The Principle of Stationary Action1 D
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14 Mass on a Spring and Other Systems Described by Linear ODE
14 Mass on a spring and other systems described by linear ODE 14.1 Mass on a spring Consider a mass hanging on a spring (see the figure). The position of the mass in uniquely defined by one coordinate x(t) along the x-axis, whose direction is chosen to be along the direction of the force of gravity. Note that if this mass is in an equilibrium, then the string is stretched, say by amount s units. The origin of x-axis is taken that point of the mass at rest. Figure 1: Mechanical system “mass on a spring” We know that the movement of the mass is determined by the second Newton’s law, that can be stated (for our particular one-dimensional case) as ma = Fi, X where m is the mass of the object, a is the acceleration, which, as we know from Calculus, is the second derivative of the displacement x(t), a =x ¨, and Fi is the net force applied. What we know about the net force? This has to include the gravity, of course: F1 = mg, where g is the acceleration 2 P due to gravity (g 9.8 m/s in metric units). The restoring force of the spring is governed by Hooke’s ≈ law, which says that the restoring force in the opposite to the movement direction is proportional to the distance stretched: F2 = k(s + x), here minus signifies that the force is acting in the opposite − direction, and the distance stretched also includes s units. Note that at the equilibrium (i.e., when x = 0) and absence of other forces we have F1 + F2 = 0 and hence mg ks = 0 (this last expression − often allows to find the spring constant k given the amount of s the spring is stretched by the mass m). -
PHYSICS of ARTIFICIAL GRAVITY Angie Bukley1, William Paloski,2 and Gilles Clément1,3
Chapter 2 PHYSICS OF ARTIFICIAL GRAVITY Angie Bukley1, William Paloski,2 and Gilles Clément1,3 1 Ohio University, Athens, Ohio, USA 2 NASA Johnson Space Center, Houston, Texas, USA 3 Centre National de la Recherche Scientifique, Toulouse, France This chapter discusses potential technologies for achieving artificial gravity in a space vehicle. We begin with a series of definitions and a general description of the rotational dynamics behind the forces ultimately exerted on the human body during centrifugation, such as gravity level, gravity gradient, and Coriolis force. Human factors considerations and comfort limits associated with a rotating environment are then discussed. Finally, engineering options for designing space vehicles with artificial gravity are presented. Figure 2-01. Artist's concept of one of NASA early (1962) concepts for a manned space station with artificial gravity: a self- inflating 22-m-diameter rotating hexagon. Photo courtesy of NASA. 1 ARTIFICIAL GRAVITY: WHAT IS IT? 1.1 Definition Artificial gravity is defined in this book as the simulation of gravitational forces aboard a space vehicle in free fall (in orbit) or in transit to another planet. Throughout this book, the term artificial gravity is reserved for a spinning spacecraft or a centrifuge within the spacecraft such that a gravity-like force results. One should understand that artificial gravity is not gravity at all. Rather, it is an inertial force that is indistinguishable from normal gravity experience on Earth in terms of its action on any mass. A centrifugal force proportional to the mass that is being accelerated centripetally in a rotating device is experienced rather than a gravitational pull. -
Vibration and Sound Damping in Polymers
GENERAL ARTICLE Vibration and Sound Damping in Polymers V G Geethamma, R Asaletha, Nandakumar Kalarikkal and Sabu Thomas Excessive vibrations or loud sounds cause deafness or reduced efficiency of people, wastage of energy and fatigue failure of machines/structures. Hence, unwanted vibrations need to be dampened. This article describes the transmis- sion of vibrations/sound through different materials such as metals and polymers. Viscoelasticity and glass transition are two important factors which influence the vibration damping of polymers. Among polymers, rubbers exhibit greater damping capability compared to plastics. Rubbers 1 V G Geethamma is at the reduce vibration and sound whereas metals radiate sound. Mahatma Gandhi Univer- sity, Kerala. Her research The damping property of rubbers is utilized in products like interests include plastics vibration damper, shock absorber, bridge bearing, seismic and rubber composites, and soft lithograpy. absorber, etc. 2R Asaletha is at the Cochin University of Sound is created by the pressure fluctuations in the medium due Science and Technology. to vibration (oscillation) of an object. Vibration is a desirable Her research topic is NR/PS blend- phenomenon as it originates sound. But, continuous vibration is compatibilization studies. harmful to machines and structures since it results in wastage of 3Nandakumar Kalarikkal is energy and causes fatigue failure. Sometimes vibration is a at the Mahatma Gandhi nuisance as it creates noise, and exposure to loud sound causes University, Kerala. His research interests include deafness or reduced efficiency of people. So it is essential to nonlinear optics, synthesis, reduce excessive vibrations and sound. characterization and applications of nano- multiferroics, nano- We can imagine how noisy and irritating it would be to pull a steel semiconductors, nano- chair along the floor. -
