and Tetsuyuki Sasai* *, Members, TMSJ Abstract

Size: px
Start display at page:

Download "and Tetsuyuki Sasai* *, Members, TMSJ Abstract"

Transcription

1 N Theoretical Analysis on Tensile Properties of Textured Yarns By Sueo Kawabata* and Tetsuyuki Sasai* *, Members, TMSJ *Department of Polymer Chemistry, Kyoto University, Kyoto * *Faculty of Engineering, Gunma University, Kiryu, Gunma Prefecture Based on the Journal of the Textile Machinery Society of Japan, Transactions, Vol. 29, No. 10, T (1976) Abstract In this paper, tensile properties of textured yarns will be analysed. First, the property is calculated on the basis of a "independent fiber model" where each fiber contributes independently to the yarn tensile property, i.e., no mechanical interactions among fibers are considered. One of the purpose of this paper is to examine the accuracy of this no-interaction assumption for making distinct the mechanical interaction among fibers. Second, the tensile property of a crimped single fiber is calculated by applying the so-called "strain additive method"~l~ to a helical coil model of a fiber. Then the tensile property of a textured yarn is introduced by summing up the tensile property of each crimped fiber. A good agreement between the calculated and the observed values is obtained over a wide range of the tensile atrain of the yarn by assuming the independent model. No interaction is observed except the small deformation region. The hysteresis behavior observed at the repeated extension is also examined, and it is confirmed that the independent model is still suitable for this case. The experimental results agree well with the calculated results with good accuracy, too. 1. Introduction For analysing the tensile property of a crimped fiber, KondoL2~ considered two models for a crimped fiber : a plane zig-zag form and a three-dimensional helical spring form. He examined the conformity between the calculated and the experimental values of load-extension curves. Kawasaki et al.~37 and Holdaway~4~ also expressed the loadextension curve by applying a helical coil model. It is however difficult to apply their theory to our study just as it is, because they did not take into consideration the elongation of fibers themselves during the extension of the spring model. This neglect leads to considerable error in actual cases, and is not suitable for our precise calculation of the load-extension curve. In this paper, we first apply a large deformation equation equation of a helical coill3,6,7] to calculate the tensile property of a crimped fiber with no fiber elongation. Then we use the so-called "strain additive method"~l~ to introduce the fiber elongation to its load-extension property. The strain additive method is as follows: The tensile deformation of a helical coil is composed of two deformations, coil extension and fiber extension. Both deformations, of course, occur at the same time during the extension process of the helical coil. However, the analysis of it becomes much complicated. Therefore, we calculate first the load-extension curve with no fiber elongation using the equation of large deformation of a helical coil, and combine it with the tensile property of the fiber in a straight form by the following Vol. 24 No,1(1978) method such that both elongations corresponding to the same stretching force are summed up together. Then, we calculate the tensile property of the textured yarn using an "independent fiber model", and will examine whether the mechanical interaction between fibers will exist or not by comparing the calculated results with the experimental ones. 2. Theory 2.1 Yarn model We assume that the tensile property of each crimped fiber contributes independently to the tensile property of a yarn with no interaction among fibers. We call this the "independent fiber model". Following the model, the tensile force of a yarn can be obtained by summing up the forces of all fibers in the yarn as follows; F(A)=j f (2) i_1...(1) where t~11v1v /~] : extension ratio 11L~1V of Vl ~i a yarn,6l111 F(A) : tensile force of the yarn as a function of A f (A): tensile force of a crimped fiber in the yarn as a function of A N: number of fibers in the yarn cross-section. In the case when all fibers in a yarn have the same tensile property, Eq. (1) becomes F(A) =N f (A)...(2) In order to examine the conformity of this independent 13

2 fiber-model, it is necessary to know the precise tensile property of a crimped fiber. 2.2 Model of a crimped fiber We have assumed two models on the form of a crimped fiber, a helical coil model and a plane-arc-bar model.~6~ Comparing the values calculated on those two models with the experimental results, we found already that values from the helical coil model showed better agreement with the experiment than values from the plane-arc-bar model.~61 Thus we use the helical coil model for the crimped fiber. Fig. 1 shows the helical coil model. The details are given in the next section. 2.3 Tensile force of a crimped fiber We devide the extension deformation of a helical coil model into two deformations. The first is the extension deformation due to the extension of a helical coil while the fiber itself is assumed not to be elongated along the fiber axis. We call this the "coil effect region". Another is the extension deformation due to the elongation of the fiber straightened. We call this the "extension effect region". In our method, the latter region starts when the coil effect region ended just after the coil was straightened. The "critical extension state" is the state when the coil became straight at the end of the coil effect region. It should be noted that these deformations and states do not exist in actual cases, but are only considered as an ideal model of deformation. Then, the effects of these two regions are combined by strain additive method as follows; x(f)=xh(f)+xt(f)...(3) where f : tensile force along the coil-axis x(f) : elongation of the crimped fiber along the coilaxis xh(f) : elongation of the coil model as a function of the applied tensile force. The calculation is carried out under the assumption that the fiber is not elongated. XT(f) : elongation of the fiber as a function of the applied tensile force after the fiber is straightened. Fig. 1 Helical coil model. In the coil effect region, the tensile force, fh, can be calculated by following equations~5'6'7~ (see Appendix); f( n d4e ~ 2)= -a-- R~ sin a cost a (\/'+2m(1---)-1) -stn a 1- ~ sin a ~... (4) where m : =G/E G : shear modulus of the fiber E: tensile modulus of the fiber d: diameter of the fiber when the cross-section is assumed circular A : extension ratio of the helical coil. Here, a, R and n are reduced from next equations; sina = o/lc...(5) R=l~ cosa/2,rn...(6) n=lo/(2~rr~tana)...(7) A where to : length of the coil before extension l~ : length of the coil at the critical extension state. It is equal to the length of the fiber under no tension. a : helical angle n : number of turns of the coil R : radius of the coil. In the extension effect region, the tensile property of the straightened fiber is used for obtaining xt(f ). 2.4 Critical extension ratio l~ is defined as the length of the crimped fiber at the critical extension state, and the critical extension ratio A~ is defined as follows :...(8) For the discussion of the tensileproperty of a crimped fiber, it is difficult to define the initial length of the crimped shape because of its uncertainty. However, the elongated state of a crimped fiber can be determined clearly by considering the critical extension state as the base length. Now, we can define A which is the stretch ratio based on the length at the critical extension state such that, A=l/l~...(9) =(lha)/l~/lo =A/A~ 3. Experiment (10) 3.1 Preparation of specimens and experimental apparatus Specimens used in this expriement are polyester falsetwisted textured yarns of 150 d, 48 fil. An apparatus to bring about and stabilize the crimps of yarns is shown schematically in Fig. 2. The specimen is passed for 15 sec with no tension through a pipe to which saturated water vapor at 100 C is supplied from the boiling vessel. After this process, the yarn is dried up for 24 hrs in room condi- 14 Journal of The Textile Machinery Society of Japan

