with M_∞=0.

Research of asymmetric vortex characteristic about forebody of slender wing and body;

When a fighter aircraft or missile flies at high angle of attack(AOA),asymmetric vortexes are produced from the forebody and induce strong side force and yawing moment.

In order to study the Reynolds number effects with zonal behaviors on the asymmetric vortex flow over slen- der body,the experimental investigations were carried out in D-4 Low Speed wind tunnel of BUAA and the NF-3 wind tun- nel of Northwest Polytechnic University(NPU)on a 3D pointed tangent ogive/cylinder model with f meness ratio 6 in Reynolds numbers range 0.

Experimental study of Reynolds numbers effect on asymmetric vortices and their aerodynamic characteristics over a slender body;

The pressure fluctuation on both sides along the axis of the cylinder were compared to the cross-section vortices structure, which educed by the measurement of mean pressure based on the physical model of asymmetric vortices.