61 research outputs found

    Modeling of Formation of Nanostructured Metal Surfaces by Electrodeposition through a Monolayer Colloidal Crystal Mask

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    AbstractElectrochemical deposition is a feasible and well-controlled method for the formation of various micro- and nanostructures. A rich variety of periodical nanostructures of functional materials with multi-shaped and tunable morphologies can be fabricated by the electrochemical deposition, in particular, using monolayer colloidal crystal (MCC) mask. A mathematical model of the mass-transfer processes and deposit surface evolution during the metal electrodeposition through MCC mask is presented. The mathematical model involves the equations for the potential and deposit surface evolution. The problem was solved numerically by the boundary element method, and the β€œLevel Set” method. The numerical experiments were used to study the effect of parameters, which characterize the mask geometry and the process conditions, on the initial distribution of current density over the deposit surface and the variation of current density distribution in the course of the deposition

    Effect of Current Efficiency on Electrochemical Micromachining by Moving Electrode

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    AbstractIn this work, the effect of current efficiency on the electrochemical micromachining by moving electrode is studied theoretically. The Laplace equation for the electric potential and the equation of workpiece surface evolution are used as the mathematical model of the process. A new scheme of solution of free boundary problem for steady-state electrochemical micromachining is proposed. According to the scheme, the initial approximation of the workpiece surface is prescribed. In the course of modeling, the workpiece surface moves in the normal direction at a rate proportional to the discrepancy of the steady-state condition. The effect of various dependences of current efficiency on the local current density is analyzed. As a result of simulation, the dependences of the shape and sizes of machined surface on the current efficiency and the machining parameters are obtained

    Modeling of the Induced Resonant Torquesduring the Motionof an Asymmetric Spacecraft in the Atmosphere

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    Π’ настоящСй Ρ€Π°Π±ΠΎΡ‚Π΅ исслСдуСтся нСуправляСмоС Π΄Π²ΠΈΠΆΠ΅Π½ΠΈΠ΅ асиммСтричного космичСского Π°ΠΏΠΏΠ°Ρ€Π°Ρ‚Π° Π² атмосфСрС. ΠŸΡ€Π΅Π΄ΠΏΠΎΠ»ΠΎΠΆΠΈΠΌ, Ρ‡Ρ‚ΠΎ космичСский ΠΊΠΎΡ€Π°Π±Π»ΡŒ - это Ρ‚Π²Π΅Ρ€Π΄ΠΎΠ΅ Ρ‚Π΅Π»ΠΎ с ΠΌΠ°Π»Ρ‹ΠΌΠΈ массово-ΠΈΠ½Π΅Ρ€Ρ†ΠΈΠΎΠ½Π½Ρ‹ΠΌΠΈ ΠΈ ΠΌΠ°Π»Ρ‹ΠΌΠΈ аэродинамичСскими асиммСтриями. ЦСлью исслСдования являСтся ΠΈΠ·ΡƒΡ‡Π΅Π½ΠΈΠ΅ матСматичСских ΠΌΠΎΠ΄Π΅Π»Π΅ΠΉ ΠΌΠ°Π»Ρ‹Ρ… мСханичСских ΠΌΠΎΠΌΠ΅Π½Ρ‚ΠΎΠ², Π½Π°Π²Π΅Π΄Ρ‘Π½Π½Ρ‹Ρ… Π³Π»Π°Π²Π½Ρ‹ΠΌ рСзонансом Π² нСрСзонансных областях двиТСния. Π’ ΠΏΡ€Π΅Π΄Π»Π°Π³Π°Π΅ΠΌΠΎΠΌ исслСдовании Ρ€Π΅ΡˆΠ°ΡŽΡ‚ΡΡ ΡΠ»Π΅Π΄ΡƒΡŽΡ‰ΠΈΠ΅ Π·Π°Π΄Π°Ρ‡ΠΈ: ΠΏΠΎΠ»ΡƒΡ‡Π΅Π½Ρ‹ выраТСния для Π½Π°Π²Π΅Π΄Ρ‘Π½Π½ΠΎΠ³ΠΎ мСханичСского ΠΌΠΎΠΌΠ΅Π½Ρ‚Π°, ΠΎΠΏΡ€Π΅Π΄Π΅Π»Π΅Π½Ρ‹ Π²Π΅Π»ΠΈΡ‡ΠΈΠ½Ρ‹ областСй дСйствия Π΄Π°Π½Π½ΠΎΠ³ΠΎ ΠΌΠΎΠΌΠ΅Π½Ρ‚Π°. Автор ΠΏΡ€ΠΈΡ…ΠΎΠ΄ΠΈΡ‚ ΠΊ Π²Ρ‹Π²ΠΎΠ΄Ρƒ, Ρ‡Ρ‚ΠΎ ΠΏΡ€ΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠ΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° усрСднСния позволяСт ΠΈΡΡΠ»Π΅Π΄ΠΎΠ²Π°Ρ‚ΡŒ мСханичСский ΠΌΠΎΠΌΠ΅Π½Ρ‚, Π½Π°Π²Π΅Π΄Ρ‘Π½Π½Ρ‹ΠΉ рСзонансом. Π”Π°Π½Π½Ρ‹ΠΉ ΠΌΠΎΠΌΠ΅Π½Ρ‚ способствуСт Π·Π½Π°Ρ‡ΠΈΡ‚Π΅Π»ΡŒΠ½ΠΎΠΉ ΡΠ²ΠΎΠ»ΡŽΡ†ΠΈΠΈ ΡƒΠ³Π»ΠΎΠ²ΠΎΠΉ скорости вращСния космичСского Π°ΠΏΠΏΠ°Ρ€Π°Ρ‚Π° Π² нСрСзонансных областях, ΠΏΡ€ΠΈΠ»Π΅Π³Π°ΡŽΡ‰ΠΈΡ… ΠΊ рСзонансу. This paper investigates an uncontrolledmotion of an asymmetric spacecraft in the atmosphere. Suppose that the spacecraft is a rigid body with small mass-inertial and small aerodynamic asymmetries. The aim of the research is to study of mathematical models of the small mechanical torques caused by the principal resonance. The proposed study solves the following problems: revealing specific features of the mechanical torque, determining the magnitude of a domain of activity of the torque. The author conclude that the application of the averaging method allow us to research the mechanical torque induced by the resonance. This torque results in a significant angular speed evolution of rotation of a spacecraft in the non-resonance areas adjacent to the resonance