3 tion. For measuring the tensile properties of yarns and fibers, the precise tensile tester KES-G1 is used. For the torsional experiment of a single fiber to obtain shear modulus G, KES-Y1 is used. Both testers were developed by Kawabata. 3.2 Measurement of tensile properties of fibers Fig. 3 shows the stretch and recovery behavior of a single fiber observed by repeated tensile test. The numbers put near the curves show the order of repeated stretch: 1 indicates the first cycle of the vergin specimen after the vapor treatment, 2 the second cycle and so forth. The fourth stretch and thereafter give almost the same cruves as the third. Thus, the specimen after the third stretch is assumed to be in the stable state. Young's modulus E of the fiber is estimated from the slope of the straight part of the curve for each cycle. G is measured directly by the torsional testing machine under constant tension. The fiber length l~ can be measured by the photographic observation of the crimped fiber. The number of crimps per unit length of the fiber is determined by calculating the auto-correlation function of the projected curve of the crimped fiber as shown later, and is used as the value of n of the helical coil model. The fiber length at the critical state, l~, is presumed, as is illustrated in Fig. 4, from the intetsecting point of the horizontal axis with the extrapolated line of the linear part of the forceextension curve of the crimped fiber. The value of 1, is again confirmed by observing the fiber length on its photographic picture. Those values obtained above are then substituted into Eq. (4) to obtain a force-extension curve of a crimped fiber. Here, we have to call into a question about the fiber to fiber variation of these values, as there is considerably large variation between fibers. One reason for this is probably due to the variation of drawing conditions during spinning; the correlation between E and d is clearly observed as shown in Fig. 5. To make this variation effect on calculated results small, averages of about thirty fibers are used here as the representative values. Especially, we use the average d 4E instead of d ~E in Eq. (4) because of the correlation be- Fig. 4 Estimation of l~ of a crimped fibr. Fig. 2 Apparatus for bringing about and stabilizing crimps. Fig. 3 Repeated extension of a crimped fiber (experimental). Vol. 24 No, 1(1978) Fig. 5 Relation between E and d. Mark x points out the average. 15

4 Table 1 Characteristic values of crimped fibers. tween E and d. These characteristic values are shown in Table 1 for the first and the third cycles of repeated stretch. 3.3 Comparison between calculated and experimental results The tensile property of a fiber in the coil effect region is calculated by substituting the values shown in Table 1 into Eq. (4). On the other hand, the tensile property of the fiber is estimated from the force-extension curve of the crimped fiber by extrapolating the linear part of the curve, and we obtain the curve of the extension effect region as a fiber property. The complete curve in the tensile prosess is then obtained by combining the calculated values in the coil effect region with the observed values in the extension effect region using the strain additive method shown by Eq. (3). The tensile property of a fiber calculated from Eq. (3) is shown by dotted lines in Fig. 6. Both the calculated property in the coil effect region and that in the extension effect region are also shown seperately in this figure by solid lines. The curve of the third cycle is calculated by using the observed values of n and h from the crimped fiber after the second stretch, and the steretch ratio is defined by l~ of the first cycle. In Fig. 7, the calculated force-extension curve of a crimped fiber is compared with the experimental one. It is found that a good agreement is obtained between them. Because characteristic values vary considerably among fibers as mentioned before, a good agreement can only be obtained by using their averages. The curve of the third cycle slips aside from that of the first cycle by considerable amount as shown in Figs. 6 and 7. This shift is due to the change of the crimp shape by repeated extension, resulting in the change of n and R. Fig. 8 is the trace of crimped fibers projected on a plane after each repeated stretch. The change of shapes can be observed clearly. 3.4 Comparison between calculated and experimental values Using the independent fiber bundle model for textured yarns, we can introduce the force-extension property of a yarn by summing up the calculated force of each crimped fiber under given stretch ratio. This idea is proved sound by Fig. 7 Calculated and experimental curves of the tensile property of a crimped fiber. Fig. 6 Calculated tensile property of a crimped fiber. (Thick solid lines give the calculated properties of the coil effect region. Fine solid lines are of the extension effect region. Dotted lines are obtained from Eq. (3) using those two curves.) 16 Fig. 8 Plane projection of fibers after repeated stretch. Journal of The Textile Machinery Society of Japan