LECTURES 20 - 29 INTRODUCTION to CLASSICAL MECHANICS Prof
LECTURES 20 - 29 INTRODUCTION TO CLASSICAL MECHANICS Prof. N. Harnew University of Oxford HT 2017 1 OUTLINE : INTRODUCTION TO MECHANICS LECTURES 20-29 20.1 The hyperbolic orbit 20.2 Hyperbolic orbit : the distance of closest approach 20.3 Hyperbolic orbit: the angle of deflection, φ 20.3.1 Method 1 : using impulse 20.3.2 Method 2 : using hyperbola orbit parameters 20.4 Hyperbolic orbit : Rutherford scattering 21.1 NII for system of particles - translation motion 21.1.1 Kinetic energy and the CM 21.2 NII for system of particles - rotational motion 21.2.1 Angular momentum and the CM 21.3 Introduction to Moment of Inertia 21.3.1 Extend the example : J not parallel to ! 21.3.2 Moment of inertia : mass not distributed in a plane 21.3.3 Generalize for rigid bodies 22.1 Moment of inertia tensor 2 22.1.1 Rotation about a principal axis 22.2 Moment of inertia & energy of rotation 22.3 Calculation of moments of inertia 22.3.1 MoI of a thin rectangular plate 22.3.2 MoI of a thin disk perpendicular to plane of disk 22.3.3 MoI of a solid sphere 23.1 Parallel axis theorem 23.1.1 Example : compound pendulum 23.2 Perpendicular axis theorem 23.2.1 Perpendicular axis theorem : example 23.3 Example 1 : solid ball rolling down slope 23.4 Example 2 : where to hit a ball with a cricket bat 23.5 Example 3 : an aircraft landing 24.1 Lagrangian mechanics : Introduction 24.2 Introductory example : the energy method for the E of M 24.3 Becoming familiar with the jargon 24.3.1 Generalised coordinates 24.3.2 Degrees of Freedom 24.3.3 Constraints 3 24.3.4 Configuration -
Action Principle for Hydrodynamics and Thermodynamics, Including General, Rotational Flows
th December 15, 2014 Action Principle for Hydrodynamics and Thermodynamics, including general, rotational flows C. Fronsdal Depart. of Physics and Astronomy, University of California Los Angeles 90095-1547 USA ABSTRACT This paper presents an action principle for hydrodynamics and thermodynamics that includes general, rotational flows, thus responding to a challenge that is more that 100 years old. It has been lifted to the relativistic context and it can be used to provide a suitable source of rotating matter for Einstein’s equation, finally overcoming another challenge of long standing, the problem presented by the Bianchi identity. The new theory is a combination of Eulerian and Lagrangian hydrodynamics, with an extension to thermodynamics. In the first place it is an action principle for adia- batic systems, including the usual conservation laws as well as the Gibbsean variational principle. But it also provides a framework within which dissipation can be introduced in the usual way, by adding a viscosity term to the momentum equation, one of the Euler-Lagrange equations. The rate of the resulting energy dissipation is determined by the equations of motion. It is an ideal framework for the description of quasi-static processes. It is a major development of the Navier-Stokes-Fourier approach, the princi- pal advantage being a hamiltonian structure with a natural concept of energy as a first integral of the motion. Two velocity fields are needed, one the gradient of a scalar potential, the other the time derivative of a vector field (vector potential). Variation of the scalar potential gives the equation of continuity and variation of the vector potential yields the momentum equation. -
6. Non-Inertial Frames
6. Non-Inertial Frames We stated, long ago, that inertial frames provide the setting for Newtonian mechanics. But what if you, one day, find yourself in a frame that is not inertial? For example, suppose that every 24 hours you happen to spin around an axis which is 2500 miles away. What would you feel? Or what if every year you spin around an axis 36 million miles away? Would that have any e↵ect on your everyday life? In this section we will discuss what Newton’s equations of motion look like in non- inertial frames. Just as there are many ways that an animal can be not a dog, so there are many ways in which a reference frame can be non-inertial. Here we will just consider one type: reference frames that rotate. We’ll start with some basic concepts. 6.1 Rotating Frames Let’s start with the inertial frame S drawn in the figure z=z with coordinate axes x, y and z.Ourgoalistounderstand the motion of particles as seen in a non-inertial frame S0, with axes x , y and z , which is rotating with respect to S. 0 0 0 y y We’ll denote the angle between the x-axis of S and the x0- axis of S as ✓.SinceS is rotating, we clearly have ✓ = ✓(t) x 0 0 θ and ✓˙ =0. 6 x Our first task is to find a way to describe the rotation of Figure 31: the axes. For this, we can use the angular velocity vector ! that we introduced in the last section to describe the motion of particles. -
