MEC-E8001 Finite Element Analysis, Exam (example) 2018
|
|
- Denis Kelly
- 5 years ago
- Views:
Transcription
1 MEC-E8 inite Element Analysis Exam (example) 8. ind the transverse displacement wx ( ) of the structure consisting of one beam element and point forces and. he rotations of the endpoints are assumed to be equal in magnitudes but opposite in directions i.e. π Y Y < π. Problem parameters E and I are constants. Zz / / / Xx. Derive the equations of motion of the bar structure shown in terms of axial displacements u X and u X. Use two linear bar elements. External distributed load vanishes and the cross-sectional area A is piecewise constant. EAρ EAρ p Xx. Beam structure of the figure is loaded by force p acting on node. Determine the buckling force p cr of the structure if beam is considered as rigid and displacements are confined to the xz plane. Cross-sectional properties A and I of beam and Young s modulus of the material E are constants. xx zz Yy 4. A thin rectangular slab (assume plane stress conditions) is loaded by a horizontal force and allowed to move horizontally at node whereas nodes and 4 are fixed. Derive the equilibrium equation for the structure according to large displacement theory by using two three-node triangle elements Material parameters C and thickness t at the initial geometry of the slab are constants. 4 Xx 5. A plate strip of width b is simply supported on two edges and free on the other two edges. he plate is assembled at constant temperature Ι. ind the transverse displacement when the upper side temperature is 4Ι and that of the lower side Ι. Assume that temperature does not depend on x or y and use approximation w( x y) < uz( x/ )( x/ ). Problem parameters E ρ and t are constants. Zz Xx
2 ind the transverse displacement wx ( ) of the structure consisting of one beam element and point forces and. he rotations of the endpoints are assumed to be equal in magnitudes but opposite in directions i.e. πy < πy. Problem parameters E and I are constants. Zz / / / Xx Virtual work expression of the internal forces int z 6h 6h uz y EI yy 6h 4h 6h h πy z h 6 6 z y πy χu χπ < χu h h u χπ 6h h 6h 4h is available in the formulae collection. However external part for forces is given only for a constant distributed force and point forces acting on the nodes. Here the point forces are acting inside the element. heir contribution follows from the definition of work but the virtual displacement need to be expressed in terms of the displacement and rotation of nodes by using the cubic approximation for bending. he active degrees of freedom are the rotations which satisfy πy < πy ( ω) ( ω) ( ω) ω π Y x w< < x( ) π ( ωω ) π ω ( ω ) Y Y x < x. χ w ( ) χπy At the points of action of the forces and χ w < ( ) χπy < χπy and 9 χ w < ( ) χπy < χπy. 9 herefore the virtual work expression of the point forces ext 4 < χπy χπy < χπy Virtual work expression of the internal forces simplifies to 6h 6h int χπ Y 6h 4h 6h h EI π Y EI < χπ 4 π 6h 6h < χπy 6h h 6h 4h πy Y Y Principle of virtual work and the fundamental lemma of variation calculus imply.
3 int ext EI 4 < < χπy(4 πy ) < 9 π Y <. 9 EI x w < x( ) 9 EI.
4 Derive the equations of motion of the bar structure shown in terms of axial displacements u X and u X. Use two linear bar elements. External distributed load vanishes and the cross-sectional area A is piecewise constant. Bar element contributions of the formulae collection are EAρ EAρ Xx int x EA ux χu < χu h u x x and ine x θah u%% x χu < χu 6. u%% x x rom the figure the nodal displacement of bar are u x < and ux < ux. herefore EA θa < ( ) χu u 6. u%% X X X he nodal displacement of bar are ux < ux and ux < ux. herefore X EA X θa %% X χu u u < ( ) χu u 6. u%% X X X Virtual work expression of the structure is the sum of element contributions X EA X θa 6 %% X χu u u < < ( ) χu u 6. u%% X X X Principle of virtual work <! χa and the fundamental lemma of variation calculus χa <! χa < imply that EA ux θa 6 u%% X < u 6. u%% X X
5 Beam structure of the figure is loaded by force p acting on node. Determine the buckling force p cr of the structure if beam is considered as rigid and displacements are confined to the xz plane. Cross-sectional properties A and I of beam and Young s modulus of the material E are constants. he normal force N < p can be deduced without any calculations. Since beam is rigid the displacement and rotations of nodes and are related by πy < πy and uz < πy. et us consider π as the active degree of freedom of the structure. Element contribution for beam taking into Y account the beam bending mode and the interaction of the bar and beam bending modes is given by p xx zz EI p < ( ) χπ Y π Y χπ Y π Y Y EI 6 p 6 πy χπ < ( ) χπ π Y Y EI p < χπ ( 8 46) π Y Y Principle of virtual work and the fundamental lemma of variation calculus imply the equation system EI p ( 8 46) πy <. Clearly either rotation or its multiplier needs to vanish. he critical value of the loading parameter p making the solution non-unique is given by the latter option EI p 8 46 < p 4 EI EI <. cr. 85ο
