Schaum's Outlines Strength of Materials

Total Page:16

File Type:pdf, Size:1020Kb

Schaum's Outlines Strength of Materials Strength Of Materials This page intentionally left blank Strength Of Materials Fifth Edition William A. Nash, Ph.D. Former Professor of Civil Engineering University of Massachusetts Merle C. Potter, Ph.D. Professor Emeritus of Mechanical Engineering Michigan State University Schaum’s Outline Series New York Chicago San Francisco Lisbon London Madrid Mexico City Milan New Delhi San Juan Seoul Singapore Sydney Toronto Copyright © 2011, 1998, 1994, 1972 by The McGraw-Hill Companies, Inc. All rights reserved. Except as permitted under the United States Copyright Act of 1976, no part of this publication may be reproduced or distributed in any form or by any means, or stored in a database or retrieval system, without the prior written permission of the publisher. ISBN: 978-0-07-163507-3 MHID: 0-07-163507-6 The material in this eBook also appears in the print version of this title: ISBN: 978-0-07-163508-0, MHID: 0-07-163508-4. All trademarks are trademarks of their respective owners. Rather than put a trademark symbol after every occurrence of a trademarked name, we use names in an editorial fashion only, and to the benefi t of the trademark owner, with no intention of infringement of the trademark. Where such designations appear in this book, they have been printed with initial caps. McGraw-Hill eBooks are available at special quantity discounts to use as premiums and sales promotions, or for use in corporate training programs. To contact a representative please e-mail us at [email protected]. This publication is designed to provide accurate and authoritative information in regard to the subject matter covered. It is sold with the understanding that neither the author nor the publisher is engaged in rendering legal, accounting, securities trading, or other professional services. If legal advice or other expert assistance is required, the services of a competent professional person should be sought. —From a Declaration of Principles Jointly Adopted by a Committee of the American Bar Association and a Committee of Publishers and Associations Trademarks: McGraw-Hill, the McGraw-Hill Publishing logo, Schaum’s and related trade dress are trademarks or registered trademarks of The McGraw-Hill Companies and/or its affi liates in the United States and other countries and may not be used without written permission. All other trademarks are the property of their respective owners. The McGraw-Hill Companies is not associated with any product or vendor mentioned in this book. TERMS OF USE This is a copyrighted work and The McGraw-Hill Companies, Inc. (“McGrawHill”) and its licensors reserve all rights in and to the work. Use of this work is subject to these terms. Except as permitted under the Copyright Act of 1976 and the right to store and retrieve one copy of the work, you may not decompile, disassemble, reverse engineer, reproduce, modify, create derivative works based upon, transmit, distribute, disseminate, sell, publish or sublicense the work or any part of it without McGraw-Hill’s prior consent. You may use the work for your own noncommercial and personal use; any other use of the work is strictly prohibited. Your right to use the work may be terminated if you fail to comply with these terms. THE WORK IS PROVIDED “AS IS.” McGRAW-HILL AND ITS LICENSORS MAKE NO GUARANTEES OR WARRANTIES AS TO THE ACCURACY, ADEQUACY OR COMPLETENESS OF OR RESULTS TO BE OBTAINED FROM USING THE WORK, INCLUDING ANY INFORMATION THAT CAN BE ACCESSED THROUGH THE WORK VIA HYPERLINK OR OTHERWISE, AND EXPRESSLY DISCLAIM ANY WARRANTY, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. McGraw-Hill and its licensors do not warrant or guarantee that the functions contained in the work will meet your requirements or that its operation will be uninterrupted or error free. Neither McGraw-Hill nor its licensors shall be liable to you or anyone else for any inaccuracy, error or omission, regardless of cause, in the work or for any damages resulting therefrom. McGraw-Hill has no responsibility for the content of any information accessed through the work. Under no circumstances shall McGraw-Hill and/or its licensors be liable for any indirect, incidental, special, punitive, consequential or similar damages that result from the use of or inability to use the work, even if any of them has been advised of the possibility of such damages. This limitation of liability shall apply to any claim or cause whatsoever whether such claim or cause arises in contract, tort or otherwise. Preface This fifth edition of Schaum’s Strength of Materials book has been substantially modified by the second author to better fit the outline of the introductory Strength of Materials (Solid Mechanics) course, and to better fit the presentation of material in most introductory textbooks on the subject. In addition, the fol- lowing changes have been made: 1. Problem solutions and Supplementary Problems are presented using the metric SI units only. 2. The computer programs have been omitted. The use of MATLAB or other programs are available to students if more complicated problems are of interest. 