Leonhard Euler - Wikipedia, the Free Encyclopedia Page 1 of 14
Leonhard Euler - Wikipedia, the free encyclopedia Page 1 of 14 Leonhard Euler From Wikipedia, the free encyclopedia Leonhard Euler ( German pronunciation: [l]; English Leonhard Euler approximation, "Oiler" [1] 15 April 1707 – 18 September 1783) was a pioneering Swiss mathematician and physicist. He made important discoveries in fields as diverse as infinitesimal calculus and graph theory. He also introduced much of the modern mathematical terminology and notation, particularly for mathematical analysis, such as the notion of a mathematical function.[2] He is also renowned for his work in mechanics, fluid dynamics, optics, and astronomy. Euler spent most of his adult life in St. Petersburg, Russia, and in Berlin, Prussia. He is considered to be the preeminent mathematician of the 18th century, and one of the greatest of all time. He is also one of the most prolific mathematicians ever; his collected works fill 60–80 quarto volumes. [3] A statement attributed to Pierre-Simon Laplace expresses Euler's influence on mathematics: "Read Euler, read Euler, he is our teacher in all things," which has also been translated as "Read Portrait by Emanuel Handmann 1756(?) Euler, read Euler, he is the master of us all." [4] Born 15 April 1707 Euler was featured on the sixth series of the Swiss 10- Basel, Switzerland franc banknote and on numerous Swiss, German, and Died Russian postage stamps. The asteroid 2002 Euler was 18 September 1783 (aged 76) named in his honor. He is also commemorated by the [OS: 7 September 1783] Lutheran Church on their Calendar of Saints on 24 St. Petersburg, Russia May – he was a devout Christian (and believer in Residence Prussia, Russia biblical inerrancy) who wrote apologetics and argued Switzerland [5] forcefully against the prominent atheists of his time. -
Notes on the Critically Damped Harmonic Oscillator Physics 2BL - David Kleinfeld
Notes on the Critically Damped Harmonic Oscillator Physics 2BL - David Kleinfeld We often have to build an electrical or mechanical device. An understand- ing of physics may help in the design and tuning of such a device. Here, we consider a critically damped spring oscillator as a model design for the shock absorber of a car. We consider a mass, denoted m, that is connected to a spring with spring constant k, so that the restoring force is F =-kx, and which moves in a lossy manner so that the frictional force is F =-bv =-bx˙. Prof. Newton tells us that F = mx¨ = −kx − bx˙ (1) Thus k b x¨ + x + x˙ = 0 (2) m m The two reduced constants are the natural frequency k ω = (3) 0 m and the decay constant b α = (4) m so that we need to consider 2 x¨ + ω0x + αx˙ = 0 (5) The above equation describes simple harmonic motion with loss. It is dis- cussed in lots of text books, but I want to consider a formulation of the solution that is most natural for critical damping. We know that when the damping constant is zero, i.e., α = 0, the solution 2 ofx ¨ + ω0x = 0 is given by: − x(t)=Ae+iω0t + Be iω0t (6) where A and B are constants that are found from the initial conditions, i.e., x(0) andx ˙(0). In a nut shell, the system oscillates forever. 1 We know that when the the natural frequency is zero, i.e., ω0 = 0, the solution ofx ¨ + αx˙ = 0 is given by: x˙(t)=Ae−αt (7) and 1 − e−αt x(t)=A + B (8) α where A and B are constants that are found from the initial conditions. -
Low Frequency Damping Control for Power Electronics-Based AC Grid Using Inverters with Built-In PSS
energies Article Low Frequency Damping Control for Power Electronics-Based AC Grid Using Inverters with Built-In PSS Ming Yang 1, Wu Cao 1,*, Tingjun Lin 1, Jianfeng Zhao 1 and Wei Li 2 1 School of Electrical Engineering, Southeast University, Nanjing 210096, China; [email protected] (M.Y.); [email protected] (T.L.); [email protected] (J.Z.) 2 NARI Group Corporation (State Grid Electric Power Research Institute), Nanjing 211106, China; [email protected] * Correspondence: [email protected] Abstract: Low frequency oscillations are the most easily occurring dynamic stability problem in the power system. With the increasing capacity of power electronic equipment, the coupling coordination of a synchronous generator and inverter in a low frequency range is worth to be studied further. This paper analyzes the mechanism of the interaction between a normal active/reactive power control grid-connected inverters and power regulation of a synchronous generator. Based on the mechanism, the power system stabilizer built in the inverter is used to increase damping in low frequency range. The small-signal model for electromagnetic torque interaction between the grid-connected inverters and the generator is analyzed first. The small-signal model is the basis for the inverters to provide damping with specific amplitude and phase. The additional damping torque control of the inverters is realized through a built-in power system stabilizer. The fundamentals and the structure of a built-in power system stabilizer are illustrated. The built-in power system stabilizer can be realized through the active or reactive power control loop. -
