1.1 The Equations of Motion

Size: px
Start display at page:

Download "1.1 The Equations of Motion"

Transcription

1 1.1 The Equations of Motion In Book I, balance of forces and moments acting on an component was enforced in order to ensure that the component was in equilibrium. Here, allowance is made for stresses which var continuousl throughout a material, and force equilibrium of an portion of material is enforced. One-Dimensional Equation Consider a one-dimensional differential element of length and cross sectional area A, Fig Let the average bod force per unit volume acting on the element be b and the average acceleration and densit of the element be a and. Stresses act on the element. () A b,a ( ) Figure 1.1.1: a differential element under the action of surface and bod forces The net surface force acting is ( ) A ( ) A. If the element is small, then the bod force and velocit can be assumed to var linearl over the element and the average will act at the centre of the element. Then the bod force acting on the element is Ab and the inertial force is Aa. Appling Newton s second law leads to ( ) A ( ) A ba aa ( ) ( ) b a (1.1.1) so that, b the definition of the derivative, in the limit as 0, d b a 1-d Equation of Motion (1.1.2) d which is the one-dimensional equation of motion. Note that this equation was derived on the basis of a phsical law and must therefore be satisfied for all materials, whatever the be composed of. The derivative d / d is the stress gradient phsicall, it is a measure of how rapidl the stresses are changing. Eample Consider a bar of length l which hangs from a ceiling, as shown in Fig

2 z l Figure 1.1.2: a hanging bar The gravitational force is F mg downward and the bod force per unit volume is thus b g. There are no accelerating material particles. Taking the z ais positive down, an integration of the equation of motion gives d g 0 gz c (1.1.3) dz where c is an arbitrar constant. The lower end of the bar is free and so the stress there is zero, and so Two-Dimensional Equations g l z (1.1.4) Consider now a two dimensional infinitesimal element of width and height and unit depth (into the page). and Looking at the normal stress components acting in the direction, and allowing for variations in stress over the element surfaces, the stresses are as shown in Fig (, (, (, (, Figure 1.1.3: varing stresses acting on a differential element Using a (two dimensional) Talor series and dropping higher order terms then leads to the linearl varing stresses illustrated in Fig (where, and the partial derivatives are evaluated at,, which is a reasonable approimation when the element is small. 4

3 Figure 1.1.4: linearl varing stresses acting on a differential element The effect (resultant force) of this linear variation of stress on the plane can be replicated b a constant stress acting over the whole plane, the size of which is the average stress. For the left and right sides, one has, respectivel, 1 2, 1 2 (1.1.5) One can take awa the stress ( 1/ 2) / from both sides without affecting the net force acting on the element so one finall has the representation shown in Fig (, Figure 1.1.5: net stresses acting on a differential element Carring out the same procedure for the shear stresses contributing to a force in the direction leads to the stresses shown in Fig (, b, a (, Figure 1.1.6: normal and shear stresses acting on a differential element Take a, b to be the average acceleration and bod force, and to be the average densit. Newton s law then ields 5

4 b a (1.1.6) which, dividing through b and taking the limit, gives b a (1.1.7) A similar analsis for force components in the direction ields another equation and one then has the two-dimensional equations of motion: b b a a 2-D Equations of Motion (1.1.8) Three-Dimensional Equations Similarl, one can consider a three-dimensional element, and one finds that z z z z z z z zz b b b z a a a z 3-D Equations of Motion (1.1.9) These three equations epress force-balance in, respectivel, the,, z directions. 6

5 Figure 1.1.7: from Cauch s Eercices de Mathematiques (1829) The Equations of Equlibrium If the material is not moving (or is moving at constant velocit and is in static equilibrium, then the equations of motion reduce to the equations of equilibrium, z z z b z z b z zz bz z D Equations of Equilibrium (1.1.10) These equations epress the force balance between surface forces and bod forces in a material. The equations of equilibrium ma also be used as a good approimation in the analsis of materials which have relativel small accelerations Problems 1. What does the one-dimensional equation of motion sa about the stresses in a bar in the absence of an bod force or acceleration? 2. Does equilibrium eist for the following two dimensional stress distribution in the absence of bod forces? 3 48 / zz z z z z 7

6 3. The elementar beam theor predicts that the stresses in a circular beam due to bending are 4 M / I, V ( R ) / 3I ( I R / 4) and all the other stress components are zero. Do these equations satisf the equations of equilibrium? 4. With respect to aes 0 z the stress state is given in terms of the coordinates b the matri 2 z ij z z z 2 z z zz 0 z z Determine the bod force acting on the material if it is at rest What is the acceleration of a material particle of densit 0.3kgm, subjected to the stress z 2 4 ij 2 2 2z 2 4 2z 2z 2z z and gravit (the z ais is directed verticall upwards from the ground). 6. A fluid at rest is subjected to a hdrostatic pressure p and the force of gravit onl. (a) Write out the equations of motion for this case. (b) A ver basic formula of hdrostatics, to be found in an elementar book on fluid mechanics, is that giving the pressure variation in a static fluid, p gh where is the densit of the fluid, g is the acceleration due to gravit, and h is the vertical distance between the two points in the fluid (the relative depth). Show that this formula is but a special case of the equations of motion. 8