6 Yy A thin rectangular slab (assume plane stress conditions) loaded by a horizontal force is allowed to move horizontally at node and nodes and 4 are fixed. Derive the equilibrium equation for the structure according to large displacement theory by using two three-node triangle elements Material parameters C and thickness t at the initial geometry of the slab are constants. 4 Xx Virtual work density of internal force when modified for large displacement analysis with the same constitutive equation as in the linear case of plane stress is given by χ E xx E xx E xx u x u x u xu x v xv x int tc χwς χ E yy < E yy Eyy < v y v y u yu y v yv y. χe ( )/ xy Exy Exy u y v x u xu y v xv y As all the nodes of element are fixed it is enough to consider element. et us start with the approximations and the corresponding components of the Green-agrange strain. inear shape functions can be deduced from the figure. Only the shape function N < ( x/ y/ ) of node is needed. Displacement components v < w < and x y u < ( ) u X u u X x < u y < < a E xx Eyy < a a E xy and χ E xx χeyy < χa( a ) χe xy When the strain component expression is substituted there virtual work density simplifies to int tc χwς < χ a( a ) ( a a ). ( )/ erm by term calculation int tc tc ( χwς ) < χ a a χa a < ( )/ tc tc ( χw ) χ a a χa a ( )/ int ς < <
7 tc tc ( χw ) χ aa a χa a ( )/ int ς < < tc tc ( χw ) χ aa a χa a ( )/ int ς 4 < <. Virtual work density is the sum of the terms. Virtual work expression of internal forces follows after integration over the element tc a a( a a ). < χ Virtual work expression of the point force follows from the definition of work < χu < χ. X a Virtual work expression of the structure is obtained as sum over the element contributions tc < < χa[ a( a a ) ]. Principle of virtual work and the fundamental lemma of variation calculus imply the equilibrium equation tc a( a a ) <.
8 A plate strip of width b is simply supported on two edges and free on the other two edges. he plate is assembled at constant temperature Ι. ind the transverse displacement when the upper side temperature is 4Ι and that of the lower side Ι. Assume that temperature does not depend on x or y and use approximation w( x y) < uz( x/ )( x/ ). Problem parameters E ρ and t are constants. Zz Xx Assuming that the material coordinate system is chosen so that the plate bending and thin slab modes decouple in the linear analysis the Kirchhoff plate model virtual work densities of internal force and coupling terms are given by χ w xx w xx int χw χ w yy D ς < w yy χw ( )/ xy w xy where t E D < cpl χ w xx E χwς < z Ιdz χ w Χ. yy he coupling term contains an integral of temperature over the thickness of the plate. Approximation to the transverse displacement and its derivatives are x x w( x y) < uz ( ) w u < and w yy < w xy <. xx Z emperature difference and its weighted integral over the thickness (integral of the coupling term) z z z Χ Ι < Ι( z) Ι < ( ) Ι ( )4Ι Ι < Ι t t t z zχ Ιdz < z Ι dz < Ι t t 6 t/ t/. t/ t/ When the approximation to the transverse displacement is substituted there virtual work densities of the internal and the coupling parts simplify to int D χwς < χuz4 u 4 Z and cpl Ι t E χwς < χuz. Virtual work expressions are integrals of the densities over the domain occupied by the plate/element int bd < χw dxdy < χu u b int ς Z4 Z
9 cpl b cpl b E < χw dxdy u ς < χ Z Ι t. Virtual work expression is the sum of the parts int cpl b D E < < χuz [4 u Z Ι t ]. Principle of virtual work χ W <! χ a and the fundamental lemma of variation calculus give D E u Z Ι t < 4 uz < Ι ( ). t
4 NON-LINEAR ANALYSIS
4 NON-INEAR ANAYSIS arge displacement elasticity theory, principle of virtual work arge displacement FEA with solid, thin slab, and bar models Virtual work density of internal forces revisited 4-1 SOURCES
More informationMEC-E8001 FINITE ELEMENT ANALYSIS
MEC-E800 FINIE EEMEN ANAYSIS 07 - WHY FINIE EEMENS AND IS HEORY? Design of machines and structures: Solution to stress or displacement by analytical method is often impossible due to complex geometry,
More informationABHELSINKI UNIVERSITY OF TECHNOLOGY
ABHELSINKI UNIVERSITY OF TECHNOLOGY TECHNISCHE UNIVERSITÄT HELSINKI UNIVERSITE DE TECHNOLOGIE D HELSINKI A posteriori error analysis for the Morley plate element Jarkko Niiranen Department of Structural
More informationExample 3.7 Consider the undeformed configuration of a solid as shown in Figure 3.60.