5 pictures of a yarn stretched as shown in Fig. 10(b). Fig. 10 (a) shows the yarn appearance at A=0.473 of specimen 1 in Table 1, and its tension is extremely low. However, (b) is the appearance in the critical extension state having ~= In both states, fibers look like independent each other. (a) and (b) in Fig. 9 show these two states respectively. The calculated ourve is shown in Fig. 11 together with the experimental curve. The figure shows that the observed forces at given stretch ratios are a little higher than the calculated in the low extension region. This is probably due to the error caused by the independent fiber bundle model; the crimped fibers contact each other complicatedly and entangle in the low extension state. However once the entwining is released by the first stretch, a good agreement between the experimental and the calculated values can be observed. 3.5 Hysteresis behavior of yarns also apply the fiber. the properties and the structural parameters of The good agreement between calculated and experimental Fig. 11 Calculated and experimental curves of the tensile properties results of force-extension behavior of textured yarns is observed in the stretch process. The similar agreement is observed in the recovering process, and to the analysis of of a textured yarn. which we again use the independent fiber bundle model and 4. Conclusions Fig. 9 Repeated extension of a textured yarn (experimental). We have found first that the tensile property of a crimped fiber can be calculated precisely by using a helical coil model and the strain additive method. Secondly the tensile property of a textured yarn can be calculated by using an independent fiber bundle model. However it is very difficult to obtain the values most adequate to the mechanical properties and to the structural parameters of component fibers because of their large variation. It necessitates us o use average values of those fibers. We also have to use d 4E instead of d4e in Eq. (4), as there is a correlation bweteen d and E. These two cases will result in the error about 5 %. The tensile property of a yarn is then obtained from Eq. (2) based on the assumption of the independent fiber bundle model. The calculated result agrees well with the experimental one. We have also discussed the repeated stretch, which is the origin of both the configuration change of the fiber and the number of turns of helical coil per unit length. If we introduce those changes into calculation, the value obtained agrees well with the experimental value. Fig. 10 Appearance of yarns when stretched. = (a) A =0.473, (b) Acknowledgement The authors feel grateful to Professor H. Kawai, Kyoto University, for his useful suggestions. They also thank to Associate Professor M. Niwa, Nara Women's University, for her valuable discussion and helpful support. (Most of the experiments in this paper was done in Kyoto University from May, 1970 to February, 1971, by one of the authors, T. Sasai.) Vol. 24 No.1(1978) 17

6 References [1] S. Kawabata; J. Text. Mac., Soc. Japan, 23, T30 (1970) [2] T. Kondo; Memoirs of Training Institute for Engineering Teachers, Kyoto University, 2, 16 (1966) [3] K. Kawasaki and S. Murata; J. Soc. Fiber Sci. Tech., Japan, 15, 814 (1959) K. Kawasaki; "General Discussions on Textured Yarns", Text. Mac. Soc. Japan (1966) [4] H. W. Holdaway; J. Text. Inst., 47, T586 (1956) [5] S. Kawabata; Proceeding of the 5th Summer Seminar, Soc. Fiber Sci. Tech., Japan (1972) [6] S. Kawabata, M. Niwa and S. Nakabayashi; J. Text. Mac. Soc. Japan, 28, T153 (1975) [7] S. Kawabata and T. Sasai; J. Text. Mac. Soc. Japan, 28, T157 (1975) [8] S. Kawabata, M. Niwa and T. Mamiya; J. Text. Mac. Soc. Japan, 29, T119 (1976) [9] A. E. H. Love; "A Treatise on the Mathematical Theory of Elasticity", First ed., Cambridge University Press, and The Macmillan Co. Dover Publ., New York (1944). Appendix (1892), Fourth ed., The basis of the large deformation theory of a thin lod is expressed in detail in the classical work by A. E. H. Love.E9] The tensile force F of a helical coil, which is obtained by applying his basic equations written on page 397 to a helical coil is as follows; cosai sinai cosai - sina cosa ri ri r _B sinai cosai (cos2ai - cos2a ri ri r where C and B are the torsional and the bending rigidities, a and r the helical angle and the radius of the helical coil before deformation, ai and ri those values after deformation, respectively. By modifying this equation to use more easily, we can get Eq. (6). 18 Journal of The Textile Machinery Society of Japan

Stress Strain Elasticity Modulus Young s Modulus Shear Modulus Bulk Modulus. Case study

Stress Strain Elasticity Modulus Young s Modulus Shear Modulus Bulk Modulus. Case study Stress Strain Elasticity Modulus Young s Modulus Shear Modulus Bulk Modulus Case study 2 In field of Physics, it explains how an object deforms under an applied force Real rigid bodies are elastic we can

More information

CHAPTER 3 THE EFFECTS OF FORCES ON MATERIALS

CHAPTER 3 THE EFFECTS OF FORCES ON MATERIALS CHAPTER THE EFFECTS OF FORCES ON MATERIALS EXERCISE 1, Page 50 1. A rectangular bar having a cross-sectional area of 80 mm has a tensile force of 0 kn applied to it. Determine the stress in the bar. Stress

More information

AERO 214. Lab II. Measurement of elastic moduli using bending of beams and torsion of bars

AERO 214. Lab II. Measurement of elastic moduli using bending of beams and torsion of bars AERO 214 Lab II. Measurement of elastic moduli using bending of beams and torsion of bars BENDING EXPERIMENT Introduction Flexural properties of materials are of interest to engineers in many different

More information

STANDARD SAMPLE. Reduced section " Diameter. Diameter. 2" Gauge length. Radius

STANDARD SAMPLE. Reduced section  Diameter. Diameter. 2 Gauge length. Radius MATERIAL PROPERTIES TENSILE MEASUREMENT F l l 0 A 0 F STANDARD SAMPLE Reduced section 2 " 1 4 0.505" Diameter 3 4 " Diameter 2" Gauge length 3 8 " Radius TYPICAL APPARATUS Load cell Extensometer Specimen

