The invention discloses a curved surface
quadrilateral dominant grid generation method, device and equipment for an aircraft and a storage medium, and relates to the technical field of computational fluid
mechanics, and the method comprises the steps: creating a surface unstructured
grid based on surface grid generation parameters of a CAD file of the aircraft, carrying out the conformal mapping of the surface unstructured grid to a parameter domain plane, and calculating the vertex
compression ratio of each grid vertex; selecting the current starting point with the minimum
compression ratio and the maximum to-be-compared vertex in the
adjacency list, and determining the current to-be-processed vertex with the minimum
compression ratio in the adjacent vertexes and the advancing direction; determining to-be-processed
discrete points according to the current compression ratio and the coordinate information to generate a current isoline, if the current compression ratio does not exceed a threshold value, iteratively updating the current starting point, and skipping to the step of determining the current to-be-processed vertex again; the
discrete points are projected to the outer-layer isolines according to the isoline sequence, and the curved-surface
quadrilateral dominant grid is generated based on the distance proportion between each discrete point and the projection point, so that the generation efficiency of the curved-surface
quadrilateral grid is improved.