MECHANICS OF MATERIALS

Size: px
Start display at page:

Download "MECHANICS OF MATERIALS"

Transcription

1 Fifth SI Edition CHTER 1 MECHNICS OF MTERILS Ferdinand. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Introduction Concept of Stress Lecture Notes: J. Walt Oler Teas Tech University

2 Contents Concept of Stress Review of Statics Structure Free-Body Diagram Component Free-Body Diagram Method of Joints Stress nalysis Design ial Loading: Normal Stress Centric & Eccentric Loading Shearing Stress Shearing Stress Eamples Bearing Stress in Connections Stress nalysis & Design Eample Rod & Boom Normal Stresses in Shearing Stresses in Bearing Stresses Stress in Two Force Members Stress on an Oblique lane Maimum Stresses Stress Under General Loadings State of Stress Factor of Safety 1-

3 Concept of Stress The main objective of the study of the mechanics of materials is to provide the future engineer with the means of analyzing and designing various machines and load bearing structures. Both the analysis and design of a given structure involve the determination of stresses and deformations. This chapter is devoted to the concept of stress. 1-3

4 Review of Statics The structure is designed to support a 30 kn load The structure consists of a boom and rod joined by pins (zero moment connections) at the junctions and supports erform a static analysis to determine the internal force in each structural member and the reaction forces at the supports 1-4

5 Structure Free-Body Diagram Structure is detached from supports and the loads and reaction forces are indicated Conditions for static equilibrium: M 0 ( 0.6m) ( 30kN)( 0.8m) F C F y y C 40kN 0 + C y 0 30kN y and C y can not be determined from these equations + C 40kN y + C y 30kN 0 1-5

6 Component Free-Body Diagram In addition to the complete structure, each component must satisfy the conditions for static equilibrium Consider a free-body diagram for the boom: M 0 ( 0.8m) y C y B 0 30kN y substitute into the structure equilibrium equation Results: 40kN C 40kN Cy 30kN Reaction forces are directed along boom and rod 1-6

7 Method of Joints The boom and rod are -force members, i.e., the members are subjected to only two forces which are applied at member ends For equilibrium, the forces must be parallel to to an ais between the force application points, equal in magnitude, and in opposite directions Joints must satisfy the conditions for static equilibrium which may be epressed in the form of a force triangle: F 4 F F B B B 0 F 5 BC 40kN 30kN 3 F BC 50kN 1-7

8 Stress nalysis Can the structure safely support the 30 kn load? From a statics analysis F B 40 kn (compression) F BC 50 kn (tension) d BC 0 mm t any section through member BC, the internal force is 50 kn with a force intensity or stress of σ BC N m 159 Ma From the material properties for steel, the allowable stress is σ all 165 Ma Conclusion: the strength of member BC is adequate 1-8

9 Design Design of new structures requires selection of appropriate materials and component dimensions to meet performance requirements For reasons based on cost, weight, availability, etc., the choice is made to construct the rod from aluminum (σ all 100 Ma). What is an appropriate choice for the rod diameter? σ d π 4 d all 4 π σ 6 ( 10 m ).5 10 m 5.mm all π N a n aluminum rod 6 mm or more in diameter is adequate 6 m 1-9

10 ial Loading: Normal Stress The resultant of the internal forces for an aially loaded member is normal to a section cut perpendicular to the member ais. The force intensity on that section is defined as the normal stress. σ lim 0 F σ ave The normal stress at a particular point may not be equal to the average stress but the resultant of the stress distribution must satisfy σ ave df The detailed distribution of stress is statically indeterminate, i.e., can not be found from statics alone. σ d 1-10

11 Centric & Eccentric Loading uniform distribution of stress in a section infers that the line of action for the resultant of the internal forces passes through the centroid of the section. uniform distribution of stress is only possible if the concentrated loads on the end sections of two-force members are applied at the section centroids. This is referred to as centric loading. If a two-force member is eccentrically loaded, then the resultant of the stress distribution in a section must yield an aial force and a moment. The stress distributions in eccentrically loaded members cannot be uniform or symmetric. 1-11

12 Shearing Stress Forces and are applied transversely to the member B. Corresponding internal forces act in the plane of section C and are called shearing forces. The resultant of the internal shear force distribution is defined as the shear of the section and is equal to the load. The corresponding average shear stress is, τ ave Shear stress distribution varies from zero at the member surfaces to maimum values that may be much larger than the average value. The shear stress distribution cannot be assumed to be uniform. 1-1

13 Shearing Stress Eamples Single Shear Double Shear τ ave F τ ave F 1-13

14 Bearing Stress in Connections Bolts, rivets, and pins create stresses on the points of contact or bearing surfaces of the members they connect. The resultant of the force distribution on the surface is equal and opposite to the force eerted on the pin. Corresponding average force intensity is called the bearing stress, σ b t d 1-14

