Total Angular Momentum
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Further Quantum Physics
Further Quantum Physics Concepts in quantum physics and the structure of hydrogen and helium atoms Prof Andrew Steane January 18, 2005 2 Contents 1 Introduction 7 1.1 Quantum physics and atoms . 7 1.1.1 The role of classical and quantum mechanics . 9 1.2 Atomic physics—some preliminaries . .... 9 1.2.1 Textbooks...................................... 10 2 The 1-dimensional projectile: an example for revision 11 2.1 Classicaltreatment................................. ..... 11 2.2 Quantum treatment . 13 2.2.1 Mainfeatures..................................... 13 2.2.2 Precise quantum analysis . 13 3 Hydrogen 17 3.1 Some semi-classical estimates . 17 3.2 2-body system: reduced mass . 18 3.2.1 Reduced mass in quantum 2-body problem . 19 3.3 Solution of Schr¨odinger equation for hydrogen . ..... 20 3.3.1 General features of the radial solution . 21 3.3.2 Precisesolution.................................. 21 3.3.3 Meanradius...................................... 25 3.3.4 How to remember hydrogen . 25 3.3.5 Mainpoints.................................... 25 3.3.6 Appendix on series solution of hydrogen equation, off syllabus . 26 3 4 CONTENTS 4 Hydrogen-like systems and spectra 27 4.1 Hydrogen-like systems . 27 4.2 Spectroscopy ........................................ 29 4.2.1 Main points for use of grating spectrograph . ...... 29 4.2.2 Resolution...................................... 30 4.2.3 Usefulness of both emission and absorption methods . 30 4.3 The spectrum for hydrogen . 31 5 Introduction to fine structure and spin 33 5.1 Experimental observation of fine structure . ..... 33 5.2 TheDiracresult ..................................... 34 5.3 Schr¨odinger method to account for fine structure . 35 5.4 Physical nature of orbital and spin angular momenta . -
Statics FE Review 032712.Pptx
FE Stacs Review h0p://www.coe.utah.edu/current-undergrad/fee.php Scroll down to: Stacs Review - Slides Torch Ellio [email protected] (801) 587-9016 MCE room 2016 (through 2000B door) Posi'on and Unit Vectors Y If you wanted to express a 100 lb force that was in the direction from A to B in (-2,6,3). A vector form, then you would find eAB and multiply it by 100 lb. rAB O x rAB = 7i - 7j – k (units of length) B .(5,-1,2) e = (7i-7j–k)/sqrt[99] (unitless) AB z Then: F = F eAB F = 100 lb {(7i-7j–k)/sqrt[99]} Another Way to Define a Unit Vectors Y Direction Cosines The θ values are the angles from the F coordinate axes to the vector F. The θY cosines of these θ values are the O θx x θz coefficients of the unit vector in the direction of F. z If cos(θx) = 0.500, cos(θy) = 0.643, and cos(θz) = - 0.580, then: F = F (0.500i + 0.643j – 0.580k) TrigonometrY hYpotenuse opposite right triangle θ adjacent • Sin θ = opposite/hYpotenuse • Cos θ = adjacent/hYpotenuse • Tan θ = opposite/adjacent TrigonometrY Con'nued A c B anY triangle b C a Σangles = a + b + c = 180o Law of sines: (sin a)/A = (sin b)/B = (sin c)/C Law of cosines: C2 = A2 + B2 – 2AB(cos c) Products of Vectors – Dot Product U . V = UVcos(θ) for 0 <= θ <= 180ο ( This is a scalar.) U In Cartesian coordinates: θ . -
Twisting Couple on a Cylinder Or Wire
