The invention provides a design method of a blade
suction surface groove for controlling flow separation, which comprises the steps of: firstly, determining the initial position of the
initial point of a groove, the initial projection length of the groove on the molded line of a blade
suction surface and the initial function equation for describing the curved line of the groove; and secondly, optimizing the groove by adopting
genetic algorithm, wherein the initial position of the groove, the projection length of the groove on the molded line of the blade
suction surface and the initial function equation for describing the curved line of the groove are taken as optimization variables, and the static
pressure rise, the total pressure
recovery coefficient, the total pressure coefficient and the
airflow turning angle of a blade grid passage are taken as variables of the
fitness function in the
genetic algorithm, so that the optimization variable combination which can be maximize the
fitness function is taken as the modeling parameters of the groove. According to the design method, the flow in the blade grid passage can be improved, a burbling zone in the passage can be decreased or even eliminated, the efficiency and the total pressure
recovery coefficient of the passage are improved, the loss coefficient of the passage is reduced, the high
attack angle of the elementary blade type is improved, and the available
attack angle range of the elementary blade type is enlarged.