NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS OF PARAMETRIC APPROACH

Size: px
Start display at page:

Download "NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS OF PARAMETRIC APPROACH"

Transcription

1 Proceedings of Czech Japanese Seminar in Applied Mathematics August -7,, Czech Technical Universit in Prague pp NUMERICAL SIMULATION OF DISLOCATION DYNAMICS BY MEANS OF PARAMETRIC APPROACH VOJTĚCH MINÁRIK1, JAN KRATOCHVÍL, AND KAROL MIKULA 3 Abstract. The aim of this contribution is to present the current state of our research in the field of numerical simulation of dislocations moving in crstalline materials. The simulation is based on recent theor treating dislocation curves and dipolar loops interacting b means of forces of elastic nature and hindered b the lattice friction. The motion and interaction of one dislocation curve and one or more dipolar loops placed in 3D space is considered. Results of numerical eperiments made b parametrical approach to the problem (using flowing finite volume method) are presented and behaviour of the motion is described in detail. Ke words. FDM, flowing finite volume method, method of lines, parametric curves AMS subject classifications. 3K, U, 7M, 7S1 1. Introduction. Plastic deformation of crstalline solids is a result of the motion of dislocations. The theor of dislocations is described in number of tet books, e.g. [7]. Here we recall onl the basic mobile properties of dislocations and the nature of their mutual interactions. A dislocation is a line defect of the crstal lattice. Along the dislocation line the regular crstallographic arrangement of atoms is disturbed. The dislocation line is represented b a closed curve or a curve ending at the surface of the crstal. At low homologous temperatures the dislocations can move onl along crstallographic planes (the slip planes) with the highest densit of atoms. The motion results in mutual slipping of the neighbouring parts of the crstal along the slip planes. The slip displacement carried b a single dislocation, called Burgers vector, is equal to one of the vectors connecting the neighbouring atoms. The displacement field of atoms from their regular crstallographic positions around a dislocation line can be treated (ecept the close vicinit of the line) as elastic stress and strain fields. On the other hand, a stress field eerts a force on a dislocation. The combination of these two effects causes the elastic interaction among dislocations. There are two tpes of dislocations having much different characteristic length scales and mobile properties: dislocation curves and dipolar loops. Detailed description of these two tpes of dislocations can be found in [7] or [1]. The aim of this contribution is not to describe theor of dislocations; we would like to present results of our simulations and to comment them. Readers interested more in mathematical model and more details about the flowing finite volume method ma find information in [1]. 1 Department of Mathematics, Facult of Nuclear Sciences and Phsical Engineering, Czech Technical Universit in Prague, Trojanova 13, 1 Praha, Czech Republic. Department of Phsics, Facult of Civil Engineering, Czech Technical Universit in Prague, Thákurova 7, 1 9 Praha, Czech Republic. 3 Department of Mathematics and Descriptive Geometr, Slovak Universit of Technolog, Radlinského 11, 13 Bratislava, Slovakia. 1

2 Numerical simulation of dislocation dnamics 19. Dislocation curve and dipolar loop. We consider a plane dislocation segment with fied ends; the segment represented b a plane curve can bow in a slip plane which is identified with the z-plane of the coordinate sstem, i.e. =. If the dislocation segment approaches a loop, the curve can pass b or the curve and the loop start to move together or the curve is stopped b the loop [9]. F b F l F z h (a) Force interaction (b) DL geometr Fig..1. Dislocation dnamics problem geometr: (a) Dislocation curve and dipolar loop interaction; (b) Dipolar loop geometr As the loop is allowed to move along the direction parallel to its Burgers vector b onl (see Figure.1a) just the force component in that direction causes the loop motion. Additionall, the lattice friction acts against the motion. The detailed condition for the dislocation curve and the loop is specified in Section 3.3. The position of the loop is represented b 3 coordinates of its centre. There are two tpes of dipolar loops: a vacanc dipolar loop and an interstitial dipolar loop; each tpe has two stable configurations [1] with normals 1 [1, 1, ] and 1 [1, 1, ]. In vacanc loops a strip of atoms in regular crstallographic positions is missing. On the other hand; in interstitial loops an etra strip of atoms is added. For that reason the vacanc and interstitial loops produce different stress fields. The Burgers vectors of vacanc and interstitial loops have opposite directions. This fact we incorporate into our model b using negative value for the -ais component of the Burgers vector for interstitial loop. According to [1] dipolar loops are small rectangles denoted V 1, V, I 1, and I with longer sides parallel to the z-ais of the coordinate sstem. Average size of a dipolar loop is denoted b l and h. 3. Mathematical model Interaction of dislocation lines. The interaction force per unit length of dislocation line is given b the Peach-Koehler equation, which written for the i-th component reads (3.1) f i = ε ijk σ jm b m s k, where we denote: f i i-th component of the interaction force per unit length of the dislocation line ε ijk Levi-Civita smbol σ jm components of the stress field tensor at the dislocation position b m components of the Burgers vector components of unit tangential vector of the dislocation line s k 3.. Stress field of dipolar loop. Stress field produced b a dipolar loop is given b formula presented b Kroupa et al [1, 13, 1] and is ver comple, especiall

