PRBVDECE RNI AND'V'D TH THRA ACIATO RAT EQUTIO BY R. W. ARMSTRONG. S 5 Oad" (if 4dc~tRap 4e4ta'ie l/ce4 u I

Size: px
Start display at page:

Download "PRBVDECE RNI AND'V'D TH THRA ACIATO RAT EQUTIO BY R. W. ARMSTRONG. S 5 Oad" (if 4dc~tRap 4e4ta'ie l/ce4 u I"

Transcription

1 PRBVDECE RNI AND'V'D TH THRA ACIATO RAT EQUTIO BY R. W. ARMSTRONG (if 4dc~tRap 4e4ta'ie l/ce4 u I S 5 Oad"4 1966

2 Relation Between the Petch "Friction,' Stress and the Thermal Activation Rate Equation* R. W Armstrong A e? Brown Universit The following discussion is addressed towards establishing a connection between two alternative constitutive equations that have been used in the past to describe the temperature (and strain rate) dependence of the ield stress of iron. 1 Heslop and Petch proposed that the temperature dependence of the ield stress of iron was primaril determined b the intrinsic lattice resistance to crstal dislocation movement, i.e. the Peierls-Nabarro stress. Their experimental measurements for this "friction" stress, a were expressed in one form as a B exp (-T) (1) where T is the absolute temperature and B and 8 are experimental constants. It was pointed out that the strain rate has a large effect on a and this influence enters equation (1) implicitl through the parameter 82,3. However, for a fixed strain rate, (1) is relativel eas to evaluate and it ma be used as well to describe measurements obtained for other materials *This stud was supported at Brown Universit b the Advanced Research Projects Agenc and at the Solid State Division of the Oak Ridge National Laborator through a Research Participant Appointment b the Oak Ridge Associated Universities. I *W D Sov1 813

3 -2- Conrad6 has shown that the results from a considerable number of studies of the plastic ielding of iron and steel ma be expressed in the relationship # 2kT CoT +- 1.n (2) where 9 is the tensile strain rate, k is Boltzmann's constant, and Uo, V, and 9 are-parameters emploed in the thermal activation rate analsis. The parameters emploed in equation (2) have some direct theoretical basis, e.g. U is an activation energ associated with the rate controlling process involved in dislocation movement, V is the activation volume through which work is done and e is a product of several factors: a geometric factor (relating tensile strain rate and shear strain rate), the dislocation densit, the area swept out in dislocation movement between obstacles, and the vibrational frequenc of the dislocation line. Experiments have shown that V is itself a function of, at least, o, and this seems reasonable on the basis of dislocation theor. To relate the parameters emploed in (1) and (2), it ma first be noted that at T =, the value of B is directl obtained as B = V V (3) where V is the value of V at T =. For iron, U = 8.8 x 1-13 ergs, as given b Conrad 6, and B 1.8 x 1 dnes/cm 2, as determined from the data of Heslop and Petch Substitution of these values in (3) gives v L 9.6 x 1-2cm, and this value compares favorabl with the lowest value of V = 1.2 x 1-22cm3 estimated b Conrad.

4 -3- To evaluate 8, the right hand sides of (1) and (2) are equated and the terms rearranged in the form 1 io 2kT - I n [ + -VB In ](4) Now, based on the work of Conrad 6, tpical values, at T = 19 K and = -4 sec-1 for the additional parameters in (4), are V = 3.4 x 1-22 cm3 * 8-1 and e 5 x 1 sec". This value of T is selected as the median tempera- ture for the range (8-3 K) over which most measurements have been made and the value of V is also the median value obtained, b Conrad for this temperature range. Using the preceding estimates, it ma be seen that < 2kT so that 8 ma be expanded in series, taking into account, also 4 U > 2kT I 6 VB~ VBn - )I(6 to give k_ In In (- (7) e For lower or higher temperatures, or different strain rates, it occurs that the change in a% and, hence V is such that (7) should still hold ver well. Also because V increases as the temperature increases (because of the variation of at ), it appears that these changes ma largel counteract one another in (7) to give a constant vajef,lb"ai ALT),a813

5 -4- as indicated b the experimental basis for (1). This point is further examined below b comparison between the experimental value of taken from (1) and that derived from (7). The value of obtained from the experimental data of Heslop and Petch, at 6 = 1-4 sec ", is 1.43 x 12 OK -. Emploing the preceding values given for U and o the value of the second term on the right hand side of (7) is obtained b difference as I f n (---) = 9.7 x 1- OK (8) At 19 K, the value of (8) obtained directl from U, V and B is 6.5 x 1-3 OK-1. Since (8) should not var with temperature, then at fixed e, An ft ] 1 {n--) ft (2 I AT + -- AV (9) T VB T 2 VB TV From (9), the variation in (8) for the temperature interval (19-8)OK and (19-3) K is x 1-3,K-1. respectivel, using for the limiting temperatures the values of V = 2.1 x 1-22 and 4.6 x 1-22 cm3 taken from Conrad. In light of the varied experimental data and the estimates involved in all the quantities emploed, the variation given b (9) is considered to indicate that the second term on the right hand side of (7) ma be approximated b~a constant value, o. Taking = 6.5 x 1-3 K, then (7) gives a value of = 1.1 x 1-2 K-1, which compares favorabl with the value of 1.43 x 1 OK determined b Heslop and Petch. Thus (1) ma be finall rewritten k Sexp + U n ( ) T] (1) O