15 Stress nalysis & Design Eample Would like to determine the stresses in the members and connections of the structure shown. From a statics analysis: F B 40 kn (compression) F BC 50 kn (tension) Must consider maimum normal stresses in B and BC, and the shearing stress and bearing stress at each pinned connection 1-15

16 Rod & Boom Normal Stresses The rod is in tension with an aial force of 50 kn. t the rod center, the average normal stress in the circular cross-section ( m ) is σ BC +159 Ma. t the flattened rod ends, the smallest cross-sectional area occurs at the pin centerline, 6 ( 0mm)( 40mm 5mm) m σ BC, end N m 167 Ma The boom is in compression with an aial force of 40 kn and average normal stress of 6.7 Ma. The minimum area sections at the boom ends are unstressed since the boom is in compression

17 in Shearing Stresses The cross-sectional area for pins at, B, and C, 5mm π r π m The force on the pin at C is equal to the force eerted by the rod BC, N τ C, ave m 10Ma The pin at is in double shear with a total force equal to the force eerted by the boom B, 0kN m τ, ave 40.7 Ma 1-17

18 in Shearing Stresses Divide the pin at B into sections to determine the section with the largest shear force, E G 15kN 5kN (largest) Evaluate the corresponding average shearing stress, 5kN τ, G B ave m 50.9Ma 1-18

19 in Bearing Stresses To determine the bearing stress at in the boom B, we have t 30 mm and d 5 mm, σ b td 40kN ( 30mm)( 5mm) 53.3Ma To determine the bearing stress at in the bracket, we have t (5 mm) 50 mm and d 5 mm, σ b td 40kN ( 50mm)( 5mm) 3.0Ma 1-19

20 Stress in Two Force Members ial forces on a two force member result in only normal stresses on a plane cut perpendicular to the member ais. Transverse forces on bolts and pins result in only shear stresses on the plane perpendicular to bolt or pin ais. Will show that either aial or transverse forces may produce both normal and shear stresses with respect to a plane other than one cut perpendicular to the member ais. 1-0

21 Stress on an Oblique lane ass a section through the member forming an angle θ with the normal plane. From equilibrium conditions, the distributed forces (stresses) on the plane must be equivalent to the force. Resolve into components normal and tangential to the oblique section, F cosθ V sinθ The average normal and shear stresses on the oblique plane are σ τ F V θ θ cosθ 0 cosθ sinθ 0 cosθ 0 0 cos θ sinθ cosθ 1-1

22 Maimum Stresses Normal and shearing stresses on an oblique plane σ The maimum normal stress occurs when the reference plane is perpendicular to the member ais, σ cos θ τ 0 0 τ m 0 0 The maimum shear stress occurs for a plane at + 45 o with respect to the ais, τ m sin 45 cos 45 σ 0 sinθ cosθ 0 1-

23 Stress Under General Loadings member subjected to a general combination of loads is cut into two segments by a plane passing through Q The distribution of internal stress components may be defined as, σ τ y lim 0 lim 0 F V y τ z lim 0 Vz For equilibrium, an equal and opposite internal force and stress distribution must be eerted on the other segment of the member. 1-3

24 State of Stress Stress components are defined for the planes cut parallel to the, y and z aes. For equilibrium, equal and opposite stresses are eerted on the hidden planes. The combination of forces generated by the stresses must satisfy the conditions for equilibrium: F F F 0 y M z y M 0 τ τ y M y z M 0 Consider the moments about the z ais: similarly, ( τ ) a ( τ ) yz y zy It follows that only 6 components of stress are required to define the complete state of stress z y τ τ and τ τ a yz zy 1-4

25 Factor of Safety Structural members or machines must be designed such that the working stresses are less than the ultimate strength of the material. FS Factor of safety FS σ σ u all ultimate stress allowable stress Factor of safety considerations: uncertainty in material properties uncertainty of loadings uncertainty of analyses number of loading cycles types of failure maintenance requirements and deterioration effects importance of member to integrity of whole structure risk to life and property influence on machine function 1-5

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Third E CHAPTER 1 Introduction MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University Concept of Stress Contents Concept of Stress

More information

材料力學 Mechanics of Materials

材料力學 Mechanics of Materials 材料力學 Mechanics of Materials 林峻立博士 國立陽明大學生物醫學工程系教授 Chun-Li Lin, PhD., Professor, Department of Biomedical Engineering National Yang-Ming University 1-1 Cortical bone: 10-20GPa Load Cross section b Moment

More information

ARC 341 Structural Analysis II. Lecture 10: MM1.3 MM1.13

ARC 341 Structural Analysis II. Lecture 10: MM1.3 MM1.13 ARC241 Structural Analysis I Lecture 10: MM1.3 MM1.13 MM1.4) Analysis and Design MM1.5) Axial Loading; Normal Stress MM1.6) Shearing Stress MM1.7) Bearing Stress in Connections MM1.9) Method of Problem

