Abstract

The article discusses the new type of plywood panel for low-rise building. Сalculating methods for the plywood panels are considered according with the codes of rules and the method for calculating sandwich panels with a honeycomb, proposed by Soviet scientists for aviation structures.

Highlights

  • IntroductionIn the post-Soviet space, the plywood panels (figure 1) are widely used as wall and overlapcovering panels

  • In the post-Soviet space, the plywood panels are widely used as wall and overlapcovering panels

  • The main advantage of such panels is a high degree of factory readiness, but a significant disadvantage is the low degree of form stability of the main carrying ribs

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Summary

Introduction

In the post-Soviet space, the plywood panels (figure 1) are widely used as wall and overlapcovering panels. They first appeared in the 40s of the XX century. Layered structures are calculated from two groups of limiting states: by their carrying capacity (strength or stability) and by deformation. When calculating the second limiting state, the ultimate deflections of the structures are taken in accordance with the values, given in Appendix E [5] and are equal to l/125. When calculating the second limit state (in terms of deformations), the ultimate deflections of the structures are taken in accordance with the values given in Appendix E [5] and are 1/125

Methods
Calculation by the method of calculating the honeycomb aggregate
Conclusions
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