Tuned Mass Damper Systems
ConCh04v2.fm Page 217 Thursday, July 11, 2002 4:33 PM C H A PT E R 4 Tuned Mass Damper Systems 4.1 INTRODUCTION A tuned mass damper (TMD) is a device consisting of a mass, a spring, and a damper that is attached to a structure in order to reduce the dynamic response of the structure. The frequency of the damper is tuned to a particular structural frequency so that when that frequency is excited, the damper will resonate out of phase with the structural motion. Energy is dissipated by the damper inertia force acting on the structure. The TMD concept was first applied by Frahm in 1909 (Frahm, 1909) to reduce the rolling motion of ships as well as ship hull vibrations. A theory for the TMD was presented later in the paper by Ormondroyd and Den Hartog (1928), followed by a detailed discussion of optimal tuning and damping parameters in Den Hartog’s book on mechanical vibrations (1940). The initial theory was applicable for an undamped SDOF system subjected to a sinusoidal force excitation. Extension of the theory to damped SDOF systems has been investigated by numerous researchers. Significant contributions were made by Randall et al. (1981), Warburton (1981, 1982), Warburton and Ayorinde (1980), and Tsai and Lin (1993). This chapter starts with an introductory example of a TMD design and a brief description of some of the implementations of tuned mass dampers in building structures. A rigorous theory of tuned mass dampers for SDOF systems subjected to harmonic force excitation and harmonic ground motion is discussed next. -
Chapter 6 the Equations of Fluid Motion
Chapter 6 The equations of fluid motion In order to proceed further with our discussion of the circulation of the at- mosphere, and later the ocean, we must develop some of the underlying theory governing the motion of a fluid on the spinning Earth. A differen- tially heated, stratified fluid on a rotating planet cannot move in arbitrary paths. Indeed, there are strong constraints on its motion imparted by the angular momentum of the spinning Earth. These constraints are profoundly important in shaping the pattern of atmosphere and ocean circulation and their ability to transport properties around the globe. The laws governing the evolution of both fluids are the same and so our theoretical discussion willnotbespecifictoeitheratmosphereorocean,butcanandwillbeapplied to both. Because the properties of rotating fluids are often counter-intuitive and sometimes difficult to grasp, alongside our theoretical development we will describe and carry out laboratory experiments with a tank of water on a rotating table (Fig.6.1). Many of the laboratory experiments we make use of are simplified versions of ‘classics’ that have become cornerstones of geo- physical fluid dynamics. They are listed in Appendix 13.4. Furthermore we have chosen relatively simple experiments that, in the main, do nor require sophisticated apparatus. We encourage you to ‘have a go’ or view the atten- dant movie loops that record the experiments carried out in preparation of our text. We now begin a more formal development of the equations that govern the evolution of a fluid. A brief summary of the associated mathematical concepts, definitions and notation we employ can be found in an Appendix 13.2. -
Chapter 13: the Conditions of Rotary Motion
Chapter 13 Conditions of Rotary Motion KINESIOLOGY Scientific Basis of Human Motion, 11 th edition Hamilton, Weimar & Luttgens Presentation Created by TK Koesterer, Ph.D., ATC Humboldt State University Revised by Hamilton & Weimar REVISED FOR FYS by J. Wunderlich, Ph.D. Agenda 1. Eccentric Force àTorque (“Moment”) 2. Lever 3. Force Couple 4. Conservation of Angular Momentum 5. Centripetal and Centrifugal Forces ROTARY FORCE (“Eccentric Force”) § Force not in line with object’s center of gravity § Rotary and translatory motion can occur Fig 13.2 Torque (“Moment”) T = F x d F Moment T = F x d Arm F d = 0.3 cos (90-45) Fig 13.3 T = F x d Moment Arm Torque changed by changing length of moment d arm W T = F x d d W Fig 13.4 Sum of Torques (“Moments”) T = F x d Fig 13.8 Sum of Torques (“Moments”) T = F x d § Sum of torques = 0 • A balanced seesaw • Linear motion if equal parallel forces overcome resistance • Rowers Force Couple T = F x d § Effect of equal parallel forces acting in opposite direction Fig 13.6 & 13.7 LEVER § “A rigid bar that can rotate about a fixed point when a force is applied to overcome a resistance” § Used to: – Balance forces – Favor force production – Favor speed and range of motion – Change direction of applied force External Levers § Small force to overcome large resistance § Crowbar § Large Range Of Motion to overcome small resistance § Hitting golf ball § Balance force (load) § Seesaw Anatomical Levers § Nearly every bone is a lever § The joint is fulcrum § Contracting muscles are force § Don’t necessarily resemble