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHAPTER MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Teas Tech Universit Transformations of Stress and Strain 006 The McGraw-Hill Companies,

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 2009 The McGraw-Hill Companies, Inc. All rights reserved. Fifth SI Edition CHAPTER 3 MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Torsion Lecture Notes:

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS GE SI CHAPTER 3 MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Torsion Lecture Notes: J. Walt Oler Texas Tech University Torsional Loads on Circular Shafts

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 00 The McGraw-Hill Companies, Inc. All rights reserved. T Edition CHAPTER MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Teas Tech Universit

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHTER MECHNICS OF MTERILS 10 Ferdinand. Beer E. Russell Johnston, Jr. Columns John T. DeWolf cture Notes: J. Walt Oler Texas Tech University 006 The McGraw-Hill Companies, Inc. ll rights reserved. Columns

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 009 The McGraw-Hill Companies, Inc. All rights reserved. Fifth SI Edition CHAPTER 7 MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Transformations of

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS STATICS AND MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr, John T. DeWolf David E Mazurek \Cawect Mc / iur/» Craw SugomcT Hilt Introduction 1 1.1 What is Mechanics? 2 1.2 Fundamental

More information

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola MECHANICS OF MATERIALS Prepared by Engr. John Paul Timola Mechanics of materials branch of mechanics that studies the internal effects of stress and strain in a solid body. stress is associated with the

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Third E CHAPTER 2 Stress MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University and Strain Axial Loading Contents Stress & Strain:

More information

Module 5: Theories of Failure

Module 5: Theories of Failure Module 5: Theories of Failure Objectives: The objectives/outcomes of this lecture on Theories of Failure is to enable students for 1. Recognize loading on Structural Members/Machine elements and allowable

More information

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

STATICS. Bodies VECTOR MECHANICS FOR ENGINEERS: Ninth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. N E 4 Equilibrium CHAPTER VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. Lecture Notes: J. Walt Oler Texas Tech University of Rigid Bodies 2010 The McGraw-Hill Companies,

More information

STRESS. Bar. ! Stress. ! Average Normal Stress in an Axially Loaded. ! Average Shear Stress. ! Allowable Stress. ! Design of Simple Connections

STRESS. Bar. ! Stress. ! Average Normal Stress in an Axially Loaded. ! Average Shear Stress. ! Allowable Stress. ! Design of Simple Connections STRESS! Stress Evisdom! verage Normal Stress in an xially Loaded ar! verage Shear Stress! llowable Stress! Design of Simple onnections 1 Equilibrium of a Deformable ody ody Force w F R x w(s). D s y Support

More information

STATICS. Statics of Particles VECTOR MECHANICS FOR ENGINEERS: Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

STATICS. Statics of Particles VECTOR MECHANICS FOR ENGINEERS: Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. Eighth E CHAPTER VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. Statics of Particles Lecture Notes: J. Walt Oler Teas Tech Universit Contents Introduction Resultant

More information

STATICS. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Contents 9/3/2015

STATICS. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Contents 9/3/2015 6 Analsis CHAPTER VECTOR MECHANICS OR ENGINEERS: STATICS erdinand P. Beer E. Russell Johnston, Jr. of Structures Lecture Notes: J. Walt Oler Texas Tech Universit Contents Introduction Definition of a Truss

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

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 2009 The McGraw-Hill Companies, Inc. All rights reserved. Fifth SI Edition CHAPTER 6 MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Lecture Notes: J.

More information

Comb Resonator Design (2)

Comb Resonator Design (2) Lecture 6: Comb Resonator Design () -Intro. to Mechanics of Materials Sh School of felectrical ti lengineering i and dcomputer Science, Si Seoul National University Nano/Micro Systems & Controls Laboratory

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Third CHTR Stress MCHNICS OF MTRIS Ferdinand. Beer. Russell Johnston, Jr. John T. DeWolf ecture Notes: J. Walt Oler Texas Tech University and Strain xial oading Contents Stress & Strain: xial oading Normal

More information

STATICS. Equivalent Systems of Forces. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Contents & Objectives.