162 3. The linear 3-D elasticity mathematical model The 3-D elasticity model is of great importance, since it is our highest order hierarchical model assuming linear elastic behavior. Therefore, it provides
More informationChapter 12 Plate Bending Elements. Chapter 12 Plate Bending Elements
CIVL 7/8117 Chapter 12 - Plate Bending Elements 1/34 Chapter 12 Plate Bending Elements Learning Objectives To introduce basic concepts of plate bending. To derive a common plate bending element stiffness
More informationMEC-E8001 Finite Element Analysis, Exam (example) 2017
MEC-E800 Finite Element Analysis Eam (eample) 07. Find the transverse displacement w() of the strctre consisting of one beam element and po forces and. he rotations of the endpos are assmed to be eqal
More informationFinite Element Method in Geotechnical Engineering
Finite Element Method in Geotechnical Engineering Short Course on + Dynamics Boulder, Colorado January 5-8, 2004 Stein Sture Professor of Civil Engineering University of Colorado at Boulder Contents Steps
More informationStress analysis of a stepped bar
Stress analysis of a stepped bar Problem Find the stresses induced in the axially loaded stepped bar shown in Figure. The bar has cross-sectional areas of A ) and A ) over the lengths l ) and l ), respectively.
More informationQuintic beam closed form matrices (revised 2/21, 2/23/12) General elastic beam with an elastic foundation
General elastic beam with an elastic foundation Figure 1 shows a beam-column on an elastic foundation. The beam is connected to a continuous series of foundation springs. The other end of the foundation
More informationCIV-E1060 Engineering Computation and Simulation Examination, December 12, 2017 / Niiranen
CIV-E16 Engineering Computation and Simulation Examination, December 12, 217 / Niiranen This examination consists of 3 problems rated by the standard scale 1...6. Problem 1 Let us consider a long and tall
More informationUnit 13 Review of Simple Beam Theory
MIT - 16.0 Fall, 00 Unit 13 Review of Simple Beam Theory Readings: Review Unified Engineering notes on Beam Theory BMP 3.8, 3.9, 3.10 T & G 10-15 Paul A. Lagace, Ph.D. Professor of Aeronautics & Astronautics
More informationInstitute of Structural Engineering Page 1. Method of Finite Elements I. Chapter 2. The Direct Stiffness Method. Method of Finite Elements I
Institute of Structural Engineering Page 1 Chapter 2 The Direct Stiffness Method Institute of Structural Engineering Page 2 Direct Stiffness Method (DSM) Computational method for structural analysis Matrix
More informationFINAL EXAMINATION. (CE130-2 Mechanics of Materials)
UNIVERSITY OF CLIFORNI, ERKELEY FLL SEMESTER 001 FINL EXMINTION (CE130- Mechanics of Materials) Problem 1: (15 points) pinned -bar structure is shown in Figure 1. There is an external force, W = 5000N,
More information3D Elasticity Theory
3D lasticity Theory Many structural analysis problems are analysed using the theory of elasticity in which Hooke s law is used to enforce proportionality between stress and strain at any deformation level.
