The invention discloses a low-pressure
turbine blade profile aerodynamic design method based on optimization of an optimal
load distribution model, and the method comprises the steps: generating a blade profile geometric sample according to a given blade profile parameter value range and low-dimensional aerodynamic design parameters, calculating the optimal
load distribution through CFD when the total pressure loss of the blade profile is minimum, and generating a blade profile
database; constructing an optimal
load distribution model based on a multi-output
Gaussian process and a deep neural network, and training the optimal load
distribution model by minimizing a marginal likelihood
loss function according to the training samples in the blade profile
database to obtain a hyper-parameter group in the optimal load
distribution model; and according to the trained optimal load
distribution model, target optimal load distribution of the target low-dimensional aerodynamic design parameters is calculated, and an optimal aerodynamic blade profile corresponding to the target optimal load distribution is calculated by using a blade profile inverse design model. According to the design method, the precision and efficiency of pneumatic design of the
turbine blade profile can be improved, and the
geometric design period of the
turbine blade profile can be shortened.