STATICS. Equivalent Systems of Forces. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Contents & Objectives. 3 Rigid CHATER VECTOR ECHANICS FOR ENGINEERS: STATICS Ferdinand. Beer E. Russell Johnston, Jr. Lecture Notes: J. Walt Oler Teas Tech Universit Bodies: Equivalent Sstems of Forces Contents & Objectives

More information

BTECH MECHANICAL PRINCIPLES AND APPLICATIONS. Level 3 Unit 5

BTECH MECHANICAL PRINCIPLES AND APPLICATIONS. Level 3 Unit 5 BTECH MECHANICAL PRINCIPLES AND APPLICATIONS Level 3 Unit 5 FORCES AS VECTORS Vectors have a magnitude (amount) and a direction. Forces are vectors FORCES AS VECTORS (2 FORCES) Forces F1 and F2 are in

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Third E CHAPTER 6 Shearing MECHANCS OF MATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University Stresses in Beams and Thin- Walled Members Shearing

More information

Problem d d d B C E D. 0.8d. Additional lecturebook examples 29 ME 323

Problem d d d B C E D. 0.8d. Additional lecturebook examples 29 ME 323 Problem 9.1 Two beam segments, AC and CD, are connected together at C by a frictionless pin. Segment CD is cantilevered from a rigid support at D, and segment AC has a roller support at A. a) Determine

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 009 The McGraw-Hill Companies, nc. All rights reserved. Fifth S E CHAPTER 6 MECHANCS OF MATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Lecture Notes: J. Walt Oler Texas

More information

STATICS VECTOR MECHANICS FOR ENGINEERS: Distributed Forces: Centroids and Centers of Gravity. Tenth Edition CHAPTER

STATICS VECTOR MECHANICS FOR ENGINEERS: Distributed Forces: Centroids and Centers of Gravity. Tenth Edition CHAPTER Tenth E CHAPTER 5 VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Lecture Notes: John Chen California Polytechnic State University Distributed Forces:

More information

Stress and Strain ( , 3.14) MAE 316 Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering

Stress and Strain ( , 3.14) MAE 316 Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering (3.8-3.1, 3.14) MAE 316 Strength of Mechanical Components NC State Universit Department of Mechanical & Aerospace Engineering 1 Introduction MAE 316 is a continuation of MAE 314 (solid mechanics) Review

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHAPTER 6 MECHANCS OF MATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Lecture Notes: J. Walt Oler Texas Tech University Shearing Stresses in Beams and Thin- Walled Members

More information

MECE 3321 MECHANICS OF SOLIDS CHAPTER 1

MECE 3321 MECHANICS OF SOLIDS CHAPTER 1 MECE 3321 MECHANICS O SOLIDS CHAPTER 1 Samantha Ramirez, MSE WHAT IS MECHANICS O MATERIALS? Rigid Bodies Statics Dynamics Mechanics Deformable Bodies Solids/Mech. Of Materials luids 1 WHAT IS MECHANICS

More information

CHAPTER 5 ANALYSIS OF STRUCTURES. Expected Outcome:

CHAPTER 5 ANALYSIS OF STRUCTURES. Expected Outcome: CHAPTER ANALYSIS O STRUCTURES Expected Outcome: Able to analyze the equilibrium of structures made of several connected parts, using the concept of the equilibrium of a particle or of a rigid body, in

More information

[5] Stress and Strain

[5] Stress and Strain [5] Stress and Strain Page 1 of 34 [5] Stress and Strain [5.1] Internal Stress of Solids [5.2] Design of Simple Connections (will not be covered in class) [5.3] Deformation and Strain [5.4] Hooke s Law

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 00 The McGraw-Hill Copanies, Inc. All rights reserved. T Edition CHAPTER MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University

More information

two structural analysis (statics & mechanics) Structural Requirements Structure Requirements Structure Requirements serviceability efficiency

two structural analysis (statics & mechanics) Structural Requirements Structure Requirements Structure Requirements serviceability efficiency LIED RCHITECTURL STRUCTURES: STRUCTURL NLYSIS ND SYSTEMS DR. NNE NICHOLS SRING 018 lecture two structural analysis (statics & mechanics) nalysis 1 pplied rchitectural Structures 009abn Structural Requirements

More information

COLUMNS: BUCKLING (DIFFERENT ENDS)

COLUMNS: BUCKLING (DIFFERENT ENDS) COLUMNS: BUCKLING (DIFFERENT ENDS) Buckling of Long Straight Columns Example 4 Slide No. 1 A simple pin-connected truss is loaded and supported as shown in Fig. 1. All members of the truss are WT10 43

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Third CHTR Stress MCHNICS OF MTRIS Ferdinand. Beer. Russell Johnston, Jr. John T. DeWolf ecture Notes: J. Walt Oler Texas Tech University and Strain xial oading Contents Stress & Strain: xial oading Normal

More information

STATICS. Bodies. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Design of a support

STATICS. Bodies. Vector Mechanics for Engineers: Statics VECTOR MECHANICS FOR ENGINEERS: Design of a support 4 Equilibrium CHAPTER VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. Lecture Notes: J. Walt Oler Texas Tech University of Rigid Bodies 2010 The McGraw-Hill Companies,

