The application relates to an aerodynamic profile suitable for a wind tunnel and a design method thereof, and belongs to the technical field of
aviation aerodynamic wind tunnel tests. The front end surface of the aerodynamic profile is a square section, the rear end surface of the aerodynamic profile is a
circular section, the middle part of the aerodynamic profile is a transition section, and the front and rear sections are connected through the change of the section shape from front to back. The research and development purpose is to provide a novel aerodynamic profile design method for the transition from a square section to a
circular section, the flow field can be smoothly transitioned from a square to a circle, the influence on the flow
field quality is minimized, the pressure loss is reduced, and the method of
rounding the right angle and gradually increasing the
rounding radius is adopted to realize the smooth transition from the square section to the
circular section. The circular arc curve is gradually lengthened, the right angle side is gradually shortened, and finally the profile line is completely changed into a circular shape. The transition mode is natural and smooth, the change is gentle, the aerodynamic performance is good, and the interference on the flow field due to the change of the section shape can be obviously reduced.