The invention discloses an
asymmetry degree controllable three-dimensional shape transition spray
pipe design method and related equipment, and the method comprises the steps that a maximum thrust annular spray
pipe restrained by a neutral flow surface is constructed as a mother flow field, and the neutral flow surface is a flow surface with opposite
airflow radial velocity directions on the two sides in the maximum thrust annular spray
pipe; mapping an elliptical inlet contour and a rectangular outlet contour of the three-dimensional transition
nozzle to be designed to an inlet ring and an outlet ring of the mother flow field, and designing the three-dimensional transition
nozzle on the premise that the area of the rectangular outlet contour is constant, the shape of the maximum thrust annular spray pipe is changed by adjusting the
aspect ratio of the rectangular outlet contour or the
radius of an inlet ring of the mother flow field, streamline tracking and flow pipe fusion are carried out based on the maximum thrust annular spray pipe with the changed shape, and the three-dimensional transition spray pipe with different
asymmetry degrees is obtained. The invention aims to solve the problems that according to an existing three-dimensional shape transition spray pipe design method, a design frame has a fixed asymmetrical characteristic, the
asymmetry degree regulation and control capability is lacked, and inlet and outlet positions and section shapes are difficult to flexibly match according to different task requirements; and the problem that the
nozzle structure meeting the use requirement is difficult to design in a multi-configuration aircraft platform according to the specific configuration requirement is solved.