Analysis of structural and technological solutions of folding fins with the requirements of aeroelastic stability.

Aviation technics and technology


Аuthors

Nedelin V. G.

Dolgoprudny Research and Product Enteprise, DNPP, Sobina Av, 1, Dolgoprudny, 141700, Russia

e-mail: nedelinv@rambler.ru

Abstract

This article presents a general formulation and circuit of solution analysis design and technological solutions folding fins. The algorithm is based on the dependencies presented in [1], and it contains a number of changes due to structural features of the object.

Keywords:

reference theoretical solution; mathematical model; anisotropic plate; structural features; natural vibrations; aeroelasticity; flutter; divergence.


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