6 -5- Note that in a numerical evaluation of a the smaller value of B deter- mined from the thermal activation rate parameters would largel compensate for the smaller a value given above. In (1), therefore, the Petch "friction" stress has been expressed fairl directl in terms of the thermal activation rate analsis parameters. A definite connection between the equations (1) and (2) is established. In conclusion, some brief comments should perhaps be made concerning the usefulness of the foregoing analsis. It shows an explicit influence of the strain rate on the parameter 8, in agreement with the previous suggestion b Heslop and Petch 2 and Petch 3 that this parameter is strain rate dependent. The analsis offers a further indication of the relative self-consistenc of the large amount of data collected until the present time on this aspect of the deformation of iron, a view promote4 initiall b the work of Conrad6 References 1. J. Heslop and N, J. Petch, Phil. Mag. 1, 866 (1956). 2, J. Heslop and N. J. Petch, Phil. Mag. 3., 1128 (1958). 3. N, J. Petch, Fracture, Ed., B. L. Averbach, D. K. Felbeck, G. T. Hahn and D. A. Thomas, Technolog Press, Boston, 1959, p P. Feltham and G. J. Cople, Acta Met, 8, 542 (196). 5. R. W. Armstrong, Phil. Mag. 9., 163, (1964). 6. H. Conrad, J. Iron St. Inst. 198, 364, (1961).

Strain Transformation and Rosette Gage Theory

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

More information

Simulation of Nonlinear Behavior of Wall-Frame Structure during Earthquakes

Simulation of Nonlinear Behavior of Wall-Frame Structure during Earthquakes Simulation of Nonlinear Behavior of Wall-Frame Structure during Earthquakes b Masaomi Teshigawara 1, Hiroshi Fukuama 2, Hiroto Kato 2, Taiki Saito 2, Koichi Kusunoki 2, Tomohisa Mukai 2 ABSTRACT The reinforced

More information

A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS

A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS 1 A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS An ESIS Protocol Revised June 2007, Nov 2010 D R Moore, J G Williams

More information

CHAPTER 7 EARTHQUAKE RESPONSE OF INELASTIC SYSTEMS. Base shear force in a linearly elastic system due to ground excitation is Vb

CHAPTER 7 EARTHQUAKE RESPONSE OF INELASTIC SYSTEMS. Base shear force in a linearly elastic system due to ground excitation is Vb CHAPTER 7 EARTHQUAKE RESPONSE OF INELASTIC SYSTEMS Base shear force in a linearl elastic sstem due to ground excitation is Vb = ( A/ g) w where A is the pseudo-acceleration corresponding to natural period

More information

1.1 The Equations of Motion

1.1 The Equations of Motion 1.1 The Equations of Motion In Book I, balance of forces and moments acting on an component was enforced in order to ensure that the component was in equilibrium. Here, allowance is made for stresses which

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

STUDY ON CHARACTERIZATION OF NON LINEAR RESPONSE OF SDOF MODEL CONSIDERING LARGE DEFORMATION BY P-DELTA EFFECT

STUDY ON CHARACTERIZATION OF NON LINEAR RESPONSE OF SDOF MODEL CONSIDERING LARGE DEFORMATION BY P-DELTA EFFECT 13 th World Conference on Earthquake Engineering Vancouver, B.C., Canada August 1-6, 24 Paper No. 379 STUDY ON CARACTERIZATION OF NON LINEAR RESPONSE OF SDOF MODEL CONSIDERING LARGE DEFORMATION BY P-DELTA

More information

A Direct Derivation of the Griffith-Irwin Relationship using a Crack tip Unloading Stress Wave Model.

A Direct Derivation of the Griffith-Irwin Relationship using a Crack tip Unloading Stress Wave Model. A Direct Derivation of the Griffith-Irwin Relationship using a Crack tip Unloading Stress Wave Model. C.E. Neal-Sturgess. Emeritus Professor of Mechanical Engineering, The Universit of Birmingham, UK.