1 Differential Equations for Solid Mechanics

1 Differential Equations for Solid Mechanics 1 Differential Eqations for Solid Mechanics Simple problems involving homogeneos stress states have been considered so far, wherein the stress is the same throghot the component nder std. An eception to

More information

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Chapter 8 KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Figure 8.1: 195 196 CHAPTER 8. KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS 8.1 Motivation In Chapter 3, the conservation of linear momentum for a

More information

MAE 323: Chapter 4. Plane Stress and Plane Strain. The Stress Equilibrium Equation

MAE 323: Chapter 4. Plane Stress and Plane Strain. The Stress Equilibrium Equation The Stress Equilibrium Equation As we mentioned in Chapter 2, using the Galerkin formulation and a choice of shape functions, we can derive a discretized form of most differential equations. In Structural

More information

Chapter 5 Equilibrium of a Rigid Body Objectives

Chapter 5 Equilibrium of a Rigid Body Objectives Chapter 5 Equilibrium of a Rigid Bod Objectives Develop the equations of equilibrium for a rigid bod Concept of the free-bod diagram for a rigid bod Solve rigid-bod equilibrium problems using the equations

More information

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane 3.5 Plane Stress This section is concerned with a special two-dimensional state of stress called plane stress. It is important for two reasons: () it arises in real components (particularl in thin components

More information

3 Stress internal forces stress stress components Stress analysis stress transformation equations principal stresses stress invariants

3 Stress internal forces stress stress components Stress analysis stress transformation equations principal stresses stress invariants 3 Stress orces acting at the surfaces of components were considered in the previous chapter. The task now is to eamine forces arising inside materials, internal forces. Internal forces are described using

More information

Chapter 6 2D Elements Plate Elements

Chapter 6 2D Elements Plate Elements Institute of Structural Engineering Page 1 Chapter 6 2D Elements Plate Elements Method of Finite Elements I Institute of Structural Engineering Page 2 Continuum Elements Plane Stress Plane Strain Toda

More information

18 Equilibrium equation of a laminated plate (a laminate)

18 Equilibrium equation of a laminated plate (a laminate) z ν = 1 ν = ν = 3 ν = N 1 ν = N z 0 z 1 z N 1 z N z α 1 < 0 α > 0 ν = 1 ν = ν = 3 Such laminates are often described b an orientation code [α 1 /α /α 3 /α 4 ] For eample [0/-45/90/45/0/0/45/90/-45/0] Short

More information

Lecture 6: Distributed Forces Part 2 Second Moment of Area

Lecture 6: Distributed Forces Part 2 Second Moment of Area Lecture 6: Distributed Forces Part Second Moment of rea The second moment of area is also sometimes called the. This quantit takes the form of The phsical representation of the above integral can be described

More information

Fluid Mechanics II. Newton s second law applied to a control volume

Fluid Mechanics II. Newton s second law applied to a control volume Fluid Mechanics II Stead flow momentum equation Newton s second law applied to a control volume Fluids, either in a static or dnamic motion state, impose forces on immersed bodies and confining boundaries.

More information

APPLIED MECHANICS I Resultant of Concurrent Forces Consider a body acted upon by co-planar forces as shown in Fig 1.1(a).

APPLIED MECHANICS I Resultant of Concurrent Forces Consider a body acted upon by co-planar forces as shown in Fig 1.1(a). PPLIED MECHNICS I 1. Introduction to Mechanics Mechanics is a science that describes and predicts the conditions of rest or motion of bodies under the action of forces. It is divided into three parts 1.

More information

3 2D Elastostatic Problems in Cartesian Coordinates

3 2D Elastostatic Problems in Cartesian Coordinates D lastostatic Problems in Cartesian Coordinates Two dimensional elastostatic problems are discssed in this Chapter, that is, static problems of either plane stress or plane strain. Cartesian coordinates

More information

10. The dimensional formula for c) 6% d) 7%

10. The dimensional formula for c) 6% d) 7% UNIT. One of the combinations from the fundamental phsical constants is hc G. The unit of this epression is a) kg b) m 3 c) s - d) m. If the error in the measurement of radius is %, then the error in the

More information

Strain Transformation and Rosette Gage Theory

Strain Transformation and Rosette Gage Theory Strain Transformation and Rosette Gage Theor It is often desired to measure the full state of strain on the surface of a part, that is to measure not onl the two etensional strains, and, but also the shear

More information

CH. 1 FUNDAMENTAL PRINCIPLES OF MECHANICS

CH. 1 FUNDAMENTAL PRINCIPLES OF MECHANICS 446.201 (Solid echanics) Professor Youn, eng Dong CH. 1 FUNDENTL PRINCIPLES OF ECHNICS Ch. 1 Fundamental Principles of echanics 1 / 14 446.201 (Solid echanics) Professor Youn, eng Dong 1.2 Generalied Procedure