3. The more advanced materials and problems that are not found in an introductory course have been omitted for simplicity of presentation. This book is intended to be used in an introductory course only. 4. A short chapter on Fatigue, a subject included on the Fundamentals of Engineering Examination, has been added. It is a modified chapter, based on a section on Fatigue written by my friend and previous colleague, Charlie Muvdi, from “Engineering Mechanics of Materials,” by B. B. Muvdi and J. W. McNabb. 5. A section on Combined Loading has been added. 6. The chapter on Centroids and Moments of Inertia has been omitted; it is assumed to have been part of a Statics course that precedes Solid Mechanics. Strength of Materials, also called The Mechanics of Materials or Solid Mechanics, provides the basis for the design of the components that make up machines and load-bearing structures. In Statics, the forces and moments acting at various points in a structural component or at points of contact with other structures were determined. The forces, stresses, and strains existing within a component were not of interest. In Solid Mechanics, we will consider questions like, “What load will cause this structure to fail?”, “What maximum torque can this shaft transmit?”, “What material should be selected for this component?”, “At what load will this column buckle?” Such questions were not of interest in a Statics course. But, before any of these questions can be answered, we must calculate the forces and moments acting on the components that make up a structure or machine. So, Statics always precedes the study of Strength of Materials. Sometimes Statics is combined with Strength of Materials in one course since they are so closely related. I would like to thank the estate of the late William Nash for allowing me to create this fifth edition of a book that obviously required much diligent work by Professor Nash. Many thanks are also given to Dr. Charlie Muvdi who provided good advice on the content of this revision. It was a pleasure working with Kimberly Eaton of McGraw-Hill in making the many decisions required in such a venture. MERLE C. POTTER, E. LANSING, MI Michigan State University, 2010 v This page intentionally left blank Contents CHAPTER 1 Tension and Compression 1 1.1 Internal Effects of Forces 1.2 Mechanical Properties of Materials 1.3 Statically Indeterminate Force Systems 1.4 Classification of Materials 1.5 Units CHAPTER 2 Shear Stresses 27 2.1 Shear Force and Shear Stress 2.2 Deformations Due to Shear Stresses 2.3 Shear Strain CHAPTER 3 Combined Stresses 35 3.1 Introduction 3.2 General Case of Plane Stress 3.3 Principal Stresses and Maximum Shearing Stress 3.4 Mohr’s Circle CHAPTER 4 Thin-Walled Pressure Vessels 49 4.1 Introduction 4.2 Cylindrical Pressure Vessels 4.3 Spherical Pressure Vessels CHAPTER 5 Torsion 59 5.1 Introduction 5.2 Torsional Shearing Stress 5.3 Shearing Strain 5.4 Combined Torsion and Axial Loading CHAPTER 6 Shearing Force and Bending Moment 73 6.1 Basics 6.2 Internal Forces and Moments in Beams 6.3 Shear and Moment Equations with Diagrams 6.4 Singularity Functions CHAPTER 7 Stresses in Beams 97 7.1 Basics 7.2 Normal Stresses in Beams 7.3 Shearing Stresses in Beams 7.4 Combined Loading CHAPTER 8 Deflection of Beams 123 8.1 Basics 8.2 Differential Equation of the Elastic Curve 8.3 Deflection by Integration 8.4 Deflections Using Singularity Functions 8.5 Deflections Using Superposition vii viii Contents CHAPTER 9 Statically Indeterminate Elastic Beams 143 9.1 Basics CHAPTER 10 Columns 159 10.1 Basics 10.2 Critical Load of a Long Slender Column 10.3 Eccentrically Loaded Columns 10.4 Design Formulas for Columns Having Intermediate Slenderness Ratios CHAPTER 11 Fatigue 175 Index 185 CHAPTER 1 Tension and Compression 1.1 Internal Effects of Forces In this book we shall be concerned with what might be called the internal effects of forces acting on a body. The bodies themselves will no longer be considered to be perfectly rigid as was assumed in statics; instead, the calculation of the deformations of various bodies under a variety of loads will be one of our primary concerns in the study of strength of materials. Axially Loaded Bar The simplest case to consider at the start is that of an initially straight metal bar of constant cross section, loaded at its ends by a pair of oppositely directed collinear forces coinciding with the longitudinal axis of the bar and acting through the centroid of each cross section.
