The invention belongs to the technical field of engine
simulation, and relates to an engine variable-dimension numerical
simulation method and device, and the method comprises the steps: calculating the parameters of a contra-rotating
propeller fan based on a contra-rotating
propeller fan three-dimensional
lift line model; determining the axial average speed of air flow at the inlet of the air inlet; determining section parameters at an inlet of the air
inlet channel; calculating section parameters at an outlet of the air inlet; the air flow at the outlet of the air
inlet channel is divided into two parts, one part of the air flow is distorted, the other part of the air flow is distortionless, and section parameters at the outlet of the low-pressure compressor are determined through mixing at the outlet; calculating inlet and outlet section parameters of each component according to the zero-dimensional model of each component of the engine; a
balance equation is constructed according to circulation of
airflow in all parts of the engine; constructing a
balance equation according to the balance relation between the shaft power and the torque output by the free
turbine and the power and the torque calculated by the contra-rotating
propeller fan three-dimensional
lift line model; the
balance equation is iteratively solved to determine an initial
guess value, and when iteration converges, engine performance is calculated. The method is high in
simulation precision and high in speed.