More information

Distributed Forces: Moments of Inertia

Distributed Forces: Moments of Inertia Distributed Forces: Moments of nertia Contents ntroduction Moments of nertia of an Area Moments of nertia of an Area b ntegration Polar Moments of nertia Radius of Gration of an Area Sample Problems Parallel

More information

4 Strain true strain engineering strain plane strain strain transformation formulae

4 Strain true strain engineering strain plane strain strain transformation formulae 4 Strain The concept of strain is introduced in this Chapter. The approimation to the true strain of the engineering strain is discussed. The practical case of two dimensional plane strain is discussed,

More information

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are: Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements

More information

Conservation of Linear Momentum for a Differential Control Volume

Conservation of Linear Momentum for a Differential Control Volume Conservation of Linear Momentum for a Differential Control Volume When we applied the rate-form of the conservation of mass equation to a differential control volume (open sstem in Cartesian coordinates,

More information

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Ninth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Ninth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. N E 9 Distributed CHAPTER VECTOR MECHANCS FOR ENGNEERS: STATCS Ferdinand P. Beer E. Russell Johnston, Jr. Lecture Notes: J. Walt Oler Teas Tech Universit Forces: Moments of nertia Contents ntroduction

More information

Conservation of Linear Momentum

Conservation of Linear Momentum Conservation of Linear Momentum Once we have determined the continuit equation in di erential form we proceed to derive the momentum equation in di erential form. We start b writing the integral form of

More information

5.6. Differential equations

5.6. Differential equations 5.6. Differential equations The relationship between cause and effect in phsical phenomena can often be formulated using differential equations which describe how a phsical measure () and its derivative

More information

5. Nonholonomic constraint Mechanics of Manipulation

5. Nonholonomic constraint Mechanics of Manipulation 5. Nonholonomic constraint Mechanics of Manipulation Matt Mason matt.mason@cs.cmu.edu http://www.cs.cmu.edu/~mason Carnegie Mellon Lecture 5. Mechanics of Manipulation p.1 Lecture 5. Nonholonomic constraint.

More information

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Seventh Edition CHAPTER. Ferdinand P. Beer

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Seventh Edition CHAPTER. Ferdinand P. Beer 00 The McGraw-Hill Companies, nc. All rights reserved. Seventh E CHAPTER VECTOR MECHANCS FOR ENGNEERS: 9 STATCS Ferdinand P. Beer E. Russell Johnston, Jr. Distributed Forces: Lecture Notes: J. Walt Oler

More information

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted.

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted. 4.1 Strain If an object is placed on a table and then the table is moved, each material particle moves in space. The particles undergo a displacement. The particles have moved in space as a rigid bod.

More information

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 4 Pure Bending

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 4 Pure Bending EA 3702 echanics & aterials Science (echanics of aterials) Chapter 4 Pure Bending Pure Bending Ch 2 Aial Loading & Parallel Loading: uniform normal stress and shearing stress distribution Ch 3 Torsion:

More information

15 INTERLAMINAR STRESSES

15 INTERLAMINAR STRESSES 15 INTERLAMINAR STRESSES 15-1 OUT-OF-PLANE STRESSES Classical laminate plate theor predicts the stresses in the plane of the lamina,, and τ but does not account for out-of-plane stresses, τ and τ. It assumes

More information

Ocean Dynamics. Equation of motion a=σf/ρ 29/08/11. What forces might cause a parcel of water to accelerate?

Ocean Dynamics. Equation of motion a=σf/ρ 29/08/11. What forces might cause a parcel of water to accelerate? Phsical oceanograph, MSCI 300 Oceanographic Processes, MSCI 5004 Dr. Ale Sen Gupta a.sengupta@unsw.e.au Ocean Dnamics Newton s Laws of Motion An object will continue to move in a straight line and at a

More information

= C. on q 1 to the left. Using Coulomb s law, on q 2 to the right, and the charge q 2 exerts a force F 2 on 1 ( )

= C. on q 1 to the left. Using Coulomb s law, on q 2 to the right, and the charge q 2 exerts a force F 2 on 1 ( ) Phsics Solutions to Chapter 5 5.. Model: Use the charge model. Solve: (a) In the process of charging b rubbing, electrons are removed from one material and transferred to the other because the are relativel

More information

UNIT 4 HEAT TRANSFER BY CONVECTION

UNIT 4 HEAT TRANSFER BY CONVECTION UNIT 4 HEAT TRANSFER BY CONVECTION 4.1 Introduction to convection 4. Convection boundar laers 4..1 Hdrodnamic boundar laer over flat plate 4.. Thermal boundar laer 4..3 Concentration boundar laer 4.3 Dimensional

More information

Second-Order Linear Differential Equations C 2

Second-Order Linear Differential Equations C 2 C8 APPENDIX C Additional Topics in Differential Equations APPENDIX C. Second-Order Homogeneous Linear Equations Second-Order Linear Differential Equations Higher-Order Linear Differential Equations Application