Recommended publications
  • Strength Versus Gravity
    3 Strength versus gravity The existence of any differences of height on the Earth’s surface is decisive evidence that the internal stress is not hydrostatic. If the Earth was liquid any elevation would spread out horizontally until it disap- peared. The only departure of the surface from a spherical form would be the ellipticity; the outer surface would become a level surface, the ocean would cover it to a uniform depth, and that would be the end of us. The fact that we are here implies that the stress departs appreciably from being hydrostatic; … H. Jeffreys, Earthquakes and Mountains (1935) 3.1 Topography and stress Sir Harold Jeffreys (1891–1989), one of the leading geophysicists of the early twentieth century, was fascinated (one might almost say obsessed) with the strength necessary to support the observed topographic relief on the Earth and Moon. Through several books and numerous papers he made quantitative estimates of the strength of the Earth’s interior and compared the results of those estimates to the strength of common rocks. Jeffreys was not the only earth scientist who grasped the fundamental importance of rock strength. Almost ifty years before Jeffreys, American geologist G. K. Gilbert (1843–1918) wrote in a similar vein: If the Earth possessed no rigidity, its materials would arrange themselves in accordance with the laws of hydrostatic equilibrium. The matter speciically heaviest would assume the lowest position, and there would be a graduation upward to the matter speciically lightest, which would constitute the entire surface. The surface would be regularly ellipsoidal, and would be completely covered by the ocean.
    [Show full text]
  • DEPARTMENT of ENGINEERING Course CE 25200 – Strength of Materials Cross-Listed Course ME 25200 – Strength of Ma
    DEPARTMENT OF ENGINEERING Course CE 25200 – Strength of Materials Cross-listed Course ME 25200 – Strength of Materials Type of Course Required for CE program Catalog Description Plane stress, plane strain, and stress-strain laws. Applications of stress and deformation analysis to members subjected to centric, torsional, flexural, and combined loading. Introduction to theories of failure, buckling, and energy methods. Credits 3 Contact Hours 3 Prerequisite Courses CE 25000 Corequisite Courses None Prerequisites by Classification of forces Topics Equilibrium of a rigid body Internal forces Centroids and moments of inertia Textbook Mechanics of Materials, William F. Riley, Leroy D. Sturges, and Dan H. Morris, John Wiley & Sons, current edition. Course Objectives To provide basic knowledge in mechanics of materials so that the students can solve real engineering problems and design engineering systems. Course Outcomes Students who successfully complete this course will have demonstrated an ability to: 1. Understand the concepts of stress and strain at a point as well as the stress-strain relationships for homogenous, isotropic materials. (e) 2. Calculate the stresses and strains in axially-loaded members, circular torsion members, and members subject to flexural loadings. (a, e) 3. Calculate the stresses and strains associated with thin-wall spherical and cylindrical pressure vessels. (a, e) Department Syllabus CE – 25200 Page | 1 4. Determine the stresses and strains in members subjected to combined loading and apply the theories of failure for static loading. (a, e) 5. Determine and illustrate principal stresses, maximum shearing stress, and the stresses acting on a structural member. (a, e) 6. Determine the deflections and rotations produced by the three fundamental types of loads: axial, torsional, and flexural.