More informationPost Graduate Diploma in Mechanical Engineering Computational mechanics using finite element method
9210-220 Post Graduate Diploma in Mechanical Engineering Computational mechanics using finite element method You should have the following for this examination one answer book scientific calculator No
More informationHIGHER-ORDER THEORIES
HIGHER-ORDER THEORIES THIRD-ORDER SHEAR DEFORMATION PLATE THEORY LAYERWISE LAMINATE THEORY J.N. Reddy 1 Third-Order Shear Deformation Plate Theory Assumed Displacement Field µ u(x y z t) u 0 (x y t) +
More informationReview of Strain Energy Methods and Introduction to Stiffness Matrix Methods of Structural Analysis
uke University epartment of Civil and Environmental Engineering CEE 42L. Matrix Structural Analysis Henri P. Gavin Fall, 22 Review of Strain Energy Methods and Introduction to Stiffness Matrix Methods
More informationGeneral elastic beam with an elastic foundation
General elastic beam with an elastic foundation Figure 1 shows a beam-column on an elastic foundation. The beam is connected to a continuous series of foundation springs. The other end of the foundation
More informationChapter 3 Variational Formulation & the Galerkin Method
Institute of Structural Engineering Page 1 Chapter 3 Variational Formulation & the Galerkin Method Institute of Structural Engineering Page 2 Today s Lecture Contents: Introduction Differential formulation
More informationM5 Simple Beam Theory (continued)
M5 Simple Beam Theory (continued) Reading: Crandall, Dahl and Lardner 7.-7.6 In the previous lecture we had reached the point of obtaining 5 equations, 5 unknowns by application of equations of elasticity
More informationInstitute of Structural Engineering Page 1. Method of Finite Elements I. Chapter 2. The Direct Stiffness Method. Method of Finite Elements I
Institute of Structural Engineering Page 1 Chapter 2 The Direct Stiffness Method Institute of Structural Engineering Page 2 Direct Stiffness Method (DSM) Computational method for structural analysis Matrix
More informationVariational principles in mechanics
CHAPTER Variational principles in mechanics.1 Linear Elasticity n D Figure.1: A domain and its boundary = D [. Consider a domain Ω R 3 with its boundary = D [ of normal n (see Figure.1). The problem of
More information7. Hierarchical modeling examples
7. Hierarchical modeling examples The objective of this chapter is to apply the hierarchical modeling approach discussed in Chapter 1 to three selected problems using the mathematical models studied in
More informationSymmetric Bending of Beams
Symmetric Bending of Beams beam is any long structural member on which loads act perpendicular to the longitudinal axis. Learning objectives Understand the theory, its limitations and its applications
More informationLevel 7 Postgraduate Diploma in Engineering Computational mechanics using finite element method
9210-203 Level 7 Postgraduate Diploma in Engineering Computational mechanics using finite element method You should have the following for this examination one answer book No additional data is attached
More informationUNIVERSITY OF SASKATCHEWAN ME MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 13, 2008 Professor A. Dolovich
UNIVERSITY OF SASKATCHEWAN ME 313.3 MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 13, 2008 Professor A. Dolovich A CLOSED BOOK EXAMINATION TIME: 3 HOURS For Marker s Use Only LAST NAME (printed): FIRST
More informationDecember 10, PROBLEM NO points max.
PROBLEM NO. 1 25 points max. PROBLEM NO. 2 25 points max. B 3A A C D A H k P L 2L Given: Consider the structure above that is made up of rod segments BC and DH, a spring of stiffness k and rigid connectors
More informationLecture 8. Stress Strain in Multi-dimension
Lecture 8. Stress Strain in Multi-dimension Module. General Field Equations General Field Equations [] Equilibrium Equations in Elastic bodies xx x y z yx zx f x 0, etc [2] Kinematics xx u x x,etc. [3]
More informationNONLINEAR CONTINUUM FORMULATIONS CONTENTS
NONLINEAR CONTINUUM FORMULATIONS CONTENTS Introduction to nonlinear continuum mechanics Descriptions of motion Measures of stresses and strains Updated and Total Lagrangian formulations Continuum shell
More informationFREE VIBRATION OF AXIALLY LOADED FUNCTIONALLY GRADED SANDWICH BEAMS USING REFINED SHEAR DEFORMATION THEORY
FREE VIBRATION OF AXIALLY LOADED FUNCTIONALLY GRADED SANDWICH BEAMS USING REFINED SHEAR DEFORMATION THEORY Thuc P. Vo 1, Adelaja Israel Osofero 1, Marco Corradi 1, Fawad Inam 1 1 Faculty of Engineering
More informationCIVL 8/7117 Chapter 12 - Structural Dynamics 1/75. To discuss the dynamics of a single-degree-of freedom springmass
CIV 8/77 Chapter - /75 Introduction To discuss the dynamics of a single-degree-of freedom springmass system. To derive the finite element equations for the time-dependent stress analysis of the one-dimensional
More information3 2 6 Solve the initial value problem u ( t) 3. a- If A has eigenvalues λ =, λ = 1 and corresponding eigenvectors 1
Math Problem a- If A has eigenvalues λ =, λ = 1 and corresponding eigenvectors 1 3 6 Solve the initial value problem u ( t) = Au( t) with u (0) =. 3 1 u 1 =, u 1 3 = b- True or false and why 1. if A is
More informationLecture 7: The Beam Element Equations.