    Modeling of the Secondary Resonance Effects in the Spherical Motion of a Rigid Body with Flywheels

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    ΠœΠ΅Ρ‚ΠΎΠ΄Ρ‹ асимптотичСского Π°Π½Π°Π»ΠΈΠ·Π° ΠΏΡ€ΠΈΠΌΠ΅Π½ΡΡŽΡ‚ΡΡ для исслСдования ΡΠ²ΠΎΠ»ΡŽΡ†ΠΈΡ двиТСния асиммСтричного Ρ‚Π²Ρ‘Ρ€Π΄ΠΎΠ³ΠΎ Ρ‚Π΅Π»Π° с ΠΌΠ°Ρ…ΠΎΠ²ΠΈΠΊΠ°ΠΌΠΈ. ΠŸΠΎΠΊΠ°Π·Ρ‹Π²Π°Π΅Ρ‚ΡΡ, Ρ‡Ρ‚ΠΎ влияниС ΠΌΠ°Π»Ρ‹Ρ… ΠΌΠΎΠΌΠ΅Π½Ρ‚ΠΎΠ², Π²ΠΎΠ·Π½ΠΈΠΊΠ°ΡŽΡ‰ΠΈΡ… Π² Ρ€Π΅Π·ΡƒΠ»ΡŒΡ‚Π°Ρ‚Π΅ смСщСния Ρ†Π΅Π½Ρ‚Ρ€Π° масс ΠΈ ΠΌΠ°Π»Ρ‹Ρ… ΡƒΠΏΡ€Π°Π²Π»ΡΡŽΡ‰ΠΈΡ… ΠΌΠΎΠΌΠ΅Π½Ρ‚ΠΎΠ² ΠΎΡ‚ ΠΌΠ°Ρ…ΠΎΠ²ΠΈΠΊΠΎΠ², ΠΏΡ€ΠΈΠ²ΠΎΠ΄ΠΈΡ‚ ΠΊ возникновСнию Π½Π΅Π»ΠΈΠ½Π΅ΠΉΠ½Ρ‹Ρ… рСзонансных ΡΠ²ΠΎΠ»ΡŽΡ†ΠΈΠΎΠ½Π½Ρ‹Ρ… эффСктов. ЦСлью этой Ρ€Π°Π±ΠΎΡ‚Ρ‹ являСтся ΠΈΠ·ΡƒΡ‡Π΅Π½ΠΈΠ΅ рСзонансных эффСктов Π² сфСричСском Π΄Π²ΠΈΠΆΠ΅Π½ΠΈΠΈ асиммСтричного Ρ‚Π²Ρ‘Ρ€Π΄ΠΎΠ³ΠΎ Ρ‚Π΅Π»Π° с ΠΌΠ°Ρ…ΠΎΠ²ΠΈΠΊΠ°ΠΌΠΈ. ΠŸΡ€ΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠ΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈΠ½Ρ‚Π΅Π³Ρ€Π°Π»ΡŒΠ½Ρ‹Ρ… ΠΌΠ½ΠΎΠ³ΠΎΠΎΠ±Ρ€Π°Π·ΠΈΠΉ ΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° усрСднСния ΠΏΠΎΠ·Π²ΠΎΠ»ΠΈΠ»ΠΎ ΠΈΡΡΠ»Π΅Π΄ΠΎΠ²Π°Ρ‚ΡŒ ΡƒΠΊΠ°Π·Π°Π½Π½Ρ‹Π΅ рСзонансныС эффСкты. УсрСднённыС уравнСния ΠΏΠΎΠΊΠ°Π·Π°Π»ΠΈ, Ρ‡Ρ‚ΠΎ рСзонансныС эффСкты ΠΌΠΎΠ³ΡƒΡ‚ ΠΏΡ€ΠΈΠ²ΠΎΠ΄ΠΈΡ‚ΡŒ Π»ΠΈΠ±ΠΎ ΠΊ рСгулярной прСцСссии, Π»ΠΈΠ±ΠΎ ΠΊ Π΄Π»ΠΈΡ‚Π΅Π»ΡŒΠ½ΠΎΠΌΡƒ рСзонансу. The evolution of the motion of an asymmetric rigid body with flywheels can be explored by the methods of asymptotic analysis. It is shown, that the effect of small moments resulting from the displacement of the centre of mass and of small control moments from the flywheels lead to the emergence of non-linear resonance evolutionary effects. The aim of this work is to investigate the resonance effects in the spherical motion of the asymmetrical rigid body with flywheels. To explore these resonance effects we applied the method of integral manifolds and the averaging method. The averaged equations have shown that resonance effects may result in either regular precession or prolonged resonance
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