More information

Members Subjected to Torsional Loads

Members Subjected to Torsional Loads Members Subjected to Torsional Loads Torsion of circular shafts Definition of Torsion: Consider a shaft rigidly clamped at one end and twisted at the other end by a torque T = F.d applied in a plane perpendicular

More information

Supporting Information

Supporting Information Supporting Information Stepped Moduli in Layered Composites Ju-Hee So 1, Alok Tayi 1, Firat Guder, and George M. Whitesides 1,* 1 Department of Chemistry and Chemical Biology, Harvard University, 1 Oxford

More information

TORSION TEST. Figure 1 Schematic view of torsion test

TORSION TEST. Figure 1 Schematic view of torsion test TORSION TEST 1. THE PURPOSE OF THE TEST The torsion test is performed for determining the properties of materials like shear modulus (G) and shear yield stress ( A ). 2. IDENTIFICATIONS: Shear modulus:

More information

Stress-Strain Behavior

Stress-Strain Behavior Stress-Strain Behavior 6.3 A specimen of aluminum having a rectangular cross section 10 mm 1.7 mm (0.4 in. 0.5 in.) is pulled in tension with 35,500 N (8000 lb f ) force, producing only elastic deformation.

More information

ME 2570 MECHANICS OF MATERIALS

ME 2570 MECHANICS OF MATERIALS ME 2570 MECHANICS OF MATERIALS Chapter III. Mechanical Properties of Materials 1 Tension and Compression Test The strength of a material depends on its ability to sustain a load without undue deformation

More information

Evaluation of Shittori Characteristic for Fabrics

Evaluation of Shittori Characteristic for Fabrics ORIGINAL PAPER Journal of Textile Engineering (2008), Vol.54, No.3, 75-81 2008 The Textile Machinery Society of Japan Evaluation of Shittori Characteristic for Fabrics TANAKA Yukari a,*, SUKIGARA Sachiko

More information

Objectives: After completion of this module, you should be able to:

Objectives: After completion of this module, you should be able to: Chapter 12 Objectives: After completion of this module, you should be able to: Demonstrate your understanding of elasticity, elastic limit, stress, strain, and ultimate strength. Write and apply formulas

More information

Mechanical Engineering Ph.D. Preliminary Qualifying Examination Solid Mechanics February 25, 2002

Mechanical Engineering Ph.D. Preliminary Qualifying Examination Solid Mechanics February 25, 2002 student personal identification (ID) number on each sheet. Do not write your name on any sheet. #1. A homogeneous, isotropic, linear elastic bar has rectangular cross sectional area A, modulus of elasticity

More information

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV UNIT I STRESS, STRAIN DEFORMATION OF SOLIDS PART A (2 MARKS)

More information

Sean Carey Tafe No Lab Report: Hounsfield Tension Test

Sean Carey Tafe No Lab Report: Hounsfield Tension Test Sean Carey Tafe No. 366851615 Lab Report: Hounsfield Tension Test August 2012 The Hounsfield Tester The Hounsfield Tester can do a variety of tests on a small test-piece. It is mostly used for tensile

More information

Anisotropy of the Static Friction. of Plain-woven Filament Fabrics

Anisotropy of the Static Friction. of Plain-woven Filament Fabrics Anisotropy of the Static Friction of Plain-woven Filament Fabrics By Masayasu Ohsawa and Satoru Nam iki, Members, T M S J Faculty of Technology, Tokyo University of Agriculture and Technology, Koganei,

More information

TENSILE TESTS (ASTM D 638, ISO

TENSILE TESTS (ASTM D 638, ISO MODULE 4 The mechanical properties, among all the properties of plastic materials, are often the most important properties because virtually all service conditions and the majority of end-use applications

More information

MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS

MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS AUTEX Research Journal, Vol. 3, No4, December 003 AUTEX MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS Part II: 3D model based on the elastica theory

More information

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1 UNIT I STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define: Stress When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The

More information

Friction Properties of Surface with Circular Micro-patterns

Friction Properties of Surface with Circular Micro-patterns Friction Properties of Surface with Circular Micro-patterns Hideo Koguchi Mechanical Engineering, 603- Kamitomioka, Nagaoka Univ. of Tech., Nagaoka, Niigata, Japan Email: koguchi@mech.nagaokaut.ac.jp Takayoshi

More information

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State Hooke s law. 3. Define modular ratio,

More information

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A DEPARTMENT: CIVIL SUBJECT CODE: CE2201 QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State

More information

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown. D : SOLID MECHANICS Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown. Q.2 Consider the forces of magnitude F acting on the sides of the regular hexagon having

More information

The objective of this experiment is to investigate the behavior of steel specimen under a tensile test and to determine it's properties.

The objective of this experiment is to investigate the behavior of steel specimen under a tensile test and to determine it's properties. Objective: The objective of this experiment is to investigate the behavior of steel specimen under a tensile test and to determine it's properties. Introduction: Mechanical testing plays an important role

More information

FAVIMAT (AI)ROBOT2 FAVIGRAPH. Automatic Single-Fibre Testers

FAVIMAT (AI)ROBOT2 FAVIGRAPH. Automatic Single-Fibre Testers FAVIMAT (AI)ROBOT2 FAVIGRAPH Automatic Single-Fibre Testers Single-Fibre Testers FAVIMAT and FAVIGRAPH The FAVIMAT testing methods Testing and evaluation of a wide range of fibre properties are essential

More information

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC.

