Calculation and designing the contour supported composit panel loaded with cross-section force

Aviation technics and technology


Аuthors

Dudchenko A. A.1*, Cuong L. K., Lur'e S. A.2**

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Institute of Applied Mechanics of Russian Academy of Science, IAM RAS, 32a, Leninskii av., Moscow, В-334, GSP-1, 119991, Russia

*e-mail: a_dudchenko@mail.ru
**e-mail: salurie@mail.ru

Abstract

In article calculation and designing he supported composit panel loaded with cross-section loading is considered. The solution is realized in the analytical form with use of V.Z.Vlasov’s variation method in series on displacements to design planes. The panel can be loaded by any cross-section force and have any conditions of fastening. The received solution is a basis for satisfaction of a condition of strength in a designing problem. Examples of the solution of a problem are resulted.

Keywords:

contour supported panel, a composit material, cross-section loading, V.Z.Vlasova's method.


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