3 13 V. Minárik, J. Kratochvíl and K. Mikula in the closest neighbourhood of the dipolar loop. Under the assumptions that restrict the motion of dislocation curve and dipolar loops in some directions, and the fact the dipolar loop width h is ver small comparing to the other sizes, we can simplif the original Kroupa s formula b using Talor epansion and integration, and obtain an algebraic formula for the stress field of a dipolar loop: σ (,, z) = µhb { [ l z π(1 ν) ϱ [ l z (3.) + ϱ 3 + l + z ϱ 3 + where (3.3) + [ l z ϱ + l + z ϱ + + l + z ϱ + ] [ ±ν + ] [ ± ( + ) ( ± + + ] ( ( + ) 3 ) ] }, ] [ 3 ( ± ) + ϱ = + + (l z), ϱ + = + + (l + z), µ is shear modulus, ν is the Poisson ratio, and [,, z] is the position relative to the centre of dipolar loop. With the upper sign in (3.) we get the stress formula for the dipolar loops V 1 and I 1, while with the lower sign we get the formula for V and I dipolar loops. Readers more interested in the origin of (3.) can find detailed information in [1]. The compleit of the stress field is demonstrated in Figure Governing equations. The dnamics of the sstem of a dislocation curve and a dipolar loop is governed b a sstem of two equations describing their motion. The motion law for the dislocation curve Γ t can be parameterized b a smooth time dependent vector function X : I S R, i.e., at an time t it is given as the Image( X(., t)) = { X(u, t), u S} where S is a fied parameterization interval and I is a time interval. For a smooth curve X u > and for unit arc-length parameterization s, ds = X u du. Then X s and X s represent unit tangent and normal vectors, respectivel. Using the Frenet formulae, the evolution equation can be written in the form of intrinsic diffusion equation [, 1,, 11] )] (3.) B X t = ε X ss + F X s for the position vector X. Drag coefficient B and line tension ε are material constants and F represents eternal driving forces. If we denote b X (t, s) and X z (t, s) the components of the dislocation curve position vector in the z-plane, then X s = [Xs z, Xs ]. The equation (3.) is solved numericall to model complicated dislocation curve dnamics. The motion law of the dipolar loop can be easil obtained from (3.1) where all stress contributions of the whole dislocation curve should be included: (3.) F c = σ b curve n ds. Γ t The term F c is the -ais component of the total force acting on a dipolar loop, n = Xs z is the -ais component of the dislocation curve s normal vector. Incorporating lattice friction F depending on material, the equation governing the gliding of the dipolar loop is (3.) d(t) dt = 1 BP F,total(Γ t, (t)),

4 Numerical simulation of dislocation dnamics 131 where (t) is the -ais position of the dipolar loop, P = (l + h) is the perimeter of the dipolar loop, and F c F if F c > F (3.7) F,total (Γ t, (t)) = if F c < F F c + F if F c < F.. Numerical scheme. For discretization of the problem described earlier, we use the flowing finite volume method [11] in space and the method of lines [, 3, ] in time. Discrete solution is represented b a moving polgon given, at an time t, b plane points X i, i =,..., M. The values [ X and X M are prescribed in case of fied ends of the curve. The segments Xi 1, X ] i are called flowing finite volumes. [ We construct also dual volumes V i = Xi 1, ] [ X i Xi, X ] i+ 1, i = 1,.., M 1, where X i 1 = X i 1+ X i (see Fig..1). di di+1 X i 1 X i 1 X i X i+ 1 X i+1 Fig..1. Piecewise linear approimation of the dislocation curve. Integrating evolution equation (3.) in dual volume V i followed b some other straightforward steps described in [1] we get a sstem of ordinar differential equations: B d X ( i Xi+1 X = ε i X i ) X i 1 X + F i+1 X i 1 (.1) i, dt d i + d i+1 d i+1 d i d i + d i+1 i = 1,..., M 1, where d i denote distances between neighbouring nodes of the dislocation curve s discretization. In discretization of the governing equation (3.) for the dipolar loop we sum contributions of ever curve segment to obtain (.) M 1 F c = i= ( ) σ X i+ (t),, X z ( 1 i+ z b 1 curve X z i+1 Xi z ), where [(t),, z] is the centre of the dipolar loop at time t. Net, we use formula (3.7) applied to discrete F c defined above and get (.3) d dt = 1 BP F,total( X,..., X M, ). The complete discrete problem consists of (.1) and (.3) with accompaning initial and boundar conditions. The initial conditions simpl describe positions and shapes of the dislocation curve and dipolar loops at the beginning of the computation. As we consider a plane dislocation with fied ends to model a particular phsical process, the boundar condition prescribes positions of the endpoints of the dislocation curve. Thus, no tangential velocit is evaluated for the endpoints.

