The invention belongs to the technical field of aircraft design, and discloses an airfoil structure
virtual test loading
analysis method based on digital
simulation, which comprises the following steps of: firstly, carrying out detail finite
element modeling according to an airfoil structure digital model, the attribute of the connecting piece is calculated and assigned according to the simplification principle of a bush unit, and the center coordinate of a loading point is determined according to the position of an
adhesive tape or a pull-press block in the test partial load scheme;
simulation analysis is carried out after loading is completed, loading is carried out according to the
initial load direction, the load is discretized to a single loading point, then the single loading point is recorded, coordinates of a center node of the loading point and coordinates of an
actuator connecting point after deformation are obtained, then the direction of a loading vector is obtained, all loading points of the
simulation model are loaded, and a simulation result is obtained. After analysis is carried out, linear / nonlinear
static force, buckling and post-buckling calculation is carried out; analyzing a stress-strain identification test risk position according to a calculation result, and pasting a
strain gauge. The method can guide the design of a loading scheme in an airfoil structure test, improves the calculation precision, recognizes the test risk, avoids the loss of a test piece, and reduces the test cost.