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

Module 11 Design of Joints for Special Loading. Version 2 ME, IIT Kharagpur

Module 11 Design of Joints for Special Loading. Version 2 ME, IIT Kharagpur Module 11 Design of Joints for Special Loading Version ME, IIT Kharagpur Lesson Design of Eccentrically Loaded Welded Joints Version ME, IIT Kharagpur Instructional Objectives: At the end of this lesson,

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

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2 Samantha Ramirez, MSE Stress The intensity of the internal force acting on a specific plane (area) passing through a point. Δ ΔA Δ z Δ 1 2 ΔA Δ x Δ y ΔA is an infinitesimal size area with a uniform force

More information

4. SHAFTS. A shaft is an element used to transmit power and torque, and it can support

4. SHAFTS. A shaft is an element used to transmit power and torque, and it can support 4. SHAFTS A shaft is an element used to transmit power and torque, and it can support reverse bending (fatigue). Most shafts have circular cross sections, either solid or tubular. The difference between

More information

STATICS VECTOR MECHANICS FOR ENGINEERS: Eleventh Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek

STATICS VECTOR MECHANICS FOR ENGINEERS: Eleventh Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Eleventh E 6 Analysis CHAPTER VECTOR MECHANICS OR ENGINEERS: STATICS erdinand P. Beer E. Russell Johnston, Jr. David. Mazurek of Structures Contents Application Introduction Definition of a Truss Simple

More information

Tenth Edition STATICS 1 Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Lecture Notes: John Chen California Polytechnic State University

Tenth Edition STATICS 1 Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Lecture Notes: John Chen California Polytechnic State University T E CHAPTER 1 VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. David F. Mazurek Lecture Notes: Introduction John Chen California Polytechnic State University! Contents

More information

Chapter 1 Introduction- Concept of Stress

Chapter 1 Introduction- Concept of Stress hapter 1 Introduction- oncept of Stress INTRODUTION Review of Statics xial Stress earing Stress Torsional Stress 14 6 ending Stress W W L Introduction 1-1 Shear Stress W W Stress and Strain L y y τ xy

More information

Aluminum shell. Brass core. 40 in

Aluminum shell. Brass core. 40 in PROBLEM #1 (22 points) A solid brass core is connected to a hollow rod made of aluminum. Both are attached at each end to a rigid plate as shown in Fig. 1. The moduli of aluminum and brass are EA=11,000

More information

LECTURE 4 Stresses in Elastic Solid. 1 Concept of Stress

LECTURE 4 Stresses in Elastic Solid. 1 Concept of Stress V. DEMENKO MECHANICS OF MATERIALS 2015 1 LECTURE 4 Stresses in Elastic Solid 1 Concept of Stress In order to characterize the law of internal forces distribution over the section a measure of their intensity

More information

Principal Stresses, Yielding Criteria, wall structures

Principal Stresses, Yielding Criteria, wall structures Principal Stresses, Yielding Criteria, St i thi Stresses in thin wall structures Introduction The most general state of stress at a point may be represented by 6 components, x, y, z τ xy, τ yz, τ zx normal

More information

MECHANICS OF MATERIALS REVIEW

MECHANICS OF MATERIALS REVIEW MCHANICS OF MATRIALS RVIW Notation: - normal stress (psi or Pa) - shear stress (psi or Pa) - normal strain (in/in or m/m) - shearing strain (in/in or m/m) I - area moment of inertia (in 4 or m 4 ) J -

More information

Mechanics of Materials

Mechanics of Materials Mechanics of Materials 2. Introduction Dr. Rami Zakaria References: 1. Engineering Mechanics: Statics, R.C. Hibbeler, 12 th ed, Pearson 2. Mechanics of Materials: R.C. Hibbeler, 9 th ed, Pearson 3. Mechanics

More information

Determine the resultant internal loadings acting on the cross section at C of the beam shown in Fig. 1 4a.

Determine the resultant internal loadings acting on the cross section at C of the beam shown in Fig. 1 4a. E X M P L E 1.1 Determine the resultant internal loadings acting on the cross section at of the beam shown in Fig. 1 a. 70 N/m m 6 m Fig. 1 Support Reactions. This problem can be solved in the most direct

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS For updated version, please click on http://ocw.ump.edu.my MECHANICS OF MATERIALS COURSE INFORMATION by Nur Farhayu Binti Ariffin Faculty of Civil Engineering and Earth Resources farhayu@ump.edu.my MECHANICS

More information

two structural analysis (statics & mechanics) APPLIED ACHITECTURAL STRUCTURES: DR. ANNE NICHOLS SPRING 2017 lecture STRUCTURAL ANALYSIS AND SYSTEMS

two structural analysis (statics & mechanics) APPLIED ACHITECTURAL STRUCTURES: DR. ANNE NICHOLS SPRING 2017 lecture STRUCTURAL ANALYSIS AND SYSTEMS APPLIED ACHITECTURAL STRUCTURES: STRUCTURAL ANALYSIS AND SYSTEMS DR. ANNE NICHOLS SPRING 2017 lecture two structural analysis (statics & mechanics) Analysis 1 Structural Requirements strength serviceability