    [Show full text]
  • Structural Mechanics and Strength of Materials
    CHAPTER 1 ENGINEERING MECHANICS I 1.1 Verification of Lame’s Theorem: If three concurrent forces are in equilibrium, Lame’s theorem states that their magnitudes are proportional to the sine of the angle between the other forces. For example, Fig. 1.1(a) shows three concurrent forces P, Q and R in equilibrium, with the included angles between Q-R, R-P and P-Q being , and respectively. Therefore, Lame’s theorem states that P/sin = Q/sin = R/sin ….………………..(1.1) Since = 360 , sin = sin ( + ), and Eq. (1.1) becomes P/sin = Q/sin = R/sin ( + ) ….………………..(1.2) R D1 D2 P L 1 2 F1 F2 W Q (a) (b) Fig. 1.1: (a) Three concurrent forces in equilibrium, (b) Lab arrangement for Exp. 1.1 In the laboratory experiment, equilibrium is achieved among the forces F1, F2 and W. Lame’s theorem F1/sin (180 2) = F2/sin (180 1) = W/sin ( 1+ 2) F1 = W sin ( 2)/sin ( 1+ 2) …………..(1.3) F2 = W sin ( 1)/sin ( 1+ 2) …………..(1.4) The angles 1 and 2 are obtained from -1 1 = tan (D1/L) …………..(1.5) -1 2 = tan (D2/L) …………..(1.6) 1.2 Verification of Deflected Shape of Flexible Cord: The equation of a flexible cord loaded uniformly over its horizontal length is given by y = w{(L/2)2 x2}/(2Q) …………..(1.7) where w = load per horizontal length, L = horizontal span of the cable between supports, y = sag at a distance x (measured from the midspan of the cable), Q = horizontal tension on the cable.
    [Show full text]
  • Strength of Materials
    P STRENGTH OF MATERIALS L S A T N R T E N D G E T S H I G O N F M & A T E E C R O I N A O L M S ©This book is protected by law under the Copyright Act of India. This book can only be used by the I student to whom the book was provided by Career Avenues GATE Coaching as a part of its GATE course. Any other use of the book such as reselling, copying, photocopying, etc is a legal offense. C S © CAREER AVENUES /SOM 1 C H STRENGTH OF MATERIALS STRENGTH OF MATERIAL 0 INTRODUCTION 6 Introduction On the basis of time of action of load On the basis of direction of load On the basis of area of acting the load 9 1 Couple L0ADS Pure Bending torsion Free Body Diagram Introduction Strength Classification of stresses Normal stresses Shear stress 22 2 Stress tensor STRESSES Effects of various loads acting on the body Introduction Classification of strain Normal strain Longitudinal and lateral strain 44 Volumetric strain 3 Shear strains STRAINS Sign conventions for shear strains Properties of materials Young‟s modulus of elasticity Modulus of rigidity Bulk modulus 55 4 Poisson‟s ratio ELASTIC State of simple shear CONSTANTS Relationships between various constants © CAREER AVENUES /SOM 2 STRENGTH OF MATERIALS Stress and strain diagram Limit of proportionality Elasticity Plasticity 73 5 Ductility, Brittleness, Malleability MECHANICAL Yield strength, ultimate strength, rapture PROPERTIES strength OF MATERIALS Work done by load Strain energy due to torsion Strain energy due to bending Resilience 81 6 Toughness STRAIN Effect of carbon percentage on properties
    [Show full text]
  • Mechanics of Materials Course Number Course Title
    COURSE OUTLINE CIV229 Mechanics of Materials Course Number Course Title 4 3/3 _______ Credits Lecture/Laboratory Hours COURSE DESCRIPTION With an introduction to engineering materials and their mechanical properties, examines strains that occur in elastic bodies subjected to direct and combined stresses, shear and bending moment diagrams, deflections of beams, and stresses due to torsion. Lab testing involves various materials such as cast iron, steel, brass, aluminum, and wood to determine their physical properties and to demonstrate various testing techniques. Fall Offering. Text (s): Statics & Strength of Materials Author: Cheng, Fa-Hwa Publisher: McGraw Hill/Glencoe 2nd Edition, 1997 ISBN#: 0-02-803067-2 Prerequisites: CIV106 with a minimum C grade Co-requisites: Course Coordinator: Jim Maccariella Latest Review: Spring 2019 I. GENERAL OBJECTIVES A. To provide the student with an understanding of the relationship between external forces applied to an engineering structure and the resulting action of the members of the structure. B. To demonstrate that mechanics of materials is the basis of engineering design but it is not itself a course in design. C. To utilize the student’s background in mathematics, physics, statics, and engineering drawing so that he may solve various mechanics of materials problems in a simple, logical manner. D. To stimulate the student’s interest to investigate the many well-written texts on this subject. Course Competencies/Goals: The student will be able to: 1. Demonstrate basic engineering materials terminology. 2. Demonstrate the relationship between external forces member reactions. 3. Analyze various types of materials problems. 4. Generate and interpret loading diagrams. 5.