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC. BENDING STRESS The effect of a bending moment applied to a cross-section of a beam is to induce a state of stress across that section. These stresses are known as bending stresses and they act normally

More information

Chapter 7. Highlights:

Chapter 7. Highlights: Chapter 7 Highlights: 1. Understand the basic concepts of engineering stress and strain, yield strength, tensile strength, Young's(elastic) modulus, ductility, toughness, resilience, true stress and true

More information

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM - 613 403 - THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Sub : Strength of Materials Year / Sem: II / III Sub Code : MEB 310

More information

DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1

DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1 DRAPING SIMULATION Recent achievements and future trends 1 Dr. Sylvain Bel LGCIE University Lyon 1 2 DRAPING SIMULATION Why? How? What? DRAPING SIMULATION WHY? Clamps Punch Fabric Die 1 2 Resin 3 4 Fig.

More information

Module 3 : Equilibrium of rods and plates Lecture 15 : Torsion of rods. The Lecture Contains: Torsion of Rods. Torsional Energy

Module 3 : Equilibrium of rods and plates Lecture 15 : Torsion of rods. The Lecture Contains: Torsion of Rods. Torsional Energy The Lecture Contains: Torsion of Rods Torsional Energy This lecture is adopted from the following book 1. Theory of Elasticity, 3 rd edition by Landau and Lifshitz. Course of Theoretical Physics, vol-7

More information

Physics 3 Summer 1989 Lab 7 - Elasticity

Physics 3 Summer 1989 Lab 7 - Elasticity Physics 3 Summer 1989 Lab 7 - Elasticity Theory All materials deform to some extent when subjected to a stress (a force per unit area). Elastic materials have internal forces which restore the size and

More information

Laboratory 4 Topic: Buckling

Laboratory 4 Topic: Buckling Laboratory 4 Topic: Buckling Objectives: To record the load-deflection response of a clamped-clamped column. To identify, from the recorded response, the collapse load of the column. Introduction: Buckling

More information

2. be aware of the thermal properties of materials and their practical importance in everyday life;

2. be aware of the thermal properties of materials and their practical importance in everyday life; MODULE 3: THERMAL AND MECHANICAL PROPERTIES OF MATTER GENERAL OBJECTIVES On completion of this Module, students should: 1. understand the principles involved in the design and use of thermometers; 2. be

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

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

STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING

STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING 1 YEDITEPE UNIVERSITY ENGINEERING FACULTY MECHANICAL ENGINEERING LABORATORY 1. Objective: Strain Gauges Know how the change in resistance

More information

Elastic Properties of Solid Materials. Notes based on those by James Irvine at

Elastic Properties of Solid Materials. Notes based on those by James Irvine at Elastic Properties of Solid Materials Notes based on those by James Irvine at www.antonine-education.co.uk Key Words Density, Elastic, Plastic, Stress, Strain, Young modulus We study how materials behave

More information

DEPARTMENT OF MECHANICAL ENIGINEERING, UNIVERSITY OF ENGINEERING & TECHNOLOGY LAHORE (KSK CAMPUS).

DEPARTMENT OF MECHANICAL ENIGINEERING, UNIVERSITY OF ENGINEERING & TECHNOLOGY LAHORE (KSK CAMPUS). DEPARTMENT OF MECHANICAL ENIGINEERING, UNIVERSITY OF ENGINEERING & TECHNOLOGY LAHORE (KSK CAMPUS). Lab Director: Coordinating Staff: Mr. Muhammad Farooq (Lecturer) Mr. Liaquat Qureshi (Lab Supervisor)

More information

Mechanics of Solids. Mechanics Of Solids. Suraj kr. Ray Department of Civil Engineering

Mechanics of Solids. Mechanics Of Solids. Suraj kr. Ray Department of Civil Engineering Mechanics Of Solids Suraj kr. Ray (surajjj2445@gmail.com) Department of Civil Engineering 1 Mechanics of Solids is a branch of applied mechanics that deals with the behaviour of solid bodies subjected

More information

MECE 3321 MECHANICS OF SOLIDS CHAPTER 3

MECE 3321 MECHANICS OF SOLIDS CHAPTER 3 MECE 3321 MECHANICS OF SOLIDS CHAPTER 3 Samantha Ramirez TENSION AND COMPRESSION TESTS Tension and compression tests are used primarily to determine the relationship between σ avg and ε avg in any material.

More information

NAME: Given Formulae: Law of Cosines: Law of Sines:

NAME: Given Formulae: Law of Cosines: Law of Sines: NME: Given Formulae: Law of Cosines: EXM 3 PST PROBLEMS (LESSONS 21 TO 28) 100 points Thursday, November 16, 2017, 7pm to 9:30, Room 200 You are allowed to use a calculator and drawing equipment, only.

More information

Initial Stress Calculations

Initial Stress Calculations Initial Stress Calculations The following are the initial hand stress calculations conducted during the early stages of the design process. Therefore, some of the material properties as well as dimensions

More information

2012 MECHANICS OF SOLIDS

2012 MECHANICS OF SOLIDS R10 SET - 1 II B.Tech II Semester, Regular Examinations, April 2012 MECHANICS OF SOLIDS (Com. to ME, AME, MM) Time: 3 hours Max. Marks: 75 Answer any FIVE Questions All Questions carry Equal Marks ~~~~~~~~~~~~~~~~~~~~~~

More information

Introduction to Engineering Materials ENGR2000. Dr. Coates

Introduction to Engineering Materials ENGR2000. Dr. Coates Introduction to Engineering Materials ENGR2 Chapter 6: Mechanical Properties of Metals Dr. Coates 6.2 Concepts of Stress and Strain tension compression shear torsion Tension Tests The specimen is deformed

More information

CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR

CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR 2014-2015 UNIT - 1 STRESS, STRAIN AND DEFORMATION OF SOLIDS PART- A 1. Define tensile stress and tensile strain. The stress induced

More information

Inclined plane with protractor and pulley, roller, weight box, spring balance, spirit level, pan and thread.