More information

MMJ1153 COMPUTATIONAL METHOD IN SOLID MECHANICS PRELIMINARIES TO FEM

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

More information

NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS OF PARAMETRIC APPROACH

NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS OF PARAMETRIC APPROACH Proceedings of Czech Japanese Seminar in Applied Mathematics August -7,, Czech Technical Universit in Prague http://geraldine.fjfi.cvut.cz pp. 1 13 NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS

More information

A NUMERICAL STUDY OF PILED RAFT FOUNDATIONS

A NUMERICAL STUDY OF PILED RAFT FOUNDATIONS Journal of the Chinese Institute of Engineers, Vol. 9, No. 6, pp. 191-197 (6) 191 Short Paper A NUMERICAL STUDY OF PILED RAFT FOUNDATIONS Der-Gue Lin and Zheng-Yi Feng* ABSTRACT This paper presents raft-pile-soil

More information

Scattering Properties of Gas Molecules on a Water Adsorbed Surface

Scattering Properties of Gas Molecules on a Water Adsorbed Surface Scattering Properties of Gas Molecules on a Water Adsorbed Surface Hideki Takeuchi a, Koji Yamamoto b, and Toru Hakutake c a Department of Mechanical Engineering, Kochi National College of Technolog, Nankoku

More information

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS Koung-Heog LEE 1, Subhash C GOEL 2 And Bozidar STOJADINOVIC 3 SUMMARY Full restrained beam-to-column connections in steel moment resisting frames have been

More information

N = N A Pb A Pb. = ln N Q v kt. = kt ln v N

N = N A Pb A Pb. = ln N Q v kt. = kt ln v N 5. Calculate the energy for vacancy formation in silver, given that the equilibrium number of vacancies at 800 C (1073 K) is 3.6 10 3 m 3. The atomic weight and density (at 800 C) for silver are, respectively,

More information

Module-4. Mechanical Properties of Metals

Module-4. Mechanical Properties of Metals Module-4 Mechanical Properties of Metals Contents ) Elastic deformation and Plastic deformation ) Interpretation of tensile stress-strain curves 3) Yielding under multi-axial stress, Yield criteria, Macroscopic

More information

LATERAL BUCKLING ANALYSIS OF ANGLED FRAMES WITH THIN-WALLED I-BEAMS

LATERAL BUCKLING ANALYSIS OF ANGLED FRAMES WITH THIN-WALLED I-BEAMS Journal of arine Science and J.-D. Technolog, Yau: ateral Vol. Buckling 17, No. Analsis 1, pp. 9-33 of Angled (009) Frames with Thin-Walled I-Beams 9 ATERA BUCKING ANAYSIS OF ANGED FRAES WITH THIN-WAED

More information

Chapter 6 2D Elements Plate Elements

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

More information

ME111 Instructor: Peter Pinsky Class #21 November 13, 2000

ME111 Instructor: Peter Pinsky Class #21 November 13, 2000 Toda s Topics ME Instructor: Peter Pinsk Class # November,. Consider two designs of a lug wrench for an automobile: (a) single ended, (b) double ended. The distance between points A and B is in. and the

More information

INTERFACE SHEAR TRANSFER FOR HIGH STRENGTH CONCRETE AND HIGH STRENGTH REINFORCEMENT

INTERFACE SHEAR TRANSFER FOR HIGH STRENGTH CONCRETE AND HIGH STRENGTH REINFORCEMENT INTERFACE SHEAR TRANSFER FOR HIGH STRENGTH CONCRETE AND HIGH STRENGTH REINFORCEMENT 641 Susumu KONO 1 And Hitoshi TANAKA SUMMARY The shear transfer at construction joints for members with high strength

More information

A SIMPLE ANALYTICAL MODEL OF LASER BENDING

A SIMPLE ANALYTICAL MODEL OF LASER BENDING 5 th International & 6 th All India Manufacturing Technolog Design and Research Conference (AIMTDR 04) December th 4 th 04 IIT Guwahati Assam India A SIMPLE ANALYTICAL MODEL OF LASER BENDING A. Eideh U.S.

More information

ON THE CHARACTERISTICS OF SOFT SOIL INELASTIC DESIGN RESPONSE SPECTRAS FOR THE CITY OF GUAYAQUIL, ECUADOR

ON THE CHARACTERISTICS OF SOFT SOIL INELASTIC DESIGN RESPONSE SPECTRAS FOR THE CITY OF GUAYAQUIL, ECUADOR ON THE CHAACTEISTICS OF SOFT SOIL INELASTIC DESIGN ESPONSE SPECTAS FO THE CITY OF GUAYAQUIL, ECUADO 837 Otton LAA 1 And moncao MACELO SUMMAY Five accelerograph records obtained in the cit of Guaaquil,

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

Progressive wave: a new multisource vibration technique to assist forming processes - kinematic study, simulation results and design proposition

Progressive wave: a new multisource vibration technique to assist forming processes - kinematic study, simulation results and design proposition Progressive wave: a new multisource vibration technique to assist forming processes - kinematic stud, simulation results and design proposition A. Khan a, T. H. Nguen a, C. Giraud-Audine a, G. Abba b,

More information

Analytical study of sandwich structures using Euler Bernoulli beam equation

Analytical study of sandwich structures using Euler Bernoulli beam equation Analtical stud of sandwich structures using Euler Bernoulli beam equation Hui Xue and H. Khawaja Citation: AIP Conference Proceedings 1798, 020076 (2017); doi: 10.1063/1.4972668 View online: http://dx.doi.org/10.1063/1.4972668