More information

MMJ1153 COMPUTATIONAL METHOD IN SOLID MECHANICS PRELIMINARIES TO FEM

MMJ1153 COMPUTATIONAL METHOD IN SOLID MECHANICS PRELIMINARIES TO FEM B Course Content: A INTRODUCTION AND OVERVIEW Numerical method and Computer-Aided Engineering; Phsical problems; Mathematical models; Finite element method;. B Elements and nodes, natural coordinates,

More information

LECTURE NOTES - VIII. Prof. Dr. Atıl BULU

LECTURE NOTES - VIII. Prof. Dr. Atıl BULU LECTURE NOTES - VIII «LUID MECHNICS» Istanbul Technical Universit College of Civil Engineering Civil Engineering Department Hdraulics Division CHPTER 8 DIMENSIONL NLYSIS 8. INTRODUCTION Dimensional analsis

More information

Survey of Wave Types and Characteristics

Survey of Wave Types and Characteristics Seminar: Vibrations and Structure-Borne Sound in Civil Engineering Theor and Applications Surve of Wave Tpes and Characteristics Xiuu Gao April 1 st, 2006 Abstract Mechanical waves are waves which propagate

More information

Module #4. Fundamentals of strain The strain deviator Mohr s circle for strain READING LIST. DIETER: Ch. 2, Pages 38-46

Module #4. Fundamentals of strain The strain deviator Mohr s circle for strain READING LIST. DIETER: Ch. 2, Pages 38-46 HOMEWORK From Dieter 2-7 Module #4 Fundamentals of strain The strain deviator Mohr s circle for strain READING LIST DIETER: Ch. 2, Pages 38-46 Pages 11-12 in Hosford Ch. 6 in Ne Strain When a solid is

More information

The Plane Stress Problem

The Plane Stress Problem . 4 The Plane Stress Problem 4 Chapter 4: THE PLANE STRESS PROBLEM 4 TABLE OF CONTENTS Page 4.. INTRODUCTION 4 3 4... Plate in Plane Stress............... 4 3 4... Mathematical Model.............. 4 4

More information

Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators. Abstract

Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators. Abstract Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators Rajendra Singh and Seungbo Kim The Ohio State Universit Columbus, OH 4321-117, USA Abstract Much of the vibration isolation

More information

Section 1: Review of Elasticity

Section 1: Review of Elasticity Finite Elements in Elasticit Section : Review of Elasticit Stress & Strain 2 Constitutive Theor 3 Energ Methods Section : Stress and Strain Stress at a point Q : F = lim A 0 A F = lim A 0 A F = lim A 0

More information

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA)

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA) LETURE Third Edition BEMS: SHER ND MOMENT DGRMS (FORMUL). J. lark School of Engineering Department of ivil and Environmental Engineering 1 hapter 5.1 5. b Dr. brahim. ssakkaf SPRNG 00 ENES 0 Mechanics

More information

Exercise solutions: concepts from chapter 7

Exercise solutions: concepts from chapter 7 f () = -N F = +N f (1) = +4N Fundamentals of Structural Geolog 1) In the following eercise we consider some of the phsical quantities used in the stud of particle dnamics and review their relationships

More information

MAE4700/5700 Finite Element Analysis for Mechanical and Aerospace Design

MAE4700/5700 Finite Element Analysis for Mechanical and Aerospace Design MAE4700/5700 Finite Element Analsis for Mechanical and Aerospace Design Cornell Universit, Fall 2009 Nicholas Zabaras Materials Process Design and Control Laborator Sible School of Mechanical and Aerospace

More information

Equations of Motion. Figure 1.1.1: a differential element under the action of surface and body forces

Equations of Motion. Figure 1.1.1: a differential element under the action of surface and body forces Equtions of Motion In Prt I, lnce of forces nd moments cting on n component ws enforced in order to ensure tht the component ws in equilirium. Here, llownce is mde for stresses which vr continuousl throughout

More information

r some or all of m, x, yz. Similarly for I yy and I zz.

r some or all of m, x, yz. Similarly for I yy and I zz. Homework 10. Chapters 1, 1. Moments and products of inertia. 10.1 Concepts: What objects have a moment of inertia? (Section 1.1). Consider the moment of inertia S/ bu bu of an object S about a point for

More information

Additional Topics in Differential Equations

Additional Topics in Differential Equations 6 Additional Topics in Differential Equations 6. Eact First-Order Equations 6. Second-Order Homogeneous Linear Equations 6.3 Second-Order Nonhomogeneous Linear Equations 6.4 Series Solutions of Differential

More information

MATRIX TRANSFORMATIONS

MATRIX TRANSFORMATIONS CHAPTER 5. MATRIX TRANSFORMATIONS INSTITIÚID TEICNEOLAÍOCHTA CHEATHARLACH INSTITUTE OF TECHNOLOGY CARLOW MATRIX TRANSFORMATIONS Matri Transformations Definition Let A and B be sets. A function f : A B