Inclined plane with protractor and pulley, roller, weight box, spring balance, spirit level, pan and thread. To find the downward force, along an inclined plane, acting on a roller due to gravity and study its relationship with the angle of inclination by plotting graph between force and sin θ. Inclined plane

More information

Nonlinear Analytical Model for Wire Strands

Nonlinear Analytical Model for Wire Strands Advances in Engineering Research, volume 4th International Conference on Renewable Energy and Environmental Technology (ICREET 06) Nonlinear Analytical Model for Wire Strands Chun-Lei Yu, a, Wen-Guang

More information

Flexural properties of polymers

Flexural properties of polymers A2 _EN BUDAPEST UNIVERSITY OF TECHNOLOGY AND ECONOMICS FACULTY OF MECHANICAL ENGINEERING DEPARTMENT OF POLYMER ENGINEERING Flexural properties of polymers BENDING TEST OF CHECK THE VALIDITY OF NOTE ON

More information

Static Equilibrium and Elasticity. Luis Anchordoqui

Static Equilibrium and Elasticity. Luis Anchordoqui Static Equilibrium and Elasticity The Conditions for Equilibrium An object with forces acting on it, but that is not moving, is said to be in equilibrium. The Conditions for Equilibrium (cont d) The first

More information

INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS

INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS ISSN 1846-6168 (Print), ISSN 1848-5588 (Online) ID: TG-217816142553 Original scientific paper INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS Željko PENAVA, Diana ŠIMIĆ PENAVA, Željko

More information

Moment of inertia of different bodies

Moment of inertia of different bodies Moment of inertia of different bodies Aim: 1) Study moment of inertia of different bodies Objectives of the experiment 1. Measuring the period of oscillation of a thin transverse rod with weights on a

More information

Lab Exercise #5: Tension and Bending with Strain Gages

Lab Exercise #5: Tension and Bending with Strain Gages Lab Exercise #5: Tension and Bending with Strain Gages Pre-lab assignment: Yes No Goals: 1. To evaluate tension and bending stress models and Hooke s Law. a. σ = Mc/I and σ = P/A 2. To determine material

More information

Prediction of Elastic Constants on 3D Four-directional Braided

Prediction of Elastic Constants on 3D Four-directional Braided Prediction of Elastic Constants on 3D Four-directional Braided Composites Prediction of Elastic Constants on 3D Four-directional Braided Composites Liang Dao Zhou 1,2,* and Zhuo Zhuang 1 1 School of Aerospace,

More information

ENG1001 Engineering Design 1

ENG1001 Engineering Design 1 ENG1001 Engineering Design 1 Structure & Loads Determine forces that act on structures causing it to deform, bend, and stretch Forces push/pull on objects Structures are loaded by: > Dead loads permanent

More information

ME 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 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 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

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE MODULE TOPIC PERIODS 1 Simple stresses

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

Experiment: Torsion Test Expected Duration: 1.25 Hours

Experiment: Torsion Test Expected Duration: 1.25 Hours Course: Higher Diploma in Civil Engineering Unit: Structural Analysis I Experiment: Expected Duration: 1.25 Hours Objective: 1. To determine the shear modulus of the metal specimens. 2. To determine the

More information

Outline. Tensile-Test Specimen and Machine. Stress-Strain Curve. Review of Mechanical Properties. Mechanical Behaviour

Outline. Tensile-Test Specimen and Machine. Stress-Strain Curve. Review of Mechanical Properties. Mechanical Behaviour Tensile-Test Specimen and Machine Review of Mechanical Properties Outline Tensile test True stress - true strain (flow curve) mechanical properties: - Resilience - Ductility - Toughness - Hardness A standard

More information

Lab Exercise #3: Torsion

Lab Exercise #3: Torsion Lab Exercise #3: Pre-lab assignment: Yes No Goals: 1. To evaluate the equations of angular displacement, shear stress, and shear strain for a shaft undergoing torsional stress. Principles: testing of round

More information

Module 4 : Deflection of Structures Lecture 4 : Strain Energy Method

Module 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 information

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR:

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR: MECHANICS OF STRUCTURES- ASSIGNMENT NO 1 SEMESTER: V 1) Find the least moment of Inertia about the centroidal axes X-X and Y-Y of an unequal angle section 125 mm 75 mm 10 mm as shown in figure 2) Determine

More information

122 CHAPTER 2 Axially Loaded Numbers. Stresses on Inclined Sections

122 CHAPTER 2 Axially Loaded Numbers. Stresses on Inclined Sections 1 CHATER Aiall Loaded Numbers Stresses on Inclined Sections roblem.6-1 A steel bar of rectangular cross section (1.5 in..0 in.) carries a tensile load (see figure). The allowable stresses in tension and

More information

PES Institute of Technology

PES Institute of Technology PES Institute of Technology Bangalore south campus, Bangalore-5460100 Department of Mechanical Engineering Faculty name : Madhu M Date: 29/06/2012 SEM : 3 rd A SEC Subject : MECHANICS OF MATERIALS Subject

More information

ERM - Elasticity and Strength of Materials

ERM - Elasticity and Strength of Materials Coordinating unit: Teaching unit: Academic year: Degree: ECTS credits: 2018 205 - ESEIAAT - Terrassa School of Industrial, Aerospace and Audiovisual Engineering 712 - EM - Department of Mechanical Engineering

More information

COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4017 COURSE CATEGORY : A PERIODS/WEEK : 6 PERIODS/ SEMESTER : 108 CREDITS : 5

COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4017 COURSE CATEGORY : A PERIODS/WEEK : 6 PERIODS/ SEMESTER : 108 CREDITS : 5 COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4017 COURSE CATEGORY : A PERIODS/WEEK : 6 PERIODS/ SEMESTER : 108 CREDITS : 5 TIME SCHEDULE MODULE TOPICS PERIODS 1 Simple stresses

More information

A concrete cylinder having a a diameter of of in. mm and elasticity. Stress and Strain: Stress and Strain: 0.