More information

Available online at ScienceDirect. Procedia Engineering 103 (2015 ) 52 59

Available online at   ScienceDirect. Procedia Engineering 103 (2015 ) 52 59 Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 103 (2015 ) 52 59 The 13 th Hpervelocit Impact Smposium Guided Impact Mitigation in 2D and 3D Granular Crstals Haden A. Burgone

More information

MODELING OF NONLINEAR BEHAVIOR OF RC SHEAR WALLS UNDER COMBINED AXIAL, SHEAR AND FLEXURAL LOADING

MODELING OF NONLINEAR BEHAVIOR OF RC SHEAR WALLS UNDER COMBINED AXIAL, SHEAR AND FLEXURAL LOADING CD02-003 MODELING OF NONLINEAR BEHAVIOR OF RC SHEAR WALLS UNDER COMBINED AXIAL, SHEAR AND FLEXURAL LOADING B. Ghiassi 1, M. Soltani 2, A. A. Tasnimi 3 1 M.Sc. Student, School of Engineering, Tarbiat Modares

More information

DESIGN OF BEAM-COLUMNS - II

DESIGN OF BEAM-COLUMNS - II DESIGN OF BEA-COLUNS-II 14 DESIGN OF BEA-COLUNS - II 1.0 INTRODUCTION Beam-columns are members subjected to combined bending and axial compression. Their behaviour under uniaxial bending, biaxial bending

More information

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

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

More information

SHEAR STRENGTH OF SOIL. Chapter 10: Sections Chapter 12: All sections except

SHEAR STRENGTH OF SOIL. Chapter 10: Sections Chapter 12: All sections except SHEAR STRENGTH OF SOIL Chapter 10: Sections 10. 10.3 Chapter 1: All sections ecept 1.13 1.14 1.15 1.17 1.18 TOPICS Introduction Components of Shear Strength of Soils Normal and Shear Stresses on a Plane

More information

Experimental Uncertainty Review. Abstract. References. Measurement Uncertainties and Uncertainty Propagation

Experimental Uncertainty Review. Abstract. References. Measurement Uncertainties and Uncertainty Propagation Experimental Uncertaint Review Abstract This is intended as a brief summar of the basic elements of uncertaint analsis, and a hand reference for laborator use. It provides some elementar "rules-of-thumb"

More information

7. TURBULENCE SPRING 2019

7. TURBULENCE SPRING 2019 7. TRBLENCE SPRING 2019 7.1 What is turbulence? 7.2 Momentum transfer in laminar and turbulent flow 7.3 Turbulence notation 7.4 Effect of turbulence on the mean flow 7.5 Turbulence generation and transport

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

Plastic Hinge Rotation Capacity of Reinforced Concrete Beams

Plastic Hinge Rotation Capacity of Reinforced Concrete Beams Plastic Hinge Rotation Capacit of Reinforced Concrete Beams Ali Kheroddin 1 and Hosein Naderpour 2 Downloaded from ijce.iust.ac.ir at 21:57 IRDT on Monda September 10th 2018 1 Associate Professor, Department

More information

CH. 1 FUNDAMENTAL PRINCIPLES OF MECHANICS

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

More information

THEME IS FIRST OCCURANCE OF YIELDING THE LIMIT?

THEME IS FIRST OCCURANCE OF YIELDING THE LIMIT? CIE309 : PLASTICITY THEME IS FIRST OCCURANCE OF YIELDING THE LIMIT? M M - N N + + σ = σ = + f f BENDING EXTENSION Ir J.W. Welleman page nr 0 kn Normal conditions during the life time WHAT HAPPENS DUE TO

More information

1 Differential Equations for Solid Mechanics

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

More information

Vibration Analysis of Isotropic and Orthotropic Plates with Mixed Boundary Conditions

Vibration Analysis of Isotropic and Orthotropic Plates with Mixed Boundary Conditions Tamkang Journal of Science and Engineering, Vol. 6, No. 4, pp. 7-6 (003) 7 Vibration Analsis of Isotropic and Orthotropic Plates with Mied Boundar Conditions Ming-Hung Hsu epartment of Electronic Engineering

More information

Torsion Stresses in Tubes and Rods

Torsion Stresses in Tubes and Rods Torsion Stresses in Tubes and Rods This initial analysis is valid only for a restricted range of problem for which the assumptions are: Rod is initially straight. Rod twists without bending. Material is

More information

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

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

More information

SPECULAR REFLECTION BY CONTACTING CRACK FACES. J.D. Achenbach and A.N. Norris. The Technological Institute Northwestern University Evanston, IL 60201

SPECULAR REFLECTION BY CONTACTING CRACK FACES. J.D. Achenbach and A.N. Norris. The Technological Institute Northwestern University Evanston, IL 60201 SPECULAR REFLECTION BY CONTACTING CRACK FACES J.D. Achenbach and A.N. Norris The Technological Institute Northwestern Universit Evanston, IL 60201 ABSTRACT Non-linear relations are postulated between the