Course: US01CPHY01 UNIT – 2 ELASTICITY – II Introduction: We discussed fundamental concept of properties of matter in first unit. This concept will be more use full for calculating various properties of mechanics of solid material. In this unit, we shall study the detail theory and its related experimental methods for determination of elastic constants and other related properties. Twisting couple on a cylinder or wire: Consider a cylindrical rod of length l radius r and coefficient of rigidity . Its upper end is fixed and a couple is applied in a plane perpendicular to its length at lower end as shown in fig.(a) Consider a cylinder is consisting a large number of co-axial hollow cylinder. Now, consider a one hollow cylinder of radius x and radial thickness dx as shown in fig.(b). Let is the twisting angle. The displacement is greatest at the rim and decreases as the center is approached where it becomes zero. As shown in fig.(a), Let AB be the line parallel to the axis OO’ before twist produced and on twisted B shifts to B’, then line AB become AB’. Before twisting if hollow cylinder cut along AB and flatted out, it will form the rectangular ABCD as shown in fig.(c). But if it will be cut after twisting it takes the shape of a parallelogram AB’C’D. The angle of shear From fig.(c) ∠ ̼̻̼′ = ∅ From fig.(b) ɑ ̼̼ = ͠∅ ɑ BB = xθ ∴ ͠∅ = ͬ Page 1 of 20 ͬ ∴ ∅ = … … … … … … (1) The modules of͠ rigidity is ͍ℎ͙͕ͦ͛͢͝ ͙ͧͤͦͧͧ ̀ = = ͕͙͛͢͠ ͚ͣ ͧℎ͙͕ͦ & ͬ ∴ ̀ = ∙ ∅ = The surface area of this hollow cylinder͠ = 2ͬͬ͘ Total shearing force on this area ∴ ͬ = 2ͬͬ͘ ∙ ͠ ͦ The moment of this force= 2 ͬ ͬ͘ ͠ ͦ = 2 ͬ ͬ͘ ∙ ͬ ͠ 2 ͧ Now, integrating between= theͬ limits∙ ͬ͘ x = 0 and x = r, We have, total twisting couple͠ on the cylinder - 2 ͧ = ǹ ͬ ͬ͘ * ͠ - 2 ͧ = ǹ ͬ ͬ͘ ͠ * ͨ - 2 ͬ = ʨ ʩ Total twisting couple ͠ 4 * ∴ ͨ ͦ = … … … … … … (3) Then, the twisting couple2͠ per unit twist ( ) is = 1 ͨ ͦ ̽ = … … … … … … (4) This twisting couple per unit twist 2͠is also called the torsional rigidity of the cylinder or wire. -
Fundamental Governing Equations of Motion in Consistent Continuum Mechanics
Fundamental governing equations of motion in consistent continuum mechanics Ali R. Hadjesfandiari, Gary F. Dargush Department of Mechanical and Aerospace Engineering University at Buffalo, The State University of New York, Buffalo, NY 14260 USA [email protected], [email protected] October 1, 2018 Abstract We investigate the consistency of the fundamental governing equations of motion in continuum mechanics. In the first step, we examine the governing equations for a system of particles, which can be considered as the discrete analog of the continuum. Based on Newton’s third law of action and reaction, there are two vectorial governing equations of motion for a system of particles, the force and moment equations. As is well known, these equations provide the governing equations of motion for infinitesimal elements of matter at each point, consisting of three force equations for translation, and three moment equations for rotation. We also examine the character of other first and second moment equations, which result in non-physical governing equations violating Newton’s third law of action and reaction. Finally, we derive the consistent governing equations of motion in continuum mechanics within the framework of couple stress theory. For completeness, the original couple stress theory and its evolution toward consistent couple stress theory are presented in true tensorial forms. Keywords: Governing equations of motion, Higher moment equations, Couple stress theory, Third order tensors, Newton’s third law of action and reaction 1 1. Introduction The governing equations of motion in continuum mechanics are based on the governing equations for systems of particles, in which the effect of internal forces are cancelled based on Newton’s third law of action and reaction. -
Learning the Virtual Work Method in Statics: What Is a Compatible Virtual Displacement?