More information

five Mechanics of Materials 1 ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2017 lecture

five Mechanics of Materials 1 ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2017 lecture ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2017 lecture five mechanics www.carttalk.com of materials Mechanics of Materials 1 Mechanics of Materials MECHANICS MATERIALS

More information

MECHANICS OF MATERIALS. Analysis of Beams for Bending

MECHANICS OF MATERIALS. Analysis of Beams for Bending MECHANICS OF MATERIALS Analysis of Beams for Bending By NUR FARHAYU ARIFFIN Faculty of Civil Engineering & Earth Resources Chapter Description Expected Outcomes Define the elastic deformation of an axially

More information

CHAPTER 4: BENDING OF BEAMS

CHAPTER 4: BENDING OF BEAMS (74) CHAPTER 4: BENDING OF BEAMS This chapter will be devoted to the analysis of prismatic members subjected to equal and opposite couples M and M' acting in the same longitudinal plane. Such members are

More information

Chapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING )

Chapter 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 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

MECHANICS OF MATERIALS Design of a Transmission Shaft

MECHANICS OF MATERIALS Design of a Transmission Shaft Design of a Transmission Shaft If power is transferred to and from the shaft by gears or sprocket wheels, the shaft is subjected to transverse loading as well as shear loading. Normal stresses due to transverse

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS 00 The cgraw-hill Copanies, Inc. All rights reserved. Third E CHAPTER 8 Principle ECHANICS OF ATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University

More information

Equilibrium. Rigid Bodies VECTOR MECHANICS FOR ENGINEERS: STATICS. Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

Equilibrium. Rigid Bodies VECTOR MECHANICS FOR ENGINEERS: STATICS. Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr. Eighth E 4 Equilibrium CHAPTER VECTOR MECHANICS FOR ENGINEERS: STATICS Ferdinand P. Beer E. Russell Johnston, Jr. Lecture Notes: J. Walt Oler Texas Tech University of Rigid Bodies Contents Introduction

More information

7.4 The Elementary Beam Theory

7.4 The Elementary Beam Theory 7.4 The Elementary Beam Theory In this section, problems involving long and slender beams are addressed. s with pressure vessels, the geometry of the beam, and the specific type of loading which will be

More information

(48) CHAPTER 3: TORSION

(48) CHAPTER 3: TORSION (48) CHAPTER 3: TORSION Introduction: In this chapter structural members and machine parts that are in torsion will be considered. More specifically, you will analyze the stresses and strains in members

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHAPTER 2 MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf David F. Mazurek Lecture Notes: J. Walt Oler Texas Tech University Stress and Strain Axial Loading 2.1 An Introduction

More information

D e s i g n o f R i v e t e d J o i n t s, C o t t e r & K n u c k l e J o i n t s

D e s i g n o f R i v e t e d J o i n t s, C o t t e r & K n u c k l e J o i n t s D e s i g n o f R i v e t e d J o i n t s, C o t t e r & K n u c k l e J o i n t s 1. Design of various types of riveted joints under different static loading conditions, eccentrically loaded riveted joints.

More information

- Beams are structural member supporting lateral loadings, i.e., these applied perpendicular to the axes.

- Beams are structural member supporting lateral loadings, i.e., these applied perpendicular to the axes. 4. Shear and Moment functions - Beams are structural member supporting lateral loadings, i.e., these applied perpendicular to the aes. - The design of such members requires a detailed knowledge of the

More information

Module 2 Stresses in machine elements

Module 2 Stresses in machine elements Module 2 Stresses in machine elements Lesson 3 Strain analysis Instructional Objectives At the end of this lesson, the student should learn Normal and shear strains. 3-D strain matri. Constitutive equation;

More information

University of Pretoria Department of Mechanical & Aeronautical Engineering MOW 227, 2 nd Semester 2014

University of Pretoria Department of Mechanical & Aeronautical Engineering MOW 227, 2 nd Semester 2014 Universit of Pretoria Department of Mechanical & Aeronautical Engineering MOW 7, nd Semester 04 Semester Test Date: August, 04 Total: 00 Internal eaminer: Duration: hours Mr. Riaan Meeser Instructions:

More information

Lecture Triaxial Stress and Yield Criteria. When does yielding occurs in multi-axial stress states?

Lecture Triaxial Stress and Yield Criteria. When does yielding occurs in multi-axial stress states? Lecture 5.11 Triaial Stress and Yield Criteria When does ielding occurs in multi-aial stress states? Representing stress as a tensor operational stress sstem Compressive stress sstems Triaial stresses:

More information

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)?