More information

Chapter 9 BIAXIAL SHEARING

Chapter 9 BIAXIAL SHEARING 9. DEFNTON Chapter 9 BAXAL SHEARNG As we have seen in the previous chapter, biaial (oblique) shearing produced b the shear forces and, appears in a bar onl accompanied b biaial bending (we ma discuss about

More information

Pan Pearl River Delta Physics Olympiad 2005

Pan Pearl River Delta Physics Olympiad 2005 1 Jan. 29, 25 Morning Session (9 am 12 pm) Q1 (5 Two identical worms of length L are ling on a smooth and horizontal surface. The mass of the worms is evenl distributed along their bod length. The starting

More information

LECTURE 14 Strength of a Bar in Transverse Bending. 1 Introduction. As we have seen, only normal stresses occur at cross sections of a rod in pure

LECTURE 14 Strength of a Bar in Transverse Bending. 1 Introduction. As we have seen, only normal stresses occur at cross sections of a rod in pure V. DEMENKO MECHNCS OF MTERLS 015 1 LECTURE 14 Strength of a Bar in Transverse Bending 1 ntroduction s we have seen, onl normal stresses occur at cross sections of a rod in pure bending. The corresponding

More information

TENSOR TRANSFORMATION OF STRESSES

TENSOR TRANSFORMATION OF STRESSES GG303 Lecture 18 9/4/01 1 TENSOR TRANSFORMATION OF STRESSES Transformation of stresses between planes of arbitrar orientation In the 2-D eample of lecture 16, the normal and shear stresses (tractions)

More information

Ocean Dynamics. The Equations of Motion 8/27/10. Physical Oceanography, MSCI 3001 Oceanographic Processes, MSCI dt = fv. dt = fu.

Ocean Dynamics. The Equations of Motion 8/27/10. Physical Oceanography, MSCI 3001 Oceanographic Processes, MSCI dt = fv. dt = fu. Phsical Oceanograph, MSCI 3001 Oceanographic Processes, MSCI 5004 Dr. Katrin Meissner k.meissner@unsw.e.au Ocean Dnamics The Equations of Motion d u dt = 1 ρ Σ F Horizontal Equations: Acceleration = Pressure

More information

ARCH 631 Note Set 2.1 F2010abn. Statics Primer

ARCH 631 Note Set 2.1 F2010abn. Statics Primer RCH 631 Note Set.1 F010abn Statics Primer Notation: a = name for acceleration = area (net = with holes, bearing = in contact, etc...) (C) = shorthand for compression d = perpendicular distance to a force

More information

ragsdale (zdr82) HW7 ditmire (58335) 1 The magnetic force is

ragsdale (zdr82) HW7 ditmire (58335) 1 The magnetic force is ragsdale (zdr8) HW7 ditmire (585) This print-out should have 8 questions. Multiple-choice questions ma continue on the net column or page find all choices efore answering. 00 0.0 points A wire carring

More information

APPLYING NEWTON S LAWS

APPLYING NEWTON S LAWS APPLYING NEWTON S LAWS 5 igible mass. Let T r be the tension in the rope and let T c be the tension in the chain. EXECUTE: (a) The free-bod diagram for each weight is the same and is given in Figure 5.1a.

More information

Dynamics and control of mechanical systems

Dynamics and control of mechanical systems JU 18/HL Dnamics and control of mechanical sstems Date Da 1 (3/5) 5/5 Da (7/5) Da 3 (9/5) Da 4 (11/5) Da 5 (14/5) Da 6 (16/5) Content Revie of the basics of mechanics. Kinematics of rigid bodies coordinate

More information

THE GENERAL ELASTICITY PROBLEM IN SOLIDS

THE GENERAL ELASTICITY PROBLEM IN SOLIDS Chapter 10 TH GNRAL LASTICITY PROBLM IN SOLIDS In Chapters 3-5 and 8-9, we have developed equilibrium, kinematic and constitutive equations for a general three-dimensional elastic deformable solid bod.

More information

CONSERVATION OF ANGULAR MOMENTUM FOR A CONTINUUM

CONSERVATION OF ANGULAR MOMENTUM FOR A CONTINUUM Chapter 4 CONSERVATION OF ANGULAR MOMENTUM FOR A CONTINUUM Figure 4.1: 4.1 Conservation of Angular Momentum Angular momentum is defined as the moment of the linear momentum about some spatial reference

More information

First Order Equations

First Order Equations 10 1 Linear and Semilinear Equations Chapter First Order Equations Contents 1 Linear and Semilinear Equations 9 Quasilinear Equations 19 3 Wave Equation 6 4 Sstems of Equations 31 1 Linear and Semilinear

More information

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur Module Stresses in machine elements Version M, IIT Kharagpur Lesson 3 Strain analsis Version M, IIT Kharagpur Instructional Objectives At the end of this lesson, the student should learn Normal and shear

More information

Aircraft Structures Structural & Loading Discontinuities

Aircraft Structures Structural & Loading Discontinuities Universit of Liège Aerospace & Mechanical Engineering Aircraft Structures Structural & Loading Discontinuities Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/

More information

Deflection of Beams. Equation of the Elastic Curve. Boundary Conditions

Deflection of Beams. Equation of the Elastic Curve. Boundary Conditions Deflection of Beams Equation of the Elastic Curve The governing second order differential equation for the elastic curve of a beam deflection is EI d d = where EI is the fleural rigidit, is the bending

More information

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL Mathematical and Computational Applications,Vol. 15, No. 4, pp. 742-761, 21. c Association for Scientific Research CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL R. Naz 1,

More information

Two-Dimensional Formulation.