    [Show full text]
  • Lithospheric Strength Profiles
    21 LITHOSPHERIC STRENGTH PROFILES To study the mechanical response of the lithosphere to various types of forces, one has to take into account its rheology, which means knowing how it flows. As a scientific discipline, rheology describes the interactions between strain, stress and time. Strain and stress depend on the thermal structure, the fluid content, the thickness of compositional layers and various boundary conditions. The amount of time during which the load is applied is an important factor. - At the time scale of seismic waves, up to hundreds of seconds, the sub-crustal mantle behaves elastically down deep within the asthenosphere. - Over a few to thousands of years (e.g. load of ice cap), the mantle flows like a viscous fluid. - On long geological times (more than 1 million years), the upper crust and the upper mantle behave also as thin elastic and plastic plates that overlie an inviscid (i.e. with no viscosity) substratum. The dimensionless Deborah number D, summarized as natural response time/experimental observation time, is a measure of the influence of time on flow properties. Elasticity, plastic yielding, and viscous creep are therefore ingredients of the mechanical behavior of Earth materials. Each of these three modes will be considered in assessing flow processes in the lithosphere; these mechanical attributes are expressed in terms of lithospheric strength. This strength is estimated by integrating yield stress with depth. The current state of knowledge of rock rheology is sufficient to provide broad general outlines of mechanical behavior but also has important limitations. Two very thorny problems involve the scaling of rock properties with long periods and for very large length scales.
    [Show full text]
  • Lectures Notes on Mechanics of Solids
    Lectures notes On Mechanics of Solids Course Code- BME-203 Prepared by Prof. P. R. Dash SYLLABUS Module – I 1. Definition of stress, stress tensor, normal and shear stresses in axially loaded members. Stress & Strain :- Stress-strain relationship, Hooke’s law, Poisson’s ratio, shear stress, shear strain, modulus of rigidity. Relationship between material properties of isotropic materials. Stress-strain diagram for uniaxial loading of ductile and brittle materials. Introduction to mechanical properties of metals-hardness,impact. Composite Bars In Tension & Compression:-Temperature stresses in composite rods – statically indeterminate problem. (10) Module – II 2. Two Dimensional State of Stress and Strain: Principal stresses, principal strains and principal axes, calculation of principal stresses from principal strains.Stresses in thin cylinder and thin spherical shells under internal pressure , wire winding of thin cylinders. 3. Torsion of solid circular shafts, twisting moment, strength of solid and hollow circular shafts and strength of shafts in combined bending and twisting. (10) Module – III 4. Shear Force And Bending Moment Diagram: For simple beams, support reactions for statically determinant beams, relationship between bending moment and shear force, shear force and bending moment diagrams. 5. Pure bending theory of initially straight beams, distribution of normal and shear stress, beams of two materials. 6. Deflection of beams by integration method and area moment method. (12) Module – IV 7. Closed coiled helical springs. 8. Buckling of columns : Euler’s theory of initially straight columns with various end conditions, Eccentric loading of columns. Columns with initial curvature. (8) 1 Text Books-: 1. Strength of materials by G. H. Ryder, Mc Millan India Ltd., 2.