2006-823: LEARNING THE VIRTUAL WORK METHOD IN STATICS: WHAT IS A COMPATIBLE VIRTUAL DISPLACEMENT? Ing-Chang Jong, University of Arkansas Ing-Chang Jong serves as Professor of Mechanical Engineering at the University of Arkansas. He received a BSCE in 1961 from the National Taiwan University, an MSCE in 1963 from South Dakota School of Mines and Technology, and a Ph.D. in Theoretical and Applied Mechanics in 1965 from Northwestern University. He was Chair of the Mechanics Division, ASEE, in 1996-97. His research interests are in mechanics and engineering education. Page 11.878.1 Page © American Society for Engineering Education, 2006 Learning the Virtual Work Method in Statics: What Is a Compatible Virtual Displacement? Abstract Statics is a course aimed at developing in students the concepts and skills related to the analysis and prediction of conditions of bodies under the action of balanced force systems. At a number of institutions, learning the traditional approach using force and moment equilibrium equations is followed by learning the energy approach using the virtual work method to enrich the learning of students. The transition from the traditional approach to the energy approach requires learning several related key concepts and strategy. Among others, compatible virtual displacement is a key concept, which is compatible with what is required in the virtual work method but is not commonly recognized and emphasized. The virtual work method is initially not easy to learn for many people. It is surmountable when one understands the following: (a) the proper steps and strategy in the method, (b) the displacement center, (c) some basic geometry, and (d ) the radian measure formula to compute virtual displacements. -
1. the Hamiltonian, H = Α Ipi + Βm, Must Be Her- Mitian to Give Real
1. The hamiltonian, H = αipi + βm, must be her- yields mitian to give real eigenvalues. Thus, H = H† = † † † pi αi +β m. From non-relativistic quantum mechanics † † † αi pi + β m = aipi + βm (2) we know that pi = pi . In addition, [αi,pj ] = 0 because we impose that the α, β operators act on the spinor in- † † αi = αi, β = β. Thus α, β are hermitian operators. dices while pi act on the coordinates of the wave function itself. With these conditions we may proceed: To verify the other properties of the α, and β operators † † piαi + β m = αipi + βm (1) we compute 2 H = (αipi + βm) (αj pj + βm) 2 2 1 2 2 = αi pi + (αiαj + αj αi) pipj + (αiβ + βαi) m + β m , (3) 2 2 where for the second term i = j. Then imposing the Finally, making use of bi = 1 we can find the 26 2 2 2 relativistic energy relation, E = p + m , we obtain eigenvalues: biu = λu and bibiu = λbiu, hence u = λ u the anti-commutation relation | | and λ = 1. ± b ,b =2δ 1, (4) i j ij 2. We need to find the λ = +1/2 helicity eigenspinor { } ′ for an electron with momentum ~p = (p sin θ, 0, p cos θ). where b0 = β, bi = αi, and 1 n n idenitity matrix. ≡ × 1 Using the anti-commutation relation and the fact that The helicity operator is given by 2 σ pˆ, and the posi- 2 1 · bi = 1 we are able to find the trace of any bi tive eigenvalue 2 corresponds to u1 Dirac solution [see (1.5.98) in http://arXiv.org/abs/0906.1271]. -
Bound-State Solutions of Dirac Equation Plan of the Lecture