4.1 Beam Stiffness. A Beam: A long slender structural component generally subjected to transverse loading that produces significant bending effects as opposed to twisting or axial effects. MECH 40: Finite
More informationHIGHER-ORDER THEORIES
HIGHER-ORDER THEORIES Third-order Shear Deformation Plate Theory Displacement and strain fields Equations of motion Navier s solution for bending Layerwise Laminate Theory Interlaminar stress and strain
More informationFinite Element Analysis Prof. Dr. B. N. Rao Department of Civil Engineering Indian Institute of Technology, Madras. Module - 01 Lecture - 11
Finite Element Analysis Prof. Dr. B. N. Rao Department of Civil Engineering Indian Institute of Technology, Madras Module - 01 Lecture - 11 Last class, what we did is, we looked at a method called superposition
More informationSEMM Mechanics PhD Preliminary Exam Spring Consider a two-dimensional rigid motion, whose displacement field is given by
SEMM Mechanics PhD Preliminary Exam Spring 2014 1. Consider a two-dimensional rigid motion, whose displacement field is given by u(x) = [cos(β)x 1 + sin(β)x 2 X 1 ]e 1 + [ sin(β)x 1 + cos(β)x 2 X 2 ]e
More informationDue Monday, September 14 th, 12:00 midnight
Due Monday, September 14 th, 1: midnight This homework is considering the analysis of plane and space (3D) trusses as discussed in class. A list of MatLab programs that were discussed in class is provided
More informationPart D: Frames and Plates
Part D: Frames and Plates Plane Frames and Thin Plates A Beam with General Boundary Conditions The Stiffness Method Thin Plates Initial Imperfections The Ritz and Finite Element Approaches A Beam with
More information2 Introduction to mechanics
21 Motivation Thermodynamic bodies are being characterized by two competing opposite phenomena, energy and entropy which some researchers in thermodynamics would classify as cause and chance or determinancy
More informationIntroduction, Basic Mechanics 2
Computational Biomechanics 18 Lecture : Introduction, Basic Mechanics Ulli Simon, Lucas Engelhardt, Martin Pietsch Scientific Computing Centre Ulm, UZWR Ulm University Contents Mechanical Basics Moment
More informationVerification Examples. FEM-Design. version
FEM-Design 6.0 FEM-Design version. 06 FEM-Design 6.0 StruSoft AB Visit the StruSoft website for company and FEM-Design information at www.strusoft.com Copyright 06 by StruSoft, all rights reserved. Trademarks
More informationCRITERIA FOR SELECTION OF FEM MODELS.
CRITERIA FOR SELECTION OF FEM MODELS. Prof. P. C.Vasani,Applied Mechanics Department, L. D. College of Engineering,Ahmedabad- 380015 Ph.(079) 7486320 [R] E-mail:pcv-im@eth.net 1. Criteria for Convergence.
More informationCHAPTER 5. Beam Theory
CHPTER 5. Beam Theory SangJoon Shin School of Mechanical and erospace Engineering Seoul National University ctive eroelasticity and Rotorcraft Lab. 5. The Euler-Bernoulli assumptions One of its dimensions
More informationChapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING )
Chapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING ) 5.1 DEFINITION A construction member is subjected to centric (axial) tension or compression if in any cross section the single distinct stress
More informationAnalytical Mechanics: Elastic Deformation
Analytical Mechanics: Elastic Deformation Shinichi Hirai Dept. Robotics, Ritsumeikan Univ. Shinichi Hirai (Dept. Robotics, Ritsumeikan Univ.) Analytical Mechanics: Elastic Deformation 1 / 60 Agenda Agenda
More informationFinite Element Method-Part II Isoparametric FE Formulation and some numerical examples Lecture 29 Smart and Micro Systems
Finite Element Method-Part II Isoparametric FE Formulation and some numerical examples Lecture 29 Smart and Micro Systems Introduction Till now we dealt only with finite elements having straight edges.
More informationBasic Equations of Elasticity
A Basic Equations of Elasticity A.1 STRESS The state of stress at any point in a loaded bo is defined completely in terms of the nine components of stress: σ xx,σ yy,σ zz,σ xy,σ yx,σ yz,σ zy,σ zx,andσ
More informationFinite Element Analysis Prof. Dr. B. N. Rao Department of Civil Engineering Indian Institute of Technology, Madras. Module - 01 Lecture - 13
Finite Element Analysis Prof. Dr. B. N. Rao Department of Civil Engineering Indian Institute of Technology, Madras (Refer Slide Time: 00:25) Module - 01 Lecture - 13 In the last class, we have seen how
More informationModule 4 : Deflection of Structures Lecture 4 : Strain Energy Method
Module 4 : Deflection of Structures Lecture 4 : Strain Energy Method Objectives In this course you will learn the following Deflection by strain energy method. Evaluation of strain energy in member under
More informationChapter 5 Elastic Strain, Deflection, and Stability 1. Elastic Stress-Strain Relationship
Chapter 5 Elastic Strain, Deflection, and Stability Elastic Stress-Strain Relationship A stress in the x-direction causes a strain in the x-direction by σ x also causes a strain in the y-direction & z-direction
More information1 Static Plastic Behaviour of Beams
1 Static Plastic Behaviour of Beams 1.1 Introduction Many ductile materials which are used in engineering practice have a considerable reserve capacity beyond the initial yield condition. The uniaxial
More informationInternational Journal of Advanced Engineering Technology E-ISSN
Research Article INTEGRATED FORCE METHOD FOR FIBER REINFORCED COMPOSITE PLATE BENDING PROBLEMS Doiphode G. S., Patodi S. C.* Address for Correspondence Assistant Professor, Applied Mechanics Department,
More informationUsing the finite element method of structural analysis, determine displacements at nodes 1 and 2.