More information

Exercise solutions: concepts from chapter 5

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

More information

Pacific Earthquake Engineering Research Center

Pacific Earthquake Engineering Research Center Pacific Earthquake Engineering Research Center Performance Models for Flexural Damage in Reinforced Concrete Columns Michael Berr and Marc Eberhard Department of Civil & Environmental Engineering Universit

More information

Study on Energy Dissipation Law in the Process of Coal and Gas Outburst

Study on Energy Dissipation Law in the Process of Coal and Gas Outburst 6th International Conference on lectronics, Mechanics, Culture and Medicine (MCM 05) Stud on nerg Dissipation Law in the Process of Coal and Gas Outburst Shugang Li,a, Ning Wang,b * and Tianjun Zhang,c

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

Lecture #2: Split Hopkinson Bar Systems

Lecture #2: Split Hopkinson Bar Systems Lecture #2: Split Hopkinson Bar Systems by Dirk Mohr ETH Zurich, Department of Mechanical and Process Engineering, Chair of Computational Modeling of Materials in Manufacturing 2015 1 1 1 Uniaxial Compression

More information

Linear Equation Theory - 2

Linear Equation Theory - 2 Algebra Module A46 Linear Equation Theor - Copright This publication The Northern Alberta Institute of Technolog 00. All Rights Reserved. LAST REVISED June., 009 Linear Equation Theor - Statement of Prerequisite

More information

Conceptual question Conceptual question 12.2

Conceptual question Conceptual question 12.2 Conceptual question 12.1 rigid cap of weight W t g r A thin-walled tank (having an inner radius of r and wall thickness t) constructed of a ductile material contains a gas with a pressure of p. A rigid

More information

Citation Key Engineering Materials, ,

Citation Key Engineering Materials, , NASITE: Nagasaki Universit's Ac Title Author(s) Interference Analsis between Crack Plate b Bod Force Method Ino, Takuichiro; Ueno, Shohei; Saim Citation Ke Engineering Materials, 577-578, Issue Date 2014

More information

LECTURE NOTES - VIII. Prof. Dr. Atıl BULU

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

More information

Cohesive Traction-Separation Laws for Tearing of Ductile Metal Plates

Cohesive Traction-Separation Laws for Tearing of Ductile Metal Plates Cohesive Traction-Separation Laws for Tearing of Ductile Metal Plates The Harvard communit has made this article openl available. Please share how this access benefits ou. Your stor matters. Citation Published

More information

EVALUATION OF FAILURE CRITERIA IN WOOD MEMBERS

EVALUATION OF FAILURE CRITERIA IN WOOD MEMBERS EVALUATION OF FAILURE CRITERIA IN WOOD MEMBERS José M. Cabrero 1, Kifle G. Gebremedhin ABSTRACT: Multi-aial stress conditions eist in almost all engineering applications, but design procedures, in most

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

Chapter 6: Mechanical Properties of Metals. Dr. Feras Fraige

Chapter 6: Mechanical Properties of Metals. Dr. Feras Fraige Chapter 6: Mechanical Properties of Metals Dr. Feras Fraige Stress and Strain Tension Compression Shear Torsion Elastic deformation Plastic Deformation Yield Strength Tensile Strength Ductility Toughness

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

Stiffness and Strength Tailoring in Uniform Space-Filling Truss Structures

Stiffness and Strength Tailoring in Uniform Space-Filling Truss Structures NASA Technical Paper 3210 April 1992 Stiffness and Strength Tailoring in Uniform Space-Filling Truss Structures Mark S. Lake Summar This paper presents a deterministic procedure for tailoring the continuum

More information

Design of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar

Design of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar 5.4 Beams As stated previousl, the effect of local buckling should invariabl be taken into account in thin walled members, using methods described alread. Laterall stable beams are beams, which do not

More information

Survey of Wave Types and Characteristics

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

More information

6.37 Determine the modulus of resilience for each of the following alloys:

6.37 Determine the modulus of resilience for each of the following alloys: 6.37 Determine the modulus of resilience for each of the following alloys: Yield Strength Material MPa psi Steel alloy 550 80,000 Brass alloy 350 50,750 Aluminum alloy 50 36,50 Titanium alloy 800 116,000

More information

Determination of Young s modulus of glass by Cornu s apparatus

Determination of Young s modulus of glass by Cornu s apparatus Determination of Young s modulus of glass b Cornu s apparatus Objective To determine Young s modulus and Poisson s ratio of a glass plate using Cornu s method. Theoretical Background Young s modulus, also

More information

APRIL Conquering the FE & PE exams Formulas, Examples & Applications. Topics covered in this month s column:

APRIL Conquering the FE & PE exams Formulas, Examples & Applications. Topics covered in this month s column: APRIL 2015 DR. Z s CORNER Conquering the FE & PE exams Formulas, Examples & Applications Topics covered in this month s column: PE Exam Specifications (Geotechnical) Transportation (Horizontal Curves)

More information

Bending Load & Calibration Module

Bending Load & Calibration Module Bending Load & Calibration Module Objectives After completing this module, students shall be able to: 1) Conduct laboratory work to validate beam bending stress equations. 2) Develop an understanding of

