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.