Question 1 A pin-jointed plane frame, shown in Figure Q1, is fixed to rigid supports at nodes and 4 to prevent their nodal displacements. The frame is loaded at nodes 1 and by a horizontal and a vertical
More informationLecture 8: Assembly of beam elements.
ecture 8: Assembly of beam elements. 4. Example of Assemblage of Beam Stiffness Matrices. Place nodes at the load application points. Assembling the two sets of element equations (note the common elemental
More informationHydroelastic vibration of a rectangular perforated plate with a simply supported boundary condition
Fluid Structure Interaction and Moving Boundary Problems IV 63 Hydroelastic vibration of a rectangular perforated plate with a simply supported boundary condition K.-H. Jeong, G.-M. Lee, T.-W. Kim & J.-I.
More information4 Finite Element Method for Trusses
4 Finite Element Method for Trusses To solve the system of linear equations that arises in IPM, it is necessary to assemble the geometric matrix B a. For the sake of simplicity, the applied force vector
More informationIf you take CT5143 instead of CT4143 then write this at the first of your answer sheets and skip problem 4 and 6.
Delft University of Technology Faculty of Civil Engineering and Geosciences Structural Mechanics Section Write your name and study number at the top right-hand of your work. Exam CT4143 Shell Analysis
More informationEsben Byskov. Elementary Continuum. Mechanics for Everyone. With Applications to Structural Mechanics. Springer
Esben Byskov Elementary Continuum Mechanics for Everyone With Applications to Structural Mechanics Springer Contents Preface v Contents ix Introduction What Is Continuum Mechanics? "I Need Continuum Mechanics
More informationCOMPRESSION AND BENDING STIFFNESS OF FIBER-REINFORCED ELASTOMERIC BEARINGS. Abstract. Introduction
COMPRESSION AND BENDING STIFFNESS OF FIBER-REINFORCED ELASTOMERIC BEARINGS Hsiang-Chuan Tsai, National Taiwan University of Science and Technology, Taipei, Taiwan James M. Kelly, University of California,
More informationChapter 5 Structural Elements: The truss & beam elements
Institute of Structural Engineering Page 1 Chapter 5 Structural Elements: The truss & beam elements Institute of Structural Engineering Page 2 Chapter Goals Learn how to formulate the Finite Element Equations
More informationWorkshop 8. Lateral Buckling
Workshop 8 Lateral Buckling cross section A transversely loaded member that is bent about its major axis may buckle sideways if its compression flange is not laterally supported. The reason buckling occurs
More informationDesign Project 1 Design of a Cheap Thermal Switch
Design Project 1 Design of a Cheap Thermal Switch ENGR 0135 Statics and Mechanics of Materials 1 October 20 th, 2015 Professor: Dr. Guofeng Wang Group Members: Chad Foster Thomas Hinds Kyungchul Yoon John
More informationTwo Posts to Fill On School Board
Y Y 9 86 4 4 qz 86 x : ( ) z 7 854 Y x 4 z z x x 4 87 88 Y 5 x q x 8 Y 8 x x : 6 ; : 5 x ; 4 ( z ; ( ) ) x ; z 94 ; x 3 3 3 5 94 ; ; ; ; 3 x : 5 89 q ; ; x ; x ; ; x : ; ; ; ; ; ; 87 47% : () : / : 83
More informationINTRODUCTION TO STRAIN
SIMPLE STRAIN INTRODUCTION TO STRAIN In general terms, Strain is a geometric quantity that measures the deformation of a body. There are two types of strain: normal strain: characterizes dimensional changes,
More informationBasic Energy Principles in Stiffness Analysis
Basic Energy Principles in Stiffness Analysis Stress-Strain Relations The application of any theory requires knowledge of the physical properties of the material(s) comprising the structure. We are limiting
More information4. Mathematical models used in engineering structural analysis
4. Mathematical models used in engineering structural analysis In this chapter we pursue a formidable task to present the most important mathematical models in structural mechanics. In order to best situate
More informationThe CR Formulation: BE Plane Beam