More information

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading MA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading MA 3702 Mechanics & Materials Science Zhe Cheng (2018) 2 Stress & Strain - Axial Loading Statics

More information

STRESSES AROUND UNDERGROUND OPENINGS CONTENTS

STRESSES AROUND UNDERGROUND OPENINGS CONTENTS STRESSES AROUND UNDERGROUND OPENINGS CONTENTS 6.1 Introduction 6. Stresses Around Underground Opening 6.3 Circular Hole in an Elasto-Plastic Infinite Medium Under Hdrostatic Loading 6.4 Plastic Behaviour

More information

Spherical Pressure Vessels

Spherical Pressure Vessels Spherical Pressure Vessels Pressure vessels are closed structures containing liquids or gases under essure. Examples include tanks, pipes, essurized cabins, etc. Shell structures : When essure vessels

More information

torsion equations for lateral BucKling ns trahair research report r964 July 2016 issn school of civil engineering

torsion equations for lateral BucKling ns trahair research report r964 July 2016 issn school of civil engineering TORSION EQUATIONS FOR ATERA BUCKING NS TRAHAIR RESEARCH REPORT R96 Jul 6 ISSN 8-78 SCHOO OF CIVI ENGINEERING SCHOO OF CIVI ENGINEERING TORSION EQUATIONS FOR ATERA BUCKING RESEARCH REPORT R96 NS TRAHAIR

More information

The science of elasticity

The science of elasticity The science of elasticity In 1676 Hooke realized that 1.Every kind of solid changes shape when a mechanical force acts on it. 2.It is this change of shape which enables the solid to supply the reaction

More information

a + s Nucleation of cracks in a brittle sheet Cristiano L. Dias, 1, * Jens Kröger, 2 Daniel Vernon, 2 and Martin Grant 2

a + s Nucleation of cracks in a brittle sheet Cristiano L. Dias, 1, * Jens Kröger, 2 Daniel Vernon, 2 and Martin Grant 2 PHYSICAL REVIEW E 8, 6619 29 Nucleation of cracks in a brittle sheet Cristiano L. Dias, 1, * Jens Kröger, 2 Daniel Vernon, 2 and Martin Grant 2 1 Department of Applied Mathematics, Middlesex College, The

More information

STRESS DISTRIBUTION AND FRACTURE CRITERION OF TAPERED WOOD BEAM

STRESS DISTRIBUTION AND FRACTURE CRITERION OF TAPERED WOOD BEAM STRESS DISTRIBUTION AND FRACTURE CRITERION OF TAPERED WOOD BEAM Hitoshi Kuwamura ABSTRACT: The stress distribution of a tapered beam was derived b the method of stress function in order to eliminate the

More information

CONTROLLING FACTORS BASIC ISSUES SAFETY IN OPENCAST MINING WITH SPECIAL REFERENCE TO SLOPE STABILITY

CONTROLLING FACTORS BASIC ISSUES SAFETY IN OPENCAST MINING WITH SPECIAL REFERENCE TO SLOPE STABILITY SAFETY IN OPENCAST MINING WITH SPECIAL REFERENCE TO SLOPE STABILITY CONTROLLING FACTORS Dr. J C. JHANWAR Sr. Principal Scientist CSIR-Central Institute of Mining & Fuel Research Regional Centre, Nagpur

More information

On Springback Prediction In Stamping Of AHSS BIW Components Utilizing Advanced Material Models

On Springback Prediction In Stamping Of AHSS BIW Components Utilizing Advanced Material Models On Springback Prediction In Stamping Of AHSS BIW Components Utilizing Advanced Material Models Ming F. Shi and Alex A. Konieczny United States Steel Corporation Introduction Origin of Springback AHSS Springback

More information

REVIEW FOR MT3 ANSWER KEY MATH 2373, SPRING 2015

REVIEW FOR MT3 ANSWER KEY MATH 2373, SPRING 2015 REVIEW FOR MT3 ANSWER KEY MATH 373 SPRING 15 PROF. YOICHIRO MORI This list of problems is not guaranteed to be an absolutel complete review. For completeness ou must also make sure that ou know how to

More information

Ceramic Processing Research

Ceramic Processing Research Journal of Ceramic Processing Research. Vol. 10, No. 2, pp. 195~201 (2009) J O U R N A L O F Ceramic Processing Research Computer simulation of a ceramics powder compaction process and optimization of

More information

Mechanics of Materials Primer

Mechanics of Materials Primer Mechanics of Materials rimer Notation: A = area (net = with holes, bearing = in contact, etc...) b = total width of material at a horizontal section d = diameter of a hole D = symbol for diameter E = modulus

More information

NCHRP FY 2004 Rotational Limits for Elastomeric Bearings. Final Report APPENDIX E. John F. Stanton Charles W. Roeder Peter Mackenzie-Helnwein