Two-Dimensional Formulation. Two-Dimensional Formulation mi@seu.edu.cn Outline Introduction( 概论 ) Two vs. Three-Dimensional Problems Plane Strain( 平面应变 ) Plane Stress( 平面应力 ) Boundar Conditions( 边界条件 ) Correspondence between Plane

More information

Section 1.5 Formal definitions of limits

Section 1.5 Formal definitions of limits Section.5 Formal definitions of limits (3/908) Overview: The definitions of the various tpes of limits in previous sections involve phrases such as arbitraril close, sufficientl close, arbitraril large,

More information

4.1 Stress: The Creature and its Components

4.1 Stress: The Creature and its Components 4 Stress We have talked about internal forces, distributed them uniforml over an area and the became a normal stress acting perpendicular to some internal surface at a point, or a shear stress acting tangentiall,

More information

PHYS 101: Solutions to Chapter 4 Home Work

PHYS 101: Solutions to Chapter 4 Home Work PHYS 101: Solutions to Chapter 4 Home ork 3. EASONING In each case, we will appl Newton s second law. emember that it is the net force that appears in the second law. he net force is the vector sum of

More information

Stresses: Beams in Bending

Stresses: Beams in Bending CHAPTER 7 Stresses: Beams in Bending 7.1 General Remarks The organization of this chapter mimics that of the last chapter on torsion of circular shafts but the stor about stresses in beams is longer, covers

More information

Mechanics Departmental Exam Last updated November 2013

Mechanics Departmental Exam Last updated November 2013 Mechanics Departmental Eam Last updated November 213 1. Two satellites are moving about each other in circular orbits under the influence of their mutual gravitational attractions. The satellites have

More information

C. Non-linear Difference and Differential Equations: Linearization and Phase Diagram Technique

C. Non-linear Difference and Differential Equations: Linearization and Phase Diagram Technique C. Non-linear Difference and Differential Equations: Linearization and Phase Diaram Technique So far we have discussed methods of solvin linear difference and differential equations. Let us now discuss

More information

Exercise solutions: concepts from chapter 5

Exercise solutions: concepts from chapter 5 1) Stud the oöids depicted in Figure 1a and 1b. a) Assume that the thin sections of Figure 1 lie in a principal plane of the deformation. Measure and record the lengths and orientations of the principal

More information

In applications, we encounter many constrained optimization problems. Examples Basis pursuit: exact sparse recovery problem

In applications, we encounter many constrained optimization problems. Examples Basis pursuit: exact sparse recovery problem 1 Conve Analsis Main references: Vandenberghe UCLA): EECS236C - Optimiation methods for large scale sstems, http://www.seas.ucla.edu/ vandenbe/ee236c.html Parikh and Bod, Proimal algorithms, slides and

More information

Solution 11. Kinetics of rigid body(newton s Second Law)

Solution 11. Kinetics of rigid body(newton s Second Law) Solution () urpose and Requirement Solution Kinetics of rigid bod(newton s Second Law) In rob, kinematics stud regarding acceleration of mass center should be done before Newton s second law is used to

More information

Integration. 5.1 Antiderivatives and Indefinite Integration. Suppose that f(x) = 5x 4. Can we find a function F (x) whose derivative is f(x)?

Integration. 5.1 Antiderivatives and Indefinite Integration. Suppose that f(x) = 5x 4. Can we find a function F (x) whose derivative is f(x)? 5 Integration 5. Antiderivatives and Indefinite Integration Suppose that f() = 5 4. Can we find a function F () whose derivative is f()? Definition. A function F is an antiderivative of f on an interval

More information

2.2 SEPARABLE VARIABLES

2.2 SEPARABLE VARIABLES 44 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 6 Consider the autonomous DE 6 Use our ideas from Problem 5 to find intervals on the -ais for which solution curves are concave up and intervals for which

More information

Simultaneous Orthogonal Rotations Angle

Simultaneous Orthogonal Rotations Angle ELEKTROTEHNIŠKI VESTNIK 8(1-2): -11, 2011 ENGLISH EDITION Simultaneous Orthogonal Rotations Angle Sašo Tomažič 1, Sara Stančin 2 Facult of Electrical Engineering, Universit of Ljubljana 1 E-mail: saso.tomaic@fe.uni-lj.si

More information

Incompressible Viscous Flows

Incompressible Viscous Flows Incompressible Viscous Flows Q. Choose the crect answer (i) The maximum velocit of a one-dimensional incompressible full developed viscous flow between two fixed parallel plates is 6m/s. The mean velocit

More information

9/28/2009. t kz H a x. in free space. find the value(s) of k such that E satisfies both of Maxwell s curl equations.

