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Titlebook: Vortex Processes and Solid Body Dynamics; The Dynamic Problems Boris I. Rabinovich,Valeryi G. Lebedev,Alexander I Book 1994 Springer Scienc

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书目名称Vortex Processes and Solid Body Dynamics
副标题The Dynamic Problems
编辑Boris I. Rabinovich,Valeryi G. Lebedev,Alexander I
视频video
丛书名称Fluid Mechanics and Its Applications
图书封面Titlebook: Vortex Processes and Solid Body Dynamics; The Dynamic Problems Boris I. Rabinovich,Valeryi G. Lebedev,Alexander I Book 1994 Springer Scienc
描述... a wise man knows all things in a manner in which this is possible, not, however, knowing them individually. Aristotle. Metaphysics * The problem of consideration of vortex fields‘ influence on solid body dynamics has a long history. One constantly comes upon it in flight dynamics of airplanes, helicopters, and other flying vehicles (FV) moving in the atmosphere, in dynamics of ships with hydrofoils, and in dynamics of rocket carriers (RC) and spacecrafts (SC) with liquid-propellant rocket engines (LPRE), that are equipped with special damping devices and other structural elements inside fluid tanks. Similar problems occur when solving problems related to attitude control and stabilization of artificial Earth satellites (AES) and spacecrafts with magnetic (electro­ magnetic) systems, in conducting elements of which eddy currents are induced while control of those vehicles‘ angular position. It is also true with special test facilities for dynamic testing of space vehicles and their systems, with modern high-speed magnetic suspension transport systems (those based on the phenomenon of ‘magnetic levitation‘), with generators having rotors carried in ‘magnetic bearings‘, and so on.
出版日期Book 1994
关键词Counter; control; dynamics; model; satellite; solid; stability; vehicle dynamics
版次1
doihttps://doi.org/10.1007/978-94-011-1038-9
isbn_softcover978-94-010-4452-3
isbn_ebook978-94-011-1038-9Series ISSN 0926-5112 Series E-ISSN 2215-0056
issn_series 0926-5112
copyrightSpringer Science+Business Media Dordrecht 1994
The information of publication is updating

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Introduction,system. Particular cases are artificial Earth satellites (AES), rocket carriers (RC), and vehicles with magnetic levitation systems (see V.I.Bocharov and V.D.Nagorsky (Ed.) [9], T.I.Katsan, V.G.Lebedev, and A.I.Mytarev [35], Yu.A.Nikitenko .. [71], K.H.Brock .. [14], E.Gottzein [25], E.Gottzein, L.M
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Mathematical Models of High Electrical Conductivity Ferromagnetic Elements with Eddy Currents,ductivity (skin effect), is a traditional one for electrical engineering and is well studied. Practical aspects of this problem has determined two specific features of its statement, which are completely described in literature (see, e.g. N.N.Fedorov [20]):
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Mathematical Models of Stabilized Objects with Compartments Containing Vortex Low-Viscous Liquid,ncy range of natural oscillations of liquid fuel components partially filling the tanks. This relates to RC as well as SC. Conventionally a way of complete or, at least, partial solution of the problem is to apply more and more developed and complicated dampers of liquid oscillations. This, in turn,
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Analytical and Numerical Methods of Dynamics Investigation of Vehicles Described by Vortex Models,odels are used throughout the book as a tool for the analysis of dynamic properties of vehicles described by them, those properties being determined from both experimental research and mathematical simulation of perturbed motion. But before proceeding to direct usage of those models, it is necessary
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Experimental Verification of Mathematical Models for Eddy Currents and Vortex Motions of Liquid,ome mathematical research aspects of those equation solutions. Mathematical models of eddy currents in HECF elements and vortex motions of LV liquid lying in the foundation of the appropriate integrodifferential equations were obtained based on a number of heuristic considerations and simplifying as
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