Lecture 3 Bound-state solutions of Dirac equation Plan of the lecture • Few comments about Dirac equation • Free- and bound-state solutions • Dirac’s spectroscopic notations – Integrals of motion – Parity of states • Energy levels of the bound-state Dirac’s particle • Structure of Dirac’s wavefunction • Radial components of the Dirac’s wavefunction Four-vectors In the relativistic world it is more convenient to work with four-vectors: Contravariant vectors Covariant vectors 휇 푥 = 푡, 푥, 푦, 푧 푥휇 = 푡, −푥, −푦, −푧 휕 휕 휕 휕 휕 휕 휕 휕 휕휇 = , − , − , − 휕 = , , , 휕푡 휕푥 휕푦 휕푧 휇 휕푡 휕푥 휕푦 휕푧 휇 푝 = 퐸, 푝푥, 푝푦, 푝푧 푝휇 = 퐸, −푝푥, −푝푦, −푝푧 Lorentz transformation 푥′휇 = 푎휈 푥휇 ′ 휈 휇 푥휇 = 푎휇 푥휇 휈 휈 훾 −훾훽 0 0 훾 훾훽 0 0 −훾훽 훾 훾훽 훾 0 0 푎휈 = 0 0 푎휈 = 휇 0 0 1 0 휇 0 0 1 0 0 0 0 1 0 0 0 1 Klein-Gordon equation Based on the relativistic energy-mass equation: 퐸2 = 푝ҧ2 + 푚2 One can derive Klein-Gordon equation for scalar (zero-spin) relativistic particles: Oscar Klein 휇 2 휕 휕휇 + 푚 휑 푥 = 0 By introducing d'Alembert operator: 휕2 휕휇휕 =⊡= − 휵2 휇 휕푡2 We can re-write Klein-Gordon equation as: ⊡ + 푚2 휑 푥 = 0 Klein-Gordon equation We can derive Klein-Gordon equation for scalar (zero-spin) relativistic particles: 휇 2 휕 휕휇 + 푚 휑 푥 = 0 Free-particle solutions of this equation: Oscar Klein 휑 푥 = 푁 푒−푖 푝푥 = 푁 푒−푖퐸푡+푖풑풓 Allow particles with both positive and negative energy: 퐸 = ± 풑2 + 푚2 And with positive and negative probability density: 푗0 = 2 푁 2 퐸 How do we understand negative-energy solutions? And what is much worse, the negative probability density? Dirac equation We can re-write -
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 -
5.80 Small-Molecule Spectroscopy and Dynamics Fall 2008
MIT OpenCourseWare http://ocw.mit.edu 5.80 Small-Molecule Spectroscopy and Dynamics Fall 2008 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.edu/terms. Lecture #1 Supplement Contents A. Spectroscopic Notation . 1 1. H. N. Russell, A. G. Shenstone, and L. A. Turner, \Report on Notation for Atomic Spectra," 1 2. W. F. Meggers and C. E. Moore, \Report of Subcommittee f (Notation for the Spectra of Diatomic Molecules)" . 2 3. F. A. Jenkins, \Report of Subcommittee f (Notation for the Spectra of Diatomic Molecules)" 2 4. No author, \Report on Notation for the Spectra of Polyatomic Molecules" . 2 B. Good Quantum Numbers . 2 C. Perturbation Theory and Secular Equations . 3 D. Non-Orthonormal Basis Sets . 6 E. Transformation of Matrix Elements of any Operator into Perturbed Basis Set . 7 A. Spectroscopic Notation The language of spectroscopy is very explicit and elegant, capable of describing a wide range of unanticipated situations concisely and unambiguously. The coherence of this language is diligently preserved by a succession of august committees, whose agreements about notation are codified. These agreements are often published as authorless articles in major journals. The following list of citations include the best of these notation-codifying articles. 1. H. N. Russell, A. G. Shenstone, and L. A. Turner, \Report on Notation for Atomic Spectra," Phys. Rev. 33, 900-906 (1929). At an informal meeting of spectroscopists at Washington in April, 1928, the writers of this report were requested to draw up a scheme for the clarification of spectroscopic notation. After much discussion and correspondence with spectroscopists both in this country and abroad we are able to present the following recommendations. -
Waves & Normal Modes
Waves & Normal Modes Matt Jarvis February 2, 2016 Contents 1 Oscillations 2 1.0.1 Simple Harmonic Motion - revision . 2 2 Normal Modes 5 2.1 Thecoupledpendulum.............................. 6 2.1.1 TheDecouplingMethod......................... 7 2.1.2 The Matrix Method . 10 2.1.3 Initial conditions and examples . 13 2.1.4 Energy of a coupled pendulum . 15 2.2 Unequal Coupled Pendula . 18 2.3 The Horizontal Spring-Mass system . 22 2.3.1 Decouplingmethod............................ 22 2.3.2 The Matrix Method . 23 2.3.3 Energy of the horizontal spring-mass system . 25 2.3.4 Initial Condition . 26 2.4 Vertical spring-mass system . 26 2.4.1 The matrix method . 27 2.5 Interlude: Solving inhomogeneous 2nd order di↵erential equations . 28 2.6 Horizontal spring-mass system with a driving term . 31 2.7 The Forced Coupled Pendulum with a Damping Factor . 33 3 Normal modes II - towards the continuous limit 39 3.1 N-coupled oscillators . 