5 13 V. Minárik, J. Kratochvíl and K. Mikula. Eperimental results..1. Simulation 1 - standalone dislocation curve. In this simulation we present results we got for a standalone dislocation curve eerted to a periodic eternal stress. Starting with a straight dislocation line fied at ends, periodic eternal stress is applied to the sstem. The dislocation curve allowed to glide onl in the z-plane is either attracted or repelled in the z-ais direction. As positions of the curve end points are fied, initial straight line becomes curved as the time flows. We observe curvature of the curve (elastic stress of the dislocation) to partl eliminate the eternal stress, so the curve is not moving with the same speed everwhere. The bigger the curvature is, the slower is the response to the eternal stress. Of course, the motion also depends on dimensions of the dislocation curve and the eternal stress. For a longer curve it takes obviousl more time to achieve a higher curvature state (such as a semicircle) than for a shorter curve. Moreover, if the eternal stress is not high enough (will be precised later), the dislocation curve never transforms to a semicircle. When the eternal stress is switched off, the curvature pushes the dislocation curve back to its initial position, i.e. straight line. This is in agreement with the well-known minimal potential energ principle. To precise the phrase eternal stress is high enough, we should take line tension of the dislocation curve into account. Depending on the ratio of the line tension of the dislocation curve and the eternal stress, as well as the length of the time period of the eternal stress, we can get one of the following behaviours:.1.1. Behaviour 1 - equilibrium state prior reaching a semicircle shape. If the eternal stress is small comparing to the line tension of the dislocation curve, the motion stops after a certain time, and the dislocation curve will not reach a semicircle shape. It stops in a position where the eternal stress and the dislocation curve s line tension are in an equilibrium state. The rest of the time period, before the eternal stress is decreased or reversed, the dislocation remains in this equilibrium position, no matter how long the time period is (see Figure.1 (a) (d))..1.. Behaviour - time period of the eternal stress is too short. If the time period of the eternal stress is to short, the dislocation curve will not reach the equilibrium state prior the eternal stress is reversed. After reversing, dislocation curve starts to move backwards, i.e. in the opposite direction it was moving before reversing of the eternal stress Behaviour 3 - eternal stress is too large. When the eternal stress is too large and the time period long enough, the dislocation curve will create a socalled Frank-Read source. It blows up through the shape of a semicircle, grows and spreads in a much larger area than was occupied b the semicircle (see Figure.1 (e) (f))... Simulation - dislocation curve and one dipolar loop. The second simulation was computed for a single dipolar loop positioned at [,, z ], while the dislocation curve was again gliding in the z-plane ( = ). Note the dipolar loop was positioned in a different laer of the atomic lattice than the dislocation curve, i.e.. Two different settings for the eternal stress were used. In the first one a constant eternal stress was applied for the whole time of computation, while in the second a periodic eternal stress was applied. We confirmed several our epectations during the