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)? IDE 110 S08 Test 1 Name: 1. Determine the internal axial forces in segments (1), (2) and (3). (a) N 1 = kn (b) N 2 = kn (c) N 3 = kn 2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at

More information

ENGINEERING MECHANICS STATIC

ENGINEERING MECHANICS STATIC Trusses Simple trusses The basic element of a truss is the triangle, three bars joined by pins at their ends, fig. a below, constitutes a rigid frame. The term rigid is used to mean noncollapsible and

More information

Outline. Organization. Stresses in Beams

Outline. Organization. Stresses in Beams Stresses in Beams B the end of this lesson, ou should be able to: Calculate the maimum stress in a beam undergoing a bending moment 1 Outline Curvature Normal Strain Normal Stress Neutral is Moment of

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHATER MECHANICS OF MATERIAS Ferdinand. Beer E. Russell Johnston, Jr. John T. DeWolf Energy Methods ecture Notes: J. Walt Oler Teas Tech niversity 6 The McGraw-Hill Copanies, Inc. All rights reserved.

More information

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /15 PAPER A

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /15 PAPER A SSOCITE DEGREE IN ENGINEERING EXMINTIONS SEMESTER 2 2014/15 PPER COURSE NME: ENGINEERING MECHNICS - STTICS CODE: ENG 2008 GROUP: D ENG II DTE: May 2015 TIME: DURTION: 2 HOURS INSTRUCTIONS: 1. This paper

More information

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy Stress Analysis Lecture 3 ME 276 Spring 2017-2018 Dr./ Ahmed Mohamed Nagib Elmekawy Axial Stress 2 Beam under the action of two tensile forces 3 Beam under the action of two tensile forces 4 Shear Stress

More information

Truss Analysis Method of Joints. Steven Vukazich San Jose State University

Truss Analysis Method of Joints. Steven Vukazich San Jose State University Truss nalysis Method of Joints Steven Vukazich San Jose State University General Procedure for the nalysis of Simple Trusses using the Method of Joints 1. raw a Free Body iagram (FB) of the entire truss

More information

CHAPTER 6: Shearing Stresses in Beams

CHAPTER 6: Shearing Stresses in Beams (130) CHAPTER 6: Shearing Stresses in Beams When a beam is in pure bending, the only stress resultants are the bending moments and the only stresses are the normal stresses acting on the cross sections.

More information

Bone Tissue Mechanics

Bone Tissue Mechanics Bone Tissue Mechanics João Folgado Paulo R. Fernandes Instituto Superior Técnico, 2016 PART 1 and 2 Introduction The objective of this course is to study basic concepts on hard tissue mechanics. Hard tissue

More information

2. Analyzing stress: Defini n ti t ons n a nd n C onc n e c pt p s

2. Analyzing stress: Defini n ti t ons n a nd n C onc n e c pt p s 2. Analyzing tre: Definition and Concept 2.1 Introduction Stre and train - The fundamental and paramount ubject in mechanic of material - Chapter 2: Stre - Chapter 3: Strain 2.2 Normal tre under aial loading

More information

Physical Science and Engineering. Course Information. Course Number: ME 100

Physical Science and Engineering. Course Information. Course Number: ME 100 Physical Science and Engineering Course Number: ME 100 Course Title: Course Information Basic Principles of Mechanics Academic Semester: Fall Academic Year: 2016-2017 Semester Start Date: 8/21/2016 Semester

More information

Engineering Mechanics Department of Mechanical Engineering Dr. G. Saravana Kumar Indian Institute of Technology, Guwahati

Engineering Mechanics Department of Mechanical Engineering Dr. G. Saravana Kumar Indian Institute of Technology, Guwahati Engineering Mechanics Department of Mechanical Engineering Dr. G. Saravana Kumar Indian Institute of Technology, Guwahati Module 3 Lecture 6 Internal Forces Today, we will see analysis of structures part

More information

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMEBERS

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMEBERS EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMEBERS Today s Objectives: Students will be able to: a) Apply equations of equilibrium to solve for unknowns, and, b) Recognize two-force members. In-Class

More information

ME 025 Mechanics of Materials

ME 025 Mechanics of Materials ME 025 Mechanics of Materials General Information: Term: 2019 Summer Session Instructor: Staff Language of Instruction: English Classroom: TBA Office Hours: TBA Class Sessions Per Week: 5 Total Weeks:

More information

NORMAL STRESS. The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts.

NORMAL STRESS. The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts. NORMAL STRESS The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts. σ = force/area = P/A where σ = the normal stress P = the centric

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

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics Page1 PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [2910601] Introduction, Fundamentals of Statics 1. Differentiate between Scalar and Vector quantity. Write S.I.

