The application discloses a method for predicting the distribution of grid nodes of boundary lines of aircraft components and
anisotropy parameters, relates to the field of
automation and intellectualization of pre-
processing of computational fluid dynamics
simulation, and determines the geometric data of an aircraft CAD model, component semantic labels, calculation working conditions and each
boundary line. A trained multi-task graph neural
network model is used to intelligently classify the grid region types of the boundary lines, and isotropic or anisotropic classification results are obtained. Then, according to the classification results, the corresponding differential parameter prediction sub-network in the model is used to predict the corresponding grid control parameter set for each
boundary line. Finally, based on the parameter set, a
grid generator is driven to automatically generate high-quality surface grids. The application realizes
intelligent decision-making of the whole process from
semantic information to grid generation strategy and parameters, replaces the traditional method relying on artificial experience, and significantly improves the
automation degree, efficiency and grid quality consistency of CFD pre-
processing.