6 Numerical simulation of dislocation dnamics 133 (a) T =. (c) T =. (e) Frank-Read source, T = (b) T = (d) T = (f) Frank-Read source, T = Fig..1. (a) (d) Reaching an equilibrium state: at T. = an equilibrium between the eternal stress and the line tension of the dislocation curve is reached and remains for the rest of the eternal stress period; (e) (f) Creation of Frank-Read source: In the case of large eternal stress the dislocation curve blows up and a new Frank-Read source is growing further in its neighbourhood simulations. The dnamics of the sstem is highl dependent on the mutual relative position of the dislocation curve and the dipolar loop, on the shape of dislocation curve, and, of course, on the stress applied. The dipolar loop produces its own stress field that interacts with the dislocation curve. Vice versa, the dislocation curve, as a line dislocation, produces a stress field which interacts with the dipolar loop. Both stress fields are of short-range tpe, and normall the dislocation curve and the dipolar loop do not interact as the are far enough from each other. However, as the dislocation curve moves according to the applied eternal stress, it can happen that the dislocation curve moves closer to the dipolar loop and the interaction between them gains more influence over the consequent motion of the sstem. Tpicall, the dislocation curve bows around the position of the dipolar loop, and is forcing to move the dipolar loop out of its place as in Figure.. (d) and.. On the other hand, the dipolar loop is restricted to move onl in the -ais direction, and there is also some amount of energ needed to eceed in order to start the motion at all. Force corresponding to this minimal energ is called friction force...1. Positional dependence. The most significant for the behaviour of the sstem is the relative position of the dipolar loop and the dislocation curve. One can sa there is a distance threshold behind which there is almost no interaction. This threshold depends on the direction in space because of the shape of the dipolar loop. For the -ais, if the dipolar loop is positioned in a laer too far from the laer (plane) of the dislocation curve, the interaction is negligible. However, for the other two aes the situation is different. Depending on the eternal stress and its size, as well as on the line tension of the dislocation curve, there are following possibilities:

7 13 V. Minárik, J. Kratochvíl and K. Mikula (a) _DL = 3 nm (b) _DL = nm (c) _DL = 1 nm (d) _DL = 1 nm Fig... Dependence on the distance of the dipolar loop laer. Several time levels of the simulation are shown for the dipolar loop positioned initiall at [, DL, ]. For the nearest case where DL = 1 nm the dipolar loop sweeps to the right The dislocation curve stops prior to reach the interaction region around the dipolar loop (like in Section.1.1). In this case the motion of the dislocation curve is not influenced b the presence of the dipolar loop in the sstem. The dislocation curve is not moving towards the dipolar loop. In this case again the motion of the dislocation curve is not influenced b the presence of the dipolar loop - under the additional assumption both dislocations were not interacting at the beginning of the simulation. The dislocation curve is moving (in its glide plane =, of course) towards the dipolar loop, and will interact with it at some time of evolution.... Dependence on the shape of the dislocation curve. The dipolar loop can glide out of the dislocation curve s interaction region onl if there is a clear wa. If, for eample, the dipolar loop is surrounded b two hills (see Figure. (a)) of the dislocation curve, and these two hills are further growing due to the stress applied, the dipolar loop cannot move through the energetic walls of the hills and resides between them. Consequentl, the dislocation curve s motion is locall hindered and the curve distorts around the dipolar loop (Figure.). Such a situation is not rare. Even for an initiall straight dislocation curve it can happen that the forced motion of the dipolar loop is not fast enough to leave the interaction region. It can be either due to the large friction force (most energ is consumed for overcoming friction, see Figure.3), or due to the strong eternal stress (simpl the dislocation curve is moving faster than the dipolar loop can react, see Figure. (b))...3. Dependence on the applied eternal stress. Consider the situation from one of the previous sections: the dislocation curve is moving towards the dipolar loop. The stronger the eternal stress is, the closer to can the dislocation curve

8 Numerical simulation of dislocation dnamics 13 (a) T =. (b) T =.3 (c) T = (d) T =. (e) T =. (f) T = Fig..3. Dependence on the friction force of the dipolar loop. Several time levels of the simulation are shown for the dipolar loop positioned initiall at [, 3, ]. The motion of the dipolar loop is hindered b a large friction Fig... The dnamics of the sstem depends on all parameters. The rightmost image uses times bigger dipolar loop than the middle one. The leftmost image uses. times bigger dipolar loop and times bigger shear modulus than the middle one. Dipolar loop fied at [,,.1] is not shown in the images approach the dipolar loop. The closer it can approach, the stronger the interaction is. Finall, the stronger is the interaction, the faster the dipolar loop is forced to sweep awa (Figure.). The achieved results seem to be close to the real phsical processes in materials. However, during the computations we observed that the dislocation curve bows so fast that the dipolar loops are unable to respond to it. This fact is not in agreement with real phsical eperiments []. We tried to remove this drawback from our model b adding an additional term of elastic relaation to the governing equation of the dislocation curve. It is a question of further investigations and simulations, how will this term work in the model.

