The behavior of the system is a non-cylindrical reservoir – a liquid in the reserve frequency range

Journal Title: Механіка гіроскопічних систем - Year 2018, Vol 0, Issue 36

Abstract

Modern potentials of analytical methods, based on variational algorithms, allow studying the nonlinear dynamics problems of reservoirs with liquid within the framework of models of the system components combined motion and non-cylindrical shape reservoirs which are difficult to study. The results of the experiments revise some of the previously obtained theoretical data, e.g. about system behavior in a vicinity of the resonance, where oscillations modulation results in the property that even for durable time intervals the system does not pass into a steady mode of oscillations. Behavior of the reservoir – liquid system under force disturbance of translational motion in the above-resonance range of variation of frequencies is considered. The reservoir in the form of the revolution body e.g. spherical and hyperboloid reservoirs is considered. Distinctions of wave generation manifestation in comparison with below-resonance and near-resonance disturbance modes are shown. It is noted that surface wave generation is accompanied by considerable manifestation of oscillations modulation. Qualitative comparison of the obtained results with experimental data is presented.

Authors and Affiliations

O. S. Lymarchenko, Yu. А. Slusarchuk, О. Yu. Parankina

Keywords

Related Articles

ВЛИЯНИЕ КОМПЛЕКСНОГО ЛЕГИРОВАНИЯ Si И В НА СТРУКТУРУ И СВОЙСТВА КВАЗИКРИСТАЛЛИЧЕСКИХ СПЛАВОВ Al–Cu–Fe

<p>В работе исследованы структура и фазовый состав квазикристаллических сплавов Al–Cu–Fe, комплексно легированных 4–7 ат. % кремния и 1–3 ат. % бора. Подтверждено образование стабильной квазикристаллической ψ-фазы. Изуче...

ЗМЕНШЕННЯ ОПОРУ ТЕРТЯ ЛІТАКА ШЛЯХОМ МІКРОВИДУВУ ЧЕРЕЗ ПРОНИКНІ ДІЛЯНКИ ПОВЕРХНІ КРИЛА

<strong><strong></strong></strong>На прикладі крила літака Ан-124 було досліджено переваги та особливості впливу на опір літака мікровидуву повітря через пористу ділянку обтічної поверхні. Проведено параметричний аналіз...

Robust supersonic aircraft control system

The motion trajectories of an aircraft with solid fuel engine cause a rapid change in flight altitude and velocity. Therefore, for such objects, the application of stationary control laws, obtained without taking into ac...

Type influence by fighting of an aircraft design of "kachka" schedule on the distribution of aerodynamic work on the wing

The purpose of the work is to determine the stress-strain state of the centrifugal turbomachine wheel , in which, when we made calculating in one case, the wheel was considered as constructively orthotropic disk, in th...

Analysis of influence design parameters ejector pipe at the detonation specifications engine

The engines that use a detonation cycle have greater thermal efficiency than engines with constant-pressure combustion cycle. The mechanisms of ejector augmentation are evident in secondary air entrainment. The impulse c...

Download PDF file
  • EP ID EP508735
  • DOI -
  • Views 127
  • Downloads 0

How To Cite

O. S. Lymarchenko, Yu. А. Slusarchuk, О. Yu. Parankina (2018). The behavior of the system is a non-cylindrical reservoir – a liquid in the reserve frequency range. Механіка гіроскопічних систем, 0(36), 5-10. https://europub.co.uk/articles/-A-508735