A concrete cylinder having a a diameter of of in. mm and elasticity. Stress and Strain: Stress and Strain: 0. 2011 earson Education, Inc., Upper Saddle River, NJ. ll rights reserved. This material is protected under all copyright laws as they currently 8 1. 3 1. concrete cylinder having a a diameter of of 6.00

More information

Part 1 is to be completed without notes, beam tables or a calculator. DO NOT turn Part 2 over until you have completed and turned in Part 1.

Part 1 is to be completed without notes, beam tables or a calculator. DO NOT turn Part 2 over until you have completed and turned in Part 1. NAME CM 3505 Fall 06 Test 2 Part 1 is to be completed without notes, beam tables or a calculator. Part 2 is to be completed after turning in Part 1. DO NOT turn Part 2 over until you have completed and

More information

6.4 A cylindrical specimen of a titanium alloy having an elastic modulus of 107 GPa ( psi) and

6.4 A cylindrical specimen of a titanium alloy having an elastic modulus of 107 GPa ( psi) and 6.4 A cylindrical specimen of a titanium alloy having an elastic modulus of 107 GPa (15.5 10 6 psi) and an original diameter of 3.8 mm (0.15 in.) will experience only elastic deformation when a tensile

More information

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation.

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The magnitude

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

DEFLECTION OF BEAMS WlTH SPECIAL REFERENCE TO SHEAR DEFORMATIONS

DEFLECTION OF BEAMS WlTH SPECIAL REFERENCE TO SHEAR DEFORMATIONS DEFLECTION OF BEAMS WlTH SPECIAL REFERENCE TO SHEAR DEFORMATIONS THE INFLUENCE OF THE FORM OF A WOODEN BEAM ON ITS STIFFNESS AND STRENGTH-I (REPRINT FROM NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS REPORT

More information

A Novel Approach for Measurement of Fiber-on-fiber Friction

A Novel Approach for Measurement of Fiber-on-fiber Friction F98S-09 Page 1 A Novel Approach for Measurement of Fiber-on-fiber Friction Number: F98S-09 Competency: Fabrication Team Leader and members: Y. Qiu, NCSU; Y. Wang, Georgia Tech; J.Z. Mi, Cotton Inc. Graduate

More information

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING QUESTION BANK FOR THE MECHANICS OF MATERIALS-I 1. A rod 150 cm long and of diameter 2.0 cm is subjected to an axial pull of 20 kn. If the modulus

More information

MECHANICAL PROPERTIES OF SOLIDS

MECHANICAL PROPERTIES OF SOLIDS INTRODUCTION A rigid body generally means a hard solid object having a definite shape and size. But in reality, bodies can be stretched, compressed and bent. Even the appreciably rigid steel bar can be

More information

Structural Metals Lab 1.2. Torsion Testing of Structural Metals. Standards ASTM E143: Shear Modulus at Room Temperature

Structural Metals Lab 1.2. Torsion Testing of Structural Metals. Standards ASTM E143: Shear Modulus at Room Temperature Torsion Testing of Structural Metals Standards ASTM E143: Shear Modulus at Room Temperature Purpose To determine the shear modulus of structural metals Equipment Tinius-Olsen Lo-Torq Torsion Machine (figure

More information

Keywords: textile composites, braided fabric, dynamic property, fracture aspect, matrix hybrid

Keywords: textile composites, braided fabric, dynamic property, fracture aspect, matrix hybrid Mechanical Properties and Fracture Behavior of Hybrid Braided Composite Tube Yuki Sasaki, Yoshitaka Tanaka, Akio Ohtani, Asami Nakai, Hiroyuki Hamada Kyoto Institute of Technology Matsugasaki, Sakyo-ku,

More information

INTRODUCTION (Cont..)

INTRODUCTION (Cont..) INTRODUCTION Name : Mohamad Redhwan Abd Aziz Post : Lecturer @ DEAN CENTER OF HND STUDIES Subject : Solid Mechanics Code : BME 2033 Room : CENTER OF HND STUDIES OFFICE H/P No. : 019-2579663 W/SITE : Http://tatiuc.edu.my/redhwan

More information

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS Name :. Roll No. :..... Invigilator s Signature :.. 2011 SOLID MECHANICS Time Allotted : 3 Hours Full Marks : 70 The figures in the margin indicate full marks. Candidates are required to give their answers

More information

OSCILLATIONS OF A SPRING-MASS SYSTEM AND A TORSIONAL PENDULUM

OSCILLATIONS OF A SPRING-MASS SYSTEM AND A TORSIONAL PENDULUM EXPERIMENT Spring-Mass System and a Torsional Pendulum OSCILLATIONS OF A SPRING-MASS SYSTEM AND A TORSIONAL PENDULUM Structure.1 Introduction Objectives. Determination of Spring Constant Static Method

More information

MULTI-SCALE MODELLING OF FIBRE BUNDLES

MULTI-SCALE MODELLING OF FIBRE BUNDLES THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS MULTI-SCALE MODELLING OF FIBRE BUNDLES N. D. Chakladar 1, P. Mandal 1 *, P. Potluri 2 1 School of Mechanical, Aerospace and Civil Engineering,

