Aerospace Instrument-Making Annotation << Back ASSESSMENT OF FORMS OF DEPRESSION ON CARRYING CAPACITY OF THE AIRCRAFT WING PANELS WITH HOLE S.E. Zaytsev V.S. Safronov The article presents a model for evaluating the carrying capacity of the aircraft wing box with a hole and the results of numerical and theoretical studies. The influence of the submission form deflection on the bearing capacity. Selecting the appropriate waveform is the main point in the task at hand. For elastic arm valid form deformable axis must satisfy the conditions of the zero deflection and rotation angle in seals, as well as the maximum deflection and zero second derivative (the absence of torque) at the free end. The work shows the influence of the two forms of representation deflection satisfying the boundary conditions, the final result. As a method of solving the problem of energy МЕТОДЫ МОДЕЛИРОВАНИЯ КОМПЛЕКСОВ УПРАВЛЕНИЯ АВИАКОСМИЧЕСКОЕ ПРИБОРОСТРОЕНИЕ, 2015 г. № 6 23 method selected. When used to study the energy method is sufficient to approximate the function satisfies only the geometric boundary conditions, as power conditions are satisfied automatically. The results obtained on two ideas form the deflection compared with the results obtained by the finite element method. Obtained in this paper are calculated according to analytical. Key words: wing panel hole, deflection, load-bearing capacity, energy method. Contacts: E-mail: v.s.safronov@mail.ru Pp. 22-32.