6 The CR Formulation: BE Plane Beam 6 Chapter 6: THE CR FORMUATION: BE PANE BEAM TABE OF CONTENTS Page 6. Introduction..................... 6 4 6.2 CR Beam Kinematics................. 6 4 6.2. Coordinate
More informationMechanics PhD Preliminary Spring 2017
Mechanics PhD Preliminary Spring 2017 1. (10 points) Consider a body Ω that is assembled by gluing together two separate bodies along a flat interface. The normal vector to the interface is given by n
More informationLOWELL JOURNAL. MUST APOLOGIZE. such communication with the shore as Is m i Boimhle, noewwary and proper for the comfort
- 7 7 Z 8 q ) V x - X > q - < Y Y X V - z - - - - V - V - q \ - q q < -- V - - - x - - V q > x - x q - x q - x - - - 7 -» - - - - 6 q x - > - - x - - - x- - - q q - V - x - - ( Y q Y7 - >»> - x Y - ] [
More informationJEPPIAAR ENGINEERING COLLEGE
JEPPIAAR ENGINEERING COLLEGE Jeppiaar Nagar, Rajiv Gandhi Salai 600 119 DEPARTMENT OFMECHANICAL ENGINEERING QUESTION BANK VI SEMESTER ME6603 FINITE ELEMENT ANALYSIS Regulation 013 SUBJECT YEAR /SEM: III
More informationIV B.Tech. I Semester Supplementary Examinations, February/March FINITE ELEMENT METHODS (Mechanical Engineering) Time: 3 Hours Max Marks: 80
www..com www..com Code No: M0322/R07 Set No. 1 IV B.Tech. I Semester Supplementary Examinations, February/March - 2011 FINITE ELEMENT METHODS (Mechanical Engineering) Time: 3 Hours Max Marks: 80 Answer
More informationME 475 Modal Analysis of a Tapered Beam
ME 475 Modal Analysis of a Tapered Beam Objectives: 1. To find the natural frequencies and mode shapes of a tapered beam using FEA.. To compare the FE solution to analytical solutions of the vibratory
More informationVirtual Work and Variational Principles
Virtual Work and Principles Mathematically, the structural analysis problem is a boundary value problem (BVP). Forces, displacements, stresses, and strains are connected and computed within the framework
More informationSlender Structures Load carrying principles
Slender Structures Load carrying principles Basic cases: Extension, Shear, Torsion, Cable Bending (Euler) v017-1 Hans Welleman 1 Content (preliminary schedule) Basic cases Extension, shear, torsion, cable
More informationBending of Simply Supported Isotropic and Composite Laminate Plates
Bending of Simply Supported Isotropic and Composite Laminate Plates Ernesto Gutierrez-Miravete 1 Isotropic Plates Consider simply a supported rectangular plate of isotropic material (length a, width b,
More informationNonconservative Loading: Overview
35 Nonconservative Loading: Overview 35 Chapter 35: NONCONSERVATIVE LOADING: OVERVIEW TABLE OF CONTENTS Page 35. Introduction..................... 35 3 35.2 Sources...................... 35 3 35.3 Three
More informationChapter 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 informationUniversity of Groningen
University of Groningen Nature-inspired microfluidic propulsion using magnetic actuation Khaderi, S. N.; Baltussen, M. G. H. M.; Anderson, P. D.; Ioan, D.; den Toonder, J.M.J.; Onck, Patrick Published
More informationENGN2340 Final Project: Implementation of a Euler-Bernuolli Beam Element Michael Monn
ENGN234 Final Project: Implementation of a Euler-Bernuolli Beam Element Michael Monn 12/11/13 Problem Definition and Shape Functions Although there exist many analytical solutions to the Euler-Bernuolli
More informationMAE 323: Chapter 6. Structural Models
Common element types for structural analyis: oplane stress/strain, Axisymmetric obeam, truss,spring oplate/shell elements o3d solid ospecial: Usually used for contact or other constraints What you need
More informationStructural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian
Structural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian ahmadian@iust.ac.ir Dynamic Response of MDOF Systems: Mode-Superposition Method Mode-Superposition Method:
More informationTable of Contents. Preface... 13
Table of Contents Preface... 13 Chapter 1. Vibrations of Continuous Elastic Solid Media... 17 1.1. Objective of the chapter... 17 1.2. Equations of motion and boundary conditions of continuous media...