More information

MECE 3321: Mechanics of Solids Chapter 6

MECE 3321: Mechanics of Solids Chapter 6 MECE 3321: Mechanics of Solids Chapter 6 Samantha Ramirez Beams Beams are long straight members that carry loads perpendicular to their longitudinal axis Beams are classified by the way they are supported

More information

Example 4: Design of a Rigid Column Bracket (Bolted)

Example 4: Design of a Rigid Column Bracket (Bolted) Worked Example 4: Design of a Rigid Column Bracket (Bolted) Example 4: Design of a Rigid Column Bracket (Bolted) Page : 1 Example 4: Design of a Rigid Column Bracket (Bolted) Determine the size of the

More information

and F NAME: ME rd Sample Final Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points)

and F NAME: ME rd Sample Final Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points) ME 270 3 rd Sample inal Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points) IND: In your own words, please state Newton s Laws: 1 st Law = 2 nd Law = 3 rd Law = PROBLEM

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS CHAPTER MECHANCS OF MATERALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University Shearing Stresses in Beams and Thin- Walled Members 006 The McGraw-Hill

More information

ENGR-1100 Introduction to Engineering Analysis. Lecture 19

ENGR-1100 Introduction to Engineering Analysis. Lecture 19 ENGR-1100 Introduction to Engineering Analysis Lecture 19 SIMPLE TRUSSES, THE METHOD OF JOINTS, & ZERO-FORCE MEMBERS Today s Objectives: Students will be able to: In-Class Activities: a) Define a simple

More information

Solution: T, A1, A2, A3, L1, L2, L3, E1, E2, E3, P are known Five equations in five unknowns, F1, F2, F3, ua and va

Solution: T, A1, A2, A3, L1, L2, L3, E1, E2, E3, P are known Five equations in five unknowns, F1, F2, F3, ua and va ME 323 Examination # 1 February 18, 2016 Name (Print) (Last) (First) Instructor PROBLEM #1 (20 points) A structure is constructed from members 1, 2 and 3, with these members made up of the same material

More information

0.3 m. 0.4 m. 0.3 m. A 2 kn. 0.4 m. tan γ = 7. (BC = kn) γ = Fx = BC cos θ + AC cos γ =0

0.3 m. 0.4 m. 0.3 m. A 2 kn. 0.4 m. tan γ = 7. (BC = kn) γ = Fx = BC cos θ + AC cos γ =0 Problem 6.4 etermine the aial forces in the members of the truss. kn 0.3 m 0.4 m 0.6 m 1. m Solution: irst, solve for the support reactions at and, and then use the method of joints to solve for the forces

More information

Comb resonator design (2)

Comb resonator design (2) Lecture 6: Comb resonator design () -Intro Intro. to Mechanics of Materials School of Electrical l Engineering i and Computer Science, Seoul National University Nano/Micro Systems & Controls Laboratory

More information

The University of Melbourne Engineering Mechanics

The University of Melbourne Engineering Mechanics The University of Melbourne 436-291 Engineering Mechanics Tutorial Four Poisson s Ratio and Axial Loading Part A (Introductory) 1. (Problem 9-22 from Hibbeler - Statics and Mechanics of Materials) A short

More information

5.3 Rigid Bodies in Three-Dimensional Force Systems

5.3 Rigid Bodies in Three-Dimensional Force Systems 5.3 Rigid odies in Three-imensional Force Sstems 5.3 Rigid odies in Three-imensional Force Sstems Eample 1, page 1 of 5 1. For the rigid frame shown, determine the reactions at the knife-edge supports,,.

More information

CE 221: MECHANICS OF SOLIDS I CHAPTER 1: STRESS. Dr. Krisada Chaiyasarn Department of Civil Engineering, Faculty of Engineering Thammasat university

CE 221: MECHANICS OF SOLIDS I CHAPTER 1: STRESS. Dr. Krisada Chaiyasarn Department of Civil Engineering, Faculty of Engineering Thammasat university CE 221: MECHANICS OF SOLIDS I CHAPTER 1: STRESS By Dr. Krisada Chaiyasarn Department of Civil Engineering, Faculty of Engineering Thammasat university Agenda Introduction to your lecturer Introduction

More information

IDE 110 Mechanics of Materials Spring 2006 Final Examination FOR GRADING ONLY

IDE 110 Mechanics of Materials Spring 2006 Final Examination FOR GRADING ONLY Spring 2006 Final Examination STUDENT S NAME (please print) STUDENT S SIGNATURE STUDENT NUMBER IDE 110 CLASS SECTION INSTRUCTOR S NAME Do not turn this page until instructed to start. Write your name on

More information

Torsion of Shafts Learning objectives

Torsion of Shafts Learning objectives Torsion of Shafts Shafts are structural members with length significantly greater than the largest cross-sectional dimension used in transmitting torque from one plane to another. Learning objectives Understand

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