The invention provides a calculation method of the
bearing capacity of a reinforced
wall plate and belongs to the field of strength analysis of aircraft structures. According to the technical scheme, the calculation method is an
axial compression loading action based calculation method of the effective width of buckling of a
skin. Stiffness reduction is performed through modification of the cross section area and the
moment of inertia of a
stringer in a finite
element model which is formed by plate beam units after the buckling of the
skin is produced, stress analysis of a structure is performed by a
linear iteration solution method of load loading steps, comparison is performed on the working stress of the
stringer in a calculation result and the allowable limiting stress of a
stringer and
skin combined structure, the allowable limiting stress serves as a damage standard and is solved based on an
engineering method, and accordingly the
bearing capacity of the structure is obtained. Compared with the traditional full housing model, a calculation method model is a plate beam
unit model, the geometric nonlinearity and contact
problem solution which is large in time consumption and difficult to converge is replaced by the linear solution, and accordingly the modeling time consumption is small, the calculation speed is high, and the requirements for the professional quality of the
computer hardware and analysis staff are low.