9/28/2009. t kz H a x. in free space. find the value(s) of k such that E satisfies both of Maxwell s curl equations. 9//9 3- E3.1 For E E cos 6 1 tkz a in free space,, J=, find the value(s) of k such that E satisfies both of Mawell s curl equations. Noting that E E (z,t)a,we have from B E, t 3-1 a a a z B E t z E B E

More information

Functions of Several Variables

Functions of Several Variables Chapter 1 Functions of Several Variables 1.1 Introduction A real valued function of n variables is a function f : R, where the domain is a subset of R n. So: for each ( 1,,..., n ) in, the value of f is

More information

PHYSICS 1 Forces & Newton s Laws

PHYSICS 1 Forces & Newton s Laws Advanced Placement PHYSICS 1 Forces & Newton s Laws Presenter 2014-2015 Forces & Newton s Laws What I Absolutel Have to Know to Survive the AP* Exam Force is an push or pull. It is a vector. Newton s Second

More information

CHAPTER-III CONVECTION IN A POROUS MEDIUM WITH EFFECT OF MAGNETIC FIELD, VARIABLE FLUID PROPERTIES AND VARYING WALL TEMPERATURE

CHAPTER-III CONVECTION IN A POROUS MEDIUM WITH EFFECT OF MAGNETIC FIELD, VARIABLE FLUID PROPERTIES AND VARYING WALL TEMPERATURE CHAPER-III CONVECION IN A POROUS MEDIUM WIH EFFEC OF MAGNEIC FIELD, VARIABLE FLUID PROPERIES AND VARYING WALL EMPERAURE 3.1. INRODUCION Heat transer studies in porous media ind applications in several

More information

Statics Primer. Notation:

Statics Primer. Notation: Statics Primer Notation: a (C) d d d = name for acceleration = area (net = with holes, bearing = in contact, etc...) = shorthand for compression = perpendicular distance to a force from a point = difference

More information

Additional Topics in Differential Equations

Additional Topics in Differential Equations 0537_cop6.qd 0/8/08 :6 PM Page 3 6 Additional Topics in Differential Equations In Chapter 6, ou studied differential equations. In this chapter, ou will learn additional techniques for solving differential

More information

Answers !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!

Answers !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! 11 th Grade Phsics Workbook METU Development Foundation High School 1 Answers 11th Grade Chapter-1 Newton s Laws Motion Activit - 1.3.1 Applications of Newton s Laws 1. 2. Three blocks of masses 5 kg,

More information

acceleration of 2.4 m/s. (b) Now, we have two rubber bands (force 2F) pulling two glued objects (mass 2m). Using F ma, 2.0 furlongs x 2.0 s 2 4.

acceleration of 2.4 m/s. (b) Now, we have two rubber bands (force 2F) pulling two glued objects (mass 2m). Using F ma, 2.0 furlongs x 2.0 s 2 4. 5.. 5.6. Model: An object s acceleration is linearl proportional to the net force. Solve: (a) One rubber band produces a force F, two rubber bands produce a force F, and so on. Because F a and two rubber

More information

LECTURE 13 Strength of a Bar in Pure Bending

LECTURE 13 Strength of a Bar in Pure Bending V. DEMENKO MECHNCS OF MTERLS 015 1 LECTURE 13 Strength of a Bar in Pure Bending Bending is a tpe of loading under which bending moments and also shear forces occur at cross sections of a rod. f the bending

More information

Chapter 2 Basic Conservation Equations for Laminar Convection

Chapter 2 Basic Conservation Equations for Laminar Convection Chapter Basic Conservation Equations for Laminar Convection Abstract In this chapter, the basic conservation equations related to laminar fluid flow conservation equations are introduced. On this basis,

More information

roth t dive = 0 (4.2.3) divh = 0 (4.2.4) Chapter 4 Waves in Unbounded Medium Electromagnetic Sources 4.2 Uniform plane waves in free space

roth t dive = 0 (4.2.3) divh = 0 (4.2.4) Chapter 4 Waves in Unbounded Medium Electromagnetic Sources 4.2 Uniform plane waves in free space Chapter 4 Waves in Unbounded Medium 4. lectromagnetic Sources 4. Uniform plane waves in free space Mawell s equation in free space is given b: H rot = (4..) roth = (4..) div = (4..3) divh = (4..4) which

More information

2. Supports which resist forces in two directions. Fig Hinge. Rough Surface. Fig Rocker. Roller. Frictionless Surface

2. Supports which resist forces in two directions. Fig Hinge. Rough Surface. Fig Rocker. Roller. Frictionless Surface 4. Structural Equilibrium 4.1 ntroduction n statics, it becomes convenient to ignore the small deformation and displacement. We pretend that the materials used are rigid, having the propert or infinite

