The invention discloses a structural finite-element parametric modeling method applicable to a
grating-configuration
rudder surface. According to the method, a mapping transformation method based on a finite
element model and a parametric approach to achieving conversion from two-dimensional mesh parameterization division to three-dimensional appearance expansion are adopted. The method includes the steps of specifically conducting two-dimensional plane projection on the
grating-configuration
rudder surface, extracting characteristic parameters, and conducting two-dimensional parameterization division; building a mapping relation between a two-dimensional finite element mesh and a three-dimensional finite element mesh, designing a
numbering rule for finite element mesh points, and achieving conversion from the two-dimensional mesh to the three-dimensional appearance expansion; by means of a high-level computer language program, implementing the structural finite-element parametric modeling procedures for the
grating-configuration
rudder surface. By using the method, in a
conceptual design phase or a preliminary
design phase, the structural modeling efficiency can be greatly increased, the costs of time and manpower are low, parameters of self-compiled programs can be adjusted quickly, analysis applicability is high, the obtained model is applicable to analytical calculation of
structural vibration,
structural dynamics and the like, and the method is applicable to grating-configuration rudder surfaces and grating-configuration airfoils.