Analysis of structural and technological solutions of folding fins with the requirements of aeroelastic stability.
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Aviation technics and technology
Аuthors
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.Download