More information

Equilibrium of Rigid Bodies

Equilibrium of Rigid Bodies Equilibrium of Rigid Bodies 1 2 Contents Introduction Free-Bod Diagram Reactions at Supports and Connections for a wo-dimensional Structure Equilibrium of a Rigid Bod in wo Dimensions Staticall Indeterminate

More information

PHYS1100 Practice problem set, Chapter 8: 5, 9, 14, 20, 22, 25, 28, 30, 34, 35, 40, 44

PHYS1100 Practice problem set, Chapter 8: 5, 9, 14, 20, 22, 25, 28, 30, 34, 35, 40, 44 PHYS00 Practice problem set, Chapter 8: 5, 9, 4, 0,, 5, 8, 30, 34, 35, 40, 44 8.5. Solve: The top figure shows the pulle (P), block A, block B, the surface S of the incline, the rope (R), and the earth

More information

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x 5A galler of graphs Objectives To recognise the rules of a number of common algebraic relations: = = = (rectangular hperbola) + = (circle). To be able to sketch the graphs of these relations. To be able

More information

PHY 110 Handout I. Outline. Introduction

PHY 110 Handout I. Outline. Introduction Introduction PHY 110 Handout I Phsics is inherentl a science of measurement. It s a science dedicated to the stud of all natural phenomena. Phsics is a science whose objective is to stud the components

More information

1.3 LIMITS AT INFINITY; END BEHAVIOR OF A FUNCTION

1.3 LIMITS AT INFINITY; END BEHAVIOR OF A FUNCTION . Limits at Infinit; End Behavior of a Function 89. LIMITS AT INFINITY; END BEHAVIOR OF A FUNCTION Up to now we have been concerned with its that describe the behavior of a function f) as approaches some

More information

Equilibrium of Stress

Equilibrium of Stress Equilibrium f Stress Cnsider tw perpendicular planes passing thrugh a pint p. The stress cmpnents acting n these planes are as shwn in ig. 3.4.1a. These stresses are usuall shwn tgether acting n a small

More information

Math 214 Spring problem set (a) Consider these two first order equations. (I) dy dx = x + 1 dy

Math 214 Spring problem set (a) Consider these two first order equations. (I) dy dx = x + 1 dy Math 4 Spring 08 problem set. (a) Consider these two first order equations. (I) d d = + d (II) d = Below are four direction fields. Match the differential equations above to their direction fields. Provide

More information

ME 323 Examination #2 April 11, 2018

ME 323 Examination #2 April 11, 2018 ME 2 Eamination #2 April, 2 PROBLEM NO. 25 points ma. A thin-walled pressure vessel is fabricated b welding together two, open-ended stainless-steel vessels along a 6 weld line. The welded vessel has an

More information

σ = F/A. (1.2) σ xy σ yy σ zx σ xz σ yz σ, (1.3) The use of the opposite convention should cause no problem because σ ij = σ ji.

σ = F/A. (1.2) σ xy σ yy σ zx σ xz σ yz σ, (1.3) The use of the opposite convention should cause no problem because σ ij = σ ji. Cambridge Universit Press 978-1-107-00452-8 - Metal Forming: Mechanics Metallurg, Fourth Edition Ecerpt 1 Stress Strain An understing of stress strain is essential for the analsis of metal forming operations.

More information

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve:

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve: .2 INITIAL-VALUE PROBLEMS 3.2 INITIAL-VALUE PROBLEMS REVIEW MATERIAL Normal form of a DE Solution of a DE Famil of solutions INTRODUCTION We are often interested in problems in which we seek a solution

More information

FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING. Lectures AB = BA = I,

FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING. Lectures AB = BA = I, FACULTY OF MATHEMATICAL STUDIES MATHEMATICS FOR PART I ENGINEERING Lectures MODULE 7 MATRICES II Inverse of a matri Sstems of linear equations Solution of sets of linear equations elimination methods 4

More information

Transformation of kinematical quantities from rotating into static coordinate system

Transformation of kinematical quantities from rotating into static coordinate system Transformation of kinematical quantities from rotating into static coordinate sstem Dimitar G Stoanov Facult of Engineering and Pedagog in Sliven, Technical Universit of Sofia 59, Bourgasko Shaussee Blvd,

More information

Problem Set #1 Chapter 21 10, 22, 24, 43, 47, 63; Chapter 22 7, 10, 36. Chapter 21 Problems

Problem Set #1 Chapter 21 10, 22, 24, 43, 47, 63; Chapter 22 7, 10, 36. Chapter 21 Problems Problem Set #1 Chapter 1 10,, 4, 43, 47, 63; Chapter 7, 10, 36 Chapter 1 Problems 10. (a) T T m g m g (b) Before the charge is added, the cork balls are hanging verticall, so the tension is T 1 mg (0.10

More information