NCHRP FY 2004 Rotational Limits for Elastomeric Bearings. Final Report APPENDIX E. John F. Stanton Charles W. Roeder Peter Mackenzie-Helnwein NCHRP -68 FY 4 Rotational Limits for Elastomeric Bearings Final Report APPENDIX E John F. Stanton Charles W. Roeder Peter Mackenzie-Helnwein Department of Civil and Environmental Engineering Universit

More information

Figure 1: General Plane Motion (Translation and Rotation)

Figure 1: General Plane Motion (Translation and Rotation) STRIN ND TH TRNSFORMTION OF STRIN INTRODUCTION - DFORMBL BODY MOTION ) Rigid Bod Motion T T Translation Rotation Figure : General Plane Motion (Translation and Rotation) Figure shows the general plane

More information

A.R. Tusnin, M. Prokic. Behavior of symmetric steel I-sections under combined bending and torsion actions in inelastic range

A.R. Tusnin, M. Prokic. Behavior of symmetric steel I-sections under combined bending and torsion actions in inelastic range A.R. Tusnin, M. Prokic Behavior of smmetric steel Isections under combined bending and torsion actions in inelastic range In European codes and Russian standards for design of steel structures, calculation

More information

Lévy stable distribution and [0,2] power law dependence of. acoustic absorption on frequency

Lévy stable distribution and [0,2] power law dependence of. acoustic absorption on frequency Lév stable distribution and [,] power law dependence of acoustic absorption on frequenc W. Chen Institute of Applied Phsics and Computational Mathematics, P.O. Box 89, Division Box 6, Beijing 88, China

More information

3-D ANALYSIS OF FULLY FLIGHTED SCREWS OF CO-ROTATING TWIN SCREW EXTRUDER

3-D ANALYSIS OF FULLY FLIGHTED SCREWS OF CO-ROTATING TWIN SCREW EXTRUDER 3-D ANALYSIS OF FULLY FLIGHTED SCREWS OF CO-ROTATING TWIN SCREW EXTRUDER A. Lawal, S. Railkar, and D. M. Kalon Highl Filled Materials Institute Stevens Institute of Technolog Hoboken, NJ 73 Abstract A

More information

EART162: PLANETARY INTERIORS

EART162: PLANETARY INTERIORS EART162: PLANETARY INTERIORS Francis Nimmo Last Week Global gravity variations arise due to MoI difference (J 2 ) We can also determine C, the moment of inertia, either by observation (precession) or by

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

Least-Squares Independence Test

Least-Squares Independence Test IEICE Transactions on Information and Sstems, vol.e94-d, no.6, pp.333-336,. Least-Squares Independence Test Masashi Sugiama Toko Institute of Technolog, Japan PRESTO, Japan Science and Technolog Agenc,

More information

EVALUATION OF THERMAL TRANSPORT PROPERTIES USING A MICRO-CRACKING MODEL FOR WOVEN COMPOSITE LAMINATES

EVALUATION OF THERMAL TRANSPORT PROPERTIES USING A MICRO-CRACKING MODEL FOR WOVEN COMPOSITE LAMINATES EVALUATION OF THERMAL TRANSPORT PROPERTIES USING A MICRO-CRACKING MODEL FOR WOVEN COMPOSITE LAMINATES C. Luo and P. E. DesJardin* Department of Mechanical and Aerospace Engineering Universit at Buffalo,

More information

Modeling of Failure along Predefined Planes in Fractured Reservoirs

Modeling of Failure along Predefined Planes in Fractured Reservoirs PROCEEDINGS, Thirt-Ninth Workshop on Geothermal Reservoir Engineering Stanford Universit, Stanford, California, Februar 24-26, 2014 SGP-TR-202 Modeling of Failure along Predefined Planes in Fractured Reservoirs

More information

Effect of Bi-axial Residual Stresses on the Micro-Indentation Behaviour of Bulk Materials

Effect of Bi-axial Residual Stresses on the Micro-Indentation Behaviour of Bulk Materials Effect of Bi-axial Residual Stresses on the Micro-Indentation Behaviour of Bulk Materials Prakash Jadhav Department of Mechanical Engineering CMR Institute of Technolog, Bangalore, India Prakash.k@cmrit.ac.in

More information

The aircraft shown is being tested to determine how the forces due to lift would be distributed over the wing. This chapter deals with stresses and

The aircraft shown is being tested to determine how the forces due to lift would be distributed over the wing. This chapter deals with stresses and The aircraft shown is being tested to determine how the forces due to lift would be distributed over the wing. This chapter deals with stresses and strains in structures and machine components. 436 H P

More information

Chapter 1: Differential Form of Basic Equations

Chapter 1: Differential Form of Basic Equations MEG 74 Energ and Variational Methods in Mechanics I Brendan J. O Toole, Ph.D. Associate Professor of Mechanical Engineering Howard R. Hghes College of Engineering Universit of Nevada Las Vegas TBE B- (7)