More information

INSPIRE GK12 Lesson Plan. Elastic Deformation of Materials: An Investigation of Hooke s Law Length of Lesson

INSPIRE GK12 Lesson Plan. Elastic Deformation of Materials: An Investigation of Hooke s Law Length of Lesson Lesson Title Elastic Deformation of Materials: An Investigation of Hooke s Law Length of Lesson 1.5 hours Created By Justin Warren Subject Physics Grade Level 11-12 State Standards Physics: 1 c, d, f;

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

Chapter 3. Load and Stress Analysis

Chapter 3. Load and Stress Analysis Chapter 3 Load and Stress Analysis 2 Shear Force and Bending Moments in Beams Internal shear force V & bending moment M must ensure equilibrium Fig. 3 2 Sign Conventions for Bending and Shear Fig. 3 3

More information

Chapter 12. Static Equilibrium and Elasticity

Chapter 12. Static Equilibrium and Elasticity Chapter 12 Static Equilibrium and Elasticity Static Equilibrium Equilibrium implies that the object moves with both constant velocity and constant angular velocity relative to an observer in an inertial

More information

SHEAR TENSION COUPLING IN BIAXIAL BIAS EXTENSION TESTS

SHEAR TENSION COUPLING IN BIAXIAL BIAS EXTENSION TESTS SHER TENSION COUPLING IN IXIL IS EXTENSION TESTS P. Harrison *, P. Potluri Department of Mechanical Engineering, James Watt uilding (South), University of Glasgow, Glasgow G 8QQ, U.K. p.harrison@mech.gla.ac.uk

More information

TINIUS OLSEN Testing Machine Co., Inc.

TINIUS OLSEN Testing Machine Co., Inc. Interpretation of Stress-Strain Curves and Mechanical Properties of Materials Tinius Olsen has prepared this general introduction to the interpretation of stress-strain curves for the benefit of those

More information

Simulation of Geometrical Cross-Section for Practical Purposes

Simulation of Geometrical Cross-Section for Practical Purposes Simulation of Geometrical Cross-Section for Practical Purposes Bhasker R.S. 1, Prasad R. K. 2, Kumar V. 3, Prasad P. 4 123 Department of Mechanical Engineering, R.D. Engineering College, Ghaziabad, UP,

More information

Lecture 15 Strain and stress in beams

Lecture 15 Strain and stress in beams Spring, 2019 ME 323 Mechanics of Materials Lecture 15 Strain and stress in beams Reading assignment: 6.1 6.2 News: Instructor: Prof. Marcial Gonzalez Last modified: 1/6/19 9:42:38 PM Beam theory (@ ME

More information

PROBLEM #1.1 (4 + 4 points, no partial credit)

PROBLEM #1.1 (4 + 4 points, no partial credit) PROBLEM #1.1 ( + points, no partial credit A thermal switch consists of a copper bar which under elevation of temperature closes a gap and closes an electrical circuit. The copper bar possesses a length

More information

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3. ES230 STRENGTH OF MTERILS Exam 3 Study Guide Exam 3: Wednesday, March 8 th in-class Updated 3/3/17 Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on

More information

Stresses in Curved Beam

Stresses in Curved Beam Stresses in Curved Beam Consider a curved beam subjected to bending moment M b as shown in the figure. The distribution of stress in curved flexural member is determined by using the following assumptions:

More information

International Journal of Scientific & Engineering Research, Volume 5, Issue 1, January ISSN

International Journal of Scientific & Engineering Research, Volume 5, Issue 1, January ISSN International Journal of Scientific & Engineering Research, Volume 5, Issue 1, January-214 29 An Experimental Analysis of Stress Relaxation in Nonwoven Fabrics Sajid Ahmed Qureshi ABSTRACT - The current

More information

MECHANICAL PROPERTIES OF SOLIDS

MECHANICAL PROPERTIES OF SOLIDS Chapter Nine MECHANICAL PROPERTIES OF SOLIDS MCQ I 9.1 Modulus of rigidity of ideal liquids is (a) infinity. (b) zero. (c) unity. (d) some finite small non-zero constant value. 9. The maximum load a wire

More information

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR.

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR. LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR. IBIKUNLE ROTIMI ADEDAYO SIMPLE HARMONIC MOTION. Introduction Consider

More information

SECOND ENGINEER REG. III/2 APPLIED MECHANICS

SECOND ENGINEER REG. III/2 APPLIED MECHANICS SECOND ENGINEER REG. III/2 APPLIED MECHANICS LIST OF TOPICS Static s Friction Kinematics Dynamics Machines Strength of Materials Hydrostatics Hydrodynamics A STATICS 1 Solves problems involving forces

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

ELASTICITY (MDM 10203)

ELASTICITY (MDM 10203) ELASTICITY () Lecture Module 3: Fundamental Stress and Strain University Tun Hussein Onn Malaysia Normal Stress inconstant stress distribution σ= dp da P = da A dimensional Area of σ and A σ A 3 dimensional

More information

Chapter 8 BIAXIAL BENDING

Chapter 8 BIAXIAL BENDING Chapter 8 BAXAL BENDN 8.1 DEFNTON A cross section is subjected to biaial (oblique) bending if the normal (direct) stresses from section are reduced to two bending moments and. enerall oblique bending is

More information

Mechanical properties 1 Elastic behaviour of materials

Mechanical properties 1 Elastic behaviour of materials MME131: Lecture 13 Mechanical properties 1 Elastic behaviour of materials A. K. M. B. Rashid Professor, Department of MME BUET, Dhaka Today s Topics Deformation of material under the action of a mechanical

More information