    [Show full text]
  • ENGR 151--Strength of Materials Tension Testing Lab Exercise #2: Tension Testing (Uniaxial Stress)
    ENGR 151--Strength of Materials Tension Testing Lab Exercise #2: Tension Testing (Uniaxial Stress) Learning Outcomes: 1. Understand the basic concepts of stress and strain 2. Identify the engineering material properties 3. Connect stress and strain through Hooke’s Law and Young’s Modulus 4. To be able to generate stress-strain diagrams for samples experiencing tension 5. The ability to analyze and interpret data Principles: Tensile testing is one of the more basic tests to determine stress – strain relationships. A simple uniaxial test consists of slowly pulling a sample of material in tension until it breaks. Test specimens for tensile testing are generally either circular or rectangular with larger ends to facilitate gripping the sample. The typical test is to deform or “stretch” the material at a constant speed. The required load that must be applied to achieve this displacement will vary as the test proceeds. The stress in the sample can be calculated by dividing the load by the initial cross-sectional area (σ =P/A). The displacement in the sample can be measured at any section where the cross-sectional area is constant. The strain is calculated by taking this change in length and dividing it by the initial length (ε=∆L/L0). Engineering stress and strain (constant cross section) will be recorded, as opposed to the actual, (variable cross section). This is because the actual cross section of the specimen is very difficult to measure. Engineering material properties that can be found from simple tensile testing include the elastic modulus (modulus of elasticity or Young’s modulus), ultimate tensile strength (tensile strength), yield strength, fracture strength.
    [Show full text]
  • Strength of Materials (Basic Knowledge)
    Engineering mechanics – strength of materials 2 Introduction gunt Strength of materials Strength of materials is based on statics. The idealisation of a Strength of materials deals with the effect of forces on deform- Elastic deformation, law of elasticity real body as a rigid body in statics allows determining the exter- able bodies. In addition, material-dependent parameters should Machines and components elastically deform under the action mation of solids when this deformation is proportional to the nal and internal forces on structures under equilibrium. Ensur- be considered as well. An introduction to the strength of mate- of forces. While the load is not large enough, purely elastic defor- applied force. ing equilibrium is not suffi cient for calculating the mechanical rials is, therefore, given by the concept of stress and strain and mation remains. The law of elasticity describes the elastic defor- behaviour of components, including strength, rigidity, stability, by Hooke’s law, which is applied to tension, pressure, torsion and fatigue strength and ductility, in the real world of engineering bending problems. Energy methods practice. Knowledge of the deformability of material bodies is required, without consideration of the material. Geometric considerations play a subordinate role in the energy Different energy methods are used to calculate general systems methods. Instead of the previously used equilibrium conditions, and to investigate the stability of elastic structures, such as the we investigate how much work is produced by external forces principle of virtual displacement, the principle of virtual forces, Basic terms of materials strength during deformation of a system and in which energy form and the Maxwell-Betti theorem, or Castigliano’s theorem.
    [Show full text]
  • Design for Static Strength
    PDHonline Course G204 (6 PDH) Design for Static Strength Instructor: Robert B. Wilcox, P.E. 2012 PDH Online | PDH Center 5272 Meadow Estates Drive Fairfax, VA 22030-6658 Phone & Fax: 703-988-0088 www.PDHonline.org www.PDHcenter.com An Approved Continuing Education Provider www.PDHcenter.com PDH Course G204 www.PDHonline.org Design for Static Strength Robert B. Wilcox, P.E. 1.0 Prerequisites It is assumed the student has a working knowledge of stress analysis and is able to determine the state of stress at the critical location of the part. It is also assumed that the materials being evaluated are linear elastic materials, and that the loading is static. 2.0 Material Properties and Testing When a body is subjected to a purely axial load, it will elongate. This elongation is called normal strain, ε, and it is defined as the change in elongation, ∆L, divided by the original length, L. Thus normal engineering strain is defined as: ε = ∆L/L The axial load, call it "P" will create a state of normal stress, σ, in the material, defined as the load divided by the cross sectional area, "A" of the part. In the case of a simple bar in tension then, the normal stress is: σ = P/A Axial stress and strain are linearly related to one another and as long as the material is not stressed beyond a certain point, called the yield strength, it will behave in a linearly elastic manner under loading. That means it stretches under the load, but if the load is removed, it returns to its original length with no permanent, or plastic, deformation.