More information

Solute friction and forest interaction

Solute friction and forest interaction Solute friction and forest interaction Ghiath Monnet, Benoit Devincre To cite this version: Ghiath Monnet, Benoit Devincre. Solute friction and forest interaction. Philosophical Magazine, Taylor & Francis,

More information

REVIEW FOR EXAM II. Dr. Ibrahim A. Assakkaf SPRING 2002

REVIEW FOR EXAM II. Dr. Ibrahim A. Assakkaf SPRING 2002 REVIEW FOR EXM II. J. Clark School of Engineering Department of Civil and Environmental Engineering b Dr. Ibrahim. ssakkaf SPRING 00 ENES 0 Mechanics of Materials Department of Civil and Environmental

More information

UNIVERSITY COLLEGE LONDON EXAMINATION FOR INTERNAL STUDENTS

UNIVERSITY COLLEGE LONDON EXAMINATION FOR INTERNAL STUDENTS UNIVERSITY COLLEGE LONDON University of London EXAMINATION FOR INTERNAL STUDENTS For the following qualifications.'- B. Sc. M. Sci. Physics 3C25: Solid State Physics COURSE CODE - PHYS3C25 UNIT VALUE 0.50

More information

Simple Analytical Expressions for the Magnetic Field of Current Coils

Simple Analytical Expressions for the Magnetic Field of Current Coils IEEE TRANSACTIONS ON MAGNETICS, VOL. 27, NO. I, JANUARY 1991 669 Simple Analtical Expressions for the Magnetic Field of Current Coils loan R. Ciric, Senior Member, IEEE Abstract-Current coils are decomposed

More information

Method of Least Work. Theory of Structures II M Shahid Mehmood Department of Civil Engineering Swedish College of Engineering & Technology, Wah Cantt

Method of Least Work. Theory of Structures II M Shahid Mehmood Department of Civil Engineering Swedish College of Engineering & Technology, Wah Cantt Method of east Work Theor of Structures II M Shahid Mehmood epartment of ivil Engineering Swedish ollege of Engineering & Technolog, Wah antt Method of east Work / astigliano s Second Theorem Staticall

More information

Rheology: What is it?

Rheology: What is it? Schedule Rheology basics Viscous, elastic and plastic Creep processes Flow laws Yielding mechanisms Deformation maps Yield strength envelopes Constraints on the rheology from the laboratory, geology, geophysics

More information

Abstract. 1 Introduction

Abstract. 1 Introduction Contact analysis for the modelling of anchors in concrete structures H. Walter*, L. Baillet** & M. Brunet* *Laboratoire de Mecanique des Solides **Laboratoire de Mecanique des Contacts-CNRS UMR 5514 Institut

More information

EP225 Note No. 4 Wave Motion

EP225 Note No. 4 Wave Motion EP5 Note No. 4 Wave Motion 4. Sinusoidal Waves, Wave Number Waves propagate in space in contrast to oscillations which are con ned in limited regions. In describing wave motion, spatial coordinates enter

More information

A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES

A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES G. Krismanic, N. Baumgartinger and H. Pfützner Institute of Fundamentals and Theor of Electrical Engineering Bioelectricit

More information

No. Parts Qty Description Weight (lb) Cost. 4 Wheels (E) 4 Hard Rubber Tread 4 in. dia. $38.40

No. Parts Qty Description Weight (lb) Cost. 4 Wheels (E) 4 Hard Rubber Tread 4 in. dia. $38.40 4 Bill Of Materials No. Parts Qt Description Weight (lb) Cost 1 Nose and back 1 0 x50 x0.16 sheet, 04-15.7 $41.75 plates (A & B) T361 Al. Axle Bracket 8 in. 04-T361 Al. Bar, 1 in. x 0.16 in. 0.7 $3.35

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

The refinement of a meteorological preprocessor for the urban environment. Ari Karppinen, Sylvain M. Joffre and Jaakko Kukkonen

The refinement of a meteorological preprocessor for the urban environment. Ari Karppinen, Sylvain M. Joffre and Jaakko Kukkonen Int. J. Environment and Pollution, Vol. 14, No. 1-6, 000 1 The refinement of a meteorological preprocessor for the urban environment Ari Karppinen, Slvain M. Joffre and Jaakko Kukkonen Finnish Meteorological

More information

Stability Analysis of a Geometrically Imperfect Structure using a Random Field Model

Stability Analysis of a Geometrically Imperfect Structure using a Random Field Model Stabilit Analsis of a Geometricall Imperfect Structure using a Random Field Model JAN VALEŠ, ZDENĚK KALA Department of Structural Mechanics Brno Universit of Technolog, Facult of Civil Engineering Veveří

More information

Study of Pile Interval of Landslide Restraint Piles by Centrifuge Test and FEM Analysis

Study of Pile Interval of Landslide Restraint Piles by Centrifuge Test and FEM Analysis Disaster Mitigation of Debris Flows, Slope Failures and Landslides 113 Study of Pile Interval of Landslide Restraint Piles by Centrifuge Test and FEM Analysis Yasuo Ishii, 1) Hisashi Tanaka, 1) Kazunori

More information