9 13 V. Minárik, J. Kratochvíl and K. Mikula T =. T =. T = T = 1. T = 1. T = Fig... Dipolar loop swept b the curve; on the other hand, the curve is distorted b the stress field of the loop. In this test there were used: µ = GPa, ν =.33, B = 1 Pa s, b =.77 nm, l = 3 nm, h = nm, F = MPa m, applied stress σ a = 1.1 MPa. Initial position of dipolar loop was [,, 3]. The subsequent stages are shown for increasing time T Acknowledgements. The first author was partl supported b the NSF grant NSF-13 Award 113 and b the project Applied Mathematics in Technolog and Phsics MSM 771 of the Ministr of Education of the Czech Republic, the second author was partl supported b the project KONTAKT No. ME and Grant Agenc of the Czech Republic No. 1/3/, and the third author was partl supported b the grant VEGA 1/313/3. The conference participation was possible thanks to the Internal Grant of the Czech Technical Universit in Prague No REFERENCES [1] S.B. Angenent and M.E. Gurtin., Multiphase Thermomechanics with an Interfacial Structure. Evolution of an Isothermal Interface, Arch. Rat. Mech. Anal., 1 (199), pp [] M. Beneš., Diffuse-Interface Treatment of the Anisotropic Mean-Curvature Flow, Applications of Mathematics, Vol., No. (3), pp. 37-3, ISSN -79 [3] M. Beneš., Mathematical analsis of phase-field equations with numericall efficient coupling terms, Interfaces and Free Boundaries 3, (1), pp. 1 1, ISSN [] M. Beneš., Mathematical and Computational Aspects of Solidification of Crstallic Materials, Acta Mathematica Universitatis Comenianae, Volume 7 (1), No. 1, pp. 13 1, ISSN -9 [] G. Dziuk., Convergence of a Semi Discrete Scheme for the Curve Shortening Flow, Mathematical Models and Methods in Applied Sciences, (199), pp. 9 [] M. Gage and R.S. Hamilton., The Heat Equation Shrinking Conve Plane Curves, J. Diff. Geom., 3 (19), pp. 9 9 [7] J.P. Hirth and J. Lothe., Theor of Dislocations, John Wille (19)

10 Numerical simulation of dislocation dnamics 137 σ (,, ) σ (,, ) σ (,,.7*l) σ (,,.7*l) σ (,, l) σ (,, l) σ (,, 1.*l) σ (,, 1.*l) Fig... Compleit of the dipolar loop stress field. Graphs showing stress field at planes z =, z =.7l, z = l, and z = 1.l are presented.

11 13 V. Minárik, J. Kratochvíl and K. Mikula [] J. Huang, N.M. Ghoniem and J. Kratochvíl., On the sweeping mechanism of dipolar dislocation loops under fatigue conditions, Modelling and Simulation in Materials Science and Engineering, 1 (), pp [9] J. Kratochvíl, F. Kroupa and L.P. Kubin., The Sweeping of Dipolar Loops in Cclic Deformation: Kinetic Diagrams, Proceedings of the th Risoe Int. Smposium on Material Science: Deformation-Induced Microstructures: Analsis and Relation to Properties. Risoe National Laborator, Roskilde, Denmark (1999), pp [1] F. Kroupa., Long-Range Elastic Field of Semi-Infinite Dislocation Dipole and of Dislocation Jog, phs.stat.sol., Vol. 9 (19), pp. 7 3 [11] K. Mikula and D. Ševčovič., Evolution of Plane Curves Driven b a Nonlinear Function of Curvature and Anisotrop, SIAM J. Appl. Math., Vol. 1, No., pp [1] V. Minárik, J. Kratochvíl, K. Mikula and M. Beneš., Numerical Simulation of Dislocation Dnamics, Numerical Mathematics and Advanced Applications, ENUMATH (3), pp. 31 [13] Š. Verecký, J. Kratochvíl and F. Kroupa., The Stress Field of Rectangular Prismatic Dislocation Loops, Phs. Stat. Sol. (a), Vol. 191 (), pp. 1

Interactions of glide dislocations in a channel of a persistent slip band

Interactions of glide dislocations in a channel of a persistent slip band Interactions of glide dislocations in a channel of a persistent slip band JOSEF KŘIŠŤAN JAN KRATOCHVÍL Charles University, Faculty of Mathematics and Physics, Mathematical Institute, Sokolovská 83, 186

More information

Lecture on: 3D Dislocation Dynamics: Numerical Treatment

Lecture on: 3D Dislocation Dynamics: Numerical Treatment Tri-La Short Course on Dislocations in in Materials Pleasanton, CA June 8-0, 998 Lecture on: 3D Dislocation Dnamics: Numerical Treatment H.M. Zi, M. hee & J.P. Hirth School of Mechanical and Materials

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

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane 3.5 Plane Stress This section is concerned with a special two-dimensional state of stress called plane stress. It is important for two reasons: () it arises in real components (particularl in thin components

More information

ES