This invention relates to the field of
solid rocket motor technology, specifically to a method for strength analysis and modeling of
solid rocket motor casings. The steps are as follows: S1, import the 3D model of the
metal casing into
ANSYS software; S2, perform a series of
cutting, merging, and deleting operations on the 3D model to convert it into a 2D model; S3, assign material properties to the 2D model and divide it into
quadrilateral meshes to obtain a 2D finite
element model; S4, based on the coordinate characteristics of the geometric model, select the inner hole line numbers of the front and rear joints of the casing, and sequentially select the inner line groups of the casing according to "points attached to lines" and "lines associated with points," thereby determining the application position of the
pressure load; S5, rotate the 2D finite
element model by a certain angle to expand it into a 3D model; S6, after applying the
pressure load, solve the problem and extract the
equivalent stress to evaluate the structural strength of the
metal casing. This invention reduces the difficulty of
simulation, significantly improves work efficiency, and has good versatility.