The invention relates to a vortex generator structure for suppressing boundary layer separation under the action of shock
waves. One or more vortex generator structures arranged in parallel are arranged, so that a flow control device is obtained. The flow control device aims at improving separation-resistant capacity of boundary
layers in ultrasonic gas flowing under the action of the shock
waves. A vortex generator is of a tetrahedral structure basically and is located in an interference region upstream boundary layer where
shock wave boundary
layers interact, the distance between a vortex generator
trailing edge and an interference region
initial point is 15-30 times of a boundary
layer thickness when no control exists in the position where the vortex generator is located, the height of the vortex generator
trailing edge is 0.3-0.8 time of a boundary
layer thickness when no control exists in the position where the vortex generator is located, the length is directly proportional to the
trailing edge height of the vortex generator, the specific value of the length to the trailing edge height is 5 to 10, the width is directly proportional to the trailing edge height of the vortex generator, the specific value of the width to the trailing edge height is 2 to 4, the distance between vortex generators is directly proportional to the trailing edge height of the vortex generator, and the specific value of the distance to the railing edge height is 6 to 10. The vortex generator structure is suitable for supersonic flow fields where the shock
waves induce separation of boundary
layers.