The aero-engine particle separator parameterization design method comprises the following specific steps that firstly, air parameters of dust-containing
airflow are determined, and meanwhile material parameters of sand dust are determined; 2, designing initial geometric parameters of the particle separator; 3, a parameter optimization range is given, an optimization
algorithm is utilized, the total loss
delta P serves as an optimization target,
loss minimization serves as an optimization direction, new
delta P is compared with original loss, and a new geometric parameter combination with the minimum total loss is obtained; and 4, modeling by using a new geometric parameter combination, checking calculation by using three-
dimensional simulation, carrying out iteration with the step 3 according to the
simulation result satisfaction degree, and otherwise, finishing the design. According to the method, the parameterization design method is adopted, the main geometric parameters and the performance parameters of the separator are associated, the loss model is formed, the model is optimized and solved, the geometric parameter combination with the minimum loss is obtained, the experience dependence degree of the prior art can be relieved, and the design efficiency is greatly improved.