More informationMechanical Properties of Materials
Mechanical Properties of Materials Strains Material Model Stresses Learning objectives Understand the qualitative and quantitative description of mechanical properties of materials. Learn the logic of
More informationM.S Comprehensive Examination Analysis
UNIVERSITY OF CALIFORNIA, BERKELEY Spring Semester 2014 Dept. of Civil and Environmental Engineering Structural Engineering, Mechanics and Materials Name:......................................... M.S Comprehensive
More information3. Stability of built-up members in compression
3. Stability of built-up members in compression 3.1 Definitions Build-up members, made out by coupling two or more simple profiles for obtaining stronger and stiffer section are very common in steel structures,
More informationQuestion 1. Ignore bottom surface. Solution: Design variables: X = (R, H) Objective function: maximize volume, πr 2 H OR Minimize, f(x) = πr 2 H
Question 1 (Problem 2.3 of rora s Introduction to Optimum Design): Design a beer mug, shown in fig, to hold as much beer as possible. The height and radius of the mug should be not more than 20 cm. The
More informationConsider an elastic spring as shown in the Fig.2.4. When the spring is slowly
.3 Strain Energy Consider an elastic spring as shown in the Fig..4. When the spring is slowly pulled, it deflects by a small amount u 1. When the load is removed from the spring, it goes back to the original
More informationD : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each.
GTE 2016 Q. 1 Q. 9 carry one mark each. D : SOLID MECHNICS Q.1 single degree of freedom vibrating system has mass of 5 kg, stiffness of 500 N/m and damping coefficient of 100 N-s/m. To make the system
More informationCIVL4332 L1 Introduction to Finite Element Method
CIVL L Introduction to Finite Element Method CIVL L Introduction to Finite Element Method by Joe Gattas, Faris Albermani Introduction The FEM is a numerical technique for solving physical problems such
More informationCorrection of local-linear elasticity for nonlocal residuals: Application to Euler-Bernoulli beams
Correction of local-linear elasticity for nonlocal residuals: Application to Euler-Bernoulli beams Mohamed Shaat* Engineering and Manufacturing Technologies Department, DACC, New Mexico State University,
More informationME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.
ME 323 - Final Exam Name December 15, 2015 Instructor (circle) PROEM NO. 4 Part A (2 points max.) Krousgrill 11:30AM-12:20PM Ghosh 2:30-3:20PM Gonzalez 12:30-1:20PM Zhao 4:30-5:20PM M (x) y 20 kip ft 0.2
More informationGyroscopic matrixes of the straight beams and the discs
Titre : Matrice gyroscopique des poutres droites et des di[...] Date : 29/05/2013 Page : 1/12 Gyroscopic matrixes of the straight beams and the discs Summarized: This document presents the formulation
More informationME FINITE ELEMENT ANALYSIS FORMULAS
ME 2353 - FINITE ELEMENT ANALYSIS FORMULAS UNIT I FINITE ELEMENT FORMULATION OF BOUNDARY VALUE PROBLEMS 01. Global Equation for Force Vector, {F} = [K] {u} {F} = Global Force Vector [K] = Global Stiffness
More informationUNCONVENTIONAL FINITE ELEMENT MODELS FOR NONLINEAR ANALYSIS OF BEAMS AND PLATES
UNCONVENTIONAL FINITE ELEMENT MODELS FOR NONLINEAR ANALYSIS OF BEAMS AND PLATES A Thesis by WOORAM KIM Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the
More informationPrepared by M. GUNASHANKAR AP/MECH DEPARTMENT OF MECHANICAL ENGINEERING
CHETTINAD COLLEGE OF ENGINEERING AND TECHNOLOGY-KARUR FINITE ELEMENT ANALYSIS 2 MARKS QUESTIONS WITH ANSWER Prepared by M. GUNASHANKAR AP/MECH DEPARTMENT OF MECHANICAL ENGINEERING FINITE ELEMENT ANALYSIS
More informationFLEXIBILITY METHOD FOR INDETERMINATE FRAMES
UNIT - I FLEXIBILITY METHOD FOR INDETERMINATE FRAMES 1. What is meant by indeterminate structures? Structures that do not satisfy the conditions of equilibrium are called indeterminate structure. These
More informationSteps in the Finite Element Method. Chung Hua University Department of Mechanical Engineering Dr. Ching I Chen
Steps in the Finite Element Method Chung Hua University Department of Mechanical Engineering Dr. Ching I Chen General Idea Engineers are interested in evaluating effects such as deformations, stresses,
More informationMITOCW MITRES2_002S10linear_lec07_300k-mp4
MITOCW MITRES2_002S10linear_lec07_300k-mp4 The following content is provided under a Creative Commons license. Your support will help MIT OpenCourseWare continue to offer high quality educational resources
More informationHomework No. 1 MAE/CE 459/559 John A. Gilbert, Ph.D. Fall 2004
Homework No. 1 MAE/CE 459/559 John A. Gilbert, Ph.D. 1. A beam is loaded as shown. The dimensions of the cross section appear in the insert. the figure. Draw a complete free body diagram showing an equivalent
More information