39 3.1.1 Special cases . 40 3.1.2 General case . 42 3.1.3 N verylarge ............................... 44 3.1.4 Longitudinal Oscillations . 47 4WavesI 48 4.1 Thewaveequation ................................ 48 4.1.1 TheStretchedString........................... 48 4.2 d’Alambert’s solution to the wave equation . 50 4.2.1 Interpretation of d’Alambert’s solution . 51 4.2.2 d’Alambert’s solution with boundary conditions . 52 4.3 Solving the wave equation by separation of variables . 54 4.3.1 Negative C . 55 i 1 4.3.2 Positive C . 56 4.3.3 C=0.................................... 56 4.4 Sinusoidalwaves ................................ -
2D Rigid Body Dynamics: Work and Energy
J. Peraire, S. Widnall 16.07 Dynamics Fall 2008 Version 1.0 Lecture L22 - 2D Rigid Body Dynamics: Work and Energy In this lecture, we will revisit the principle of work and energy introduced in lecture L11-13 for particle dynamics, and extend it to 2D rigid body dynamics. Kinetic Energy for a 2D Rigid Body We start by recalling the kinetic energy expression for a system of particles derived in lecture L11, n 1 2 X 1 02 T = mvG + mir_i ; 2 2 i=1 0 where n is the total number of particles, mi denotes the mass of particle i, and ri is the position vector of Pn particle i with respect to the center of mass, G. Also, m = i=1 mi is the total mass of the system, and vG is the velocity of the center of mass. The above expression states that the kinetic energy of a system of particles equals the kinetic energy of a particle of mass m moving with the velocity of the center of mass, plus the kinetic energy due to the motion of the particles relative to the center of mass, G. For a 2D rigid body, the velocity of all particles relative to the center of mass is a pure rotation. Thus, we can write 0 0 r_ i = ! × ri: Therefore, we have n n n X 1 02 X 1 0 0 X 1 02 2 mir_i = mi(! × ri) · (! × ri) = miri ! ; 2 2 2 i=1 i=1 i=1 0 Pn 02 where we have used the fact that ! and ri are perpendicular. -
An Essay on Lagrangian and Eulerian Kinematics of Fluid Flow
Lagrangian and Eulerian Representations of Fluid Flow: Kinematics and the Equations of Motion James F. Price Woods Hole Oceanographic Institution, Woods Hole, MA, 02543 [email protected], http://www.whoi.edu/science/PO/people/jprice June 7, 2006 Summary: This essay introduces the two methods that are widely used to observe and analyze fluid flows, either by observing the trajectories of specific fluid parcels, which yields what is commonly termed a Lagrangian representation, or by observing the fluid velocity at fixed positions, which yields an Eulerian representation. Lagrangian methods are often the most efficient way to sample a fluid flow and the physical conservation laws are inherently Lagrangian since they apply to moving fluid volumes rather than to the fluid that happens to be present at some fixed point in space. Nevertheless, the Lagrangian equations of motion applied to a three-dimensional continuum are quite difficult in most applications, and thus almost all of the theory (forward calculation) in fluid mechanics is developed within the Eulerian system. Lagrangian and Eulerian concepts and methods are thus used side-by-side in many investigations, and the premise of this essay is that an understanding of both systems and the relationships between them can help form the framework for a study of fluid mechanics. 1 The transformation of the conservation laws from a Lagrangian to an Eulerian system can be envisaged in three steps. (1) The first is dubbed the Fundamental Principle of Kinematics; the fluid velocity at a given time and fixed position (the Eulerian velocity) is equal to the velocity of the fluid parcel (the Lagrangian velocity) that is present at that position at that instant.