The invention discloses a structure surface grid automatic generation method based on topology filling, and relates to the technical field of
aerospace engineering simulation and grid generation. The method comprises the following steps: carrying out intelligent component
subdivision on a three-dimensional CAD model to obtain components with semantic tags and geometric contours of the components; sequentially executing ordered topology filling on each component according to a preset sequence, cooperatively adjusting intersection edge points of adjacent components to ensure
grid connection, and generating a topological line; projecting the topological line to the surface of the model for calibration; performing
adaptive interpolation on the projected topological line based on the model curvature and the
simulation working condition to generate
point cloud data; generating an initial
quadrilateral grid based on the
point cloud; the initial grid nodes are projected to the surface of the model again,
quality optimization is carried out, and a final grid is output. According to the method, the end-to-end automatic generation from the CAD model to the high-quality surface grid is realized, the manual intervention is eliminated, the natural matching of the grids between the parts is ensured, and the grid generation efficiency and quality are remarkably improved.