    [Show full text]
  • CE8395 Strength of Materials for Mechanical Engineers
    CE8395 Strength of materials for Mechanical Engineers TWO MARK QUESTIONS & ANSWERS CE8395 Strength of materials for Mechanical Engineers Syllabus OBJECTIVES: • To understand the concepts of stress, strain, principal stresses and principal planes. • To study the concept of shearing force and bending moment due to external loads in determinate beams and their effect on stresses. • To determine stresses and deformation in circular shafts and helical spring due to torsion. • To compute slopes and deflections in determinate beams by various methods. • To study the stresses and deformations induced in thin and thick shells. UNIT I STRESS, STRAIN AND DEFORMATION OF SOLIDS 9 Rigid bodies and deformable solids – Tension, Compression and Shear Stresses – Deformation of simple and compound bars – Thermal stresses – Elastic constants – Volumetric strains – Stresses on inclined planes – principal stresses and principal planes – Mohr’s circle of stress. UNIT II TRANSVERSE LOADING ON BEAMS AND STRESSES IN BEAM 9 Beams – types transverse loading on beams – Shear force and bending moment in beams – Cantilevers – Simply supported beams and over – hanging beams. Theory of simple bending– bending stress distribution – Load carrying capacity – Proportioning of sections – Flitched beams – Shear stress distribution. UNIT III TORSION 9 Torsion formulation stresses and deformation in circular and hollows shafts – Stepped shafts– Deflection in shafts fixed at the both ends – Stresses in helical springs – Deflection of helical springs, carriage springs. UNIT IV DEFLECTION OF BEAMS 9 Double Integration method – Macaulay’s method – Area moment method for computation of slopes and deflections in beams - Conjugate beam and strain energy – Maxwell’s reciprocal theorems. UNIT V THIN CYLINDERS, SPHERES AND THICK CYLINDERS 9 Stresses in thin cylindrical shell due to internal pressure circumferential and longitudinal stresses and deformation in thin and thick cylinders – spherical shells subjected to internal pressure –Deformation in spherical shells – Lame’s theorem.
    [Show full text]
  • Solid Mechanics at Harvard University
    SOLID MECHANICS James R. Rice School of Engineering and Applied Sciences, and Department of Earth and Planetary Sciences Harvard University, Cambridge, MA 02138 USA Original version: October 1994 This revision: February 2010 Downloadable at: http://esag.harvard.edu/rice/e0_Solid_Mechanics_94_10.pdf TABLE OF CONTENTS provided on last three pages, pp. 87-89 INTRODUCTION The application of the principles of mechanics to bulk matter is conventionally divided into the mechanics of fluids and the mechanics of solids. The entire subject is often called continuum mechanics, particularly when we adopt the useful model of matter as being continuously divisible, making no reference to its discrete structure at microscopic length scales well below those of the application or phenomenon of interest. Solid mechanics is concerned with the stressing, deformation and failure of solid materials and structures. What, then, is a solid? Any material, fluid or solid, can support normal forces. These are forces directed perpendicular, or normal, to a material plane across which they act. The force per unit of area of that plane is called the normal stress. Water at the base of a pond, air in an automobile tire, the stones of a Roman arch, rocks at base of a mountain, the skin of a pressurized airplane cabin, a stretched rubber band and the bones of a runner all support force in that way (some only when the force is compressive). We call a material solid rather than fluid if it can also support a substantial shearing force over the time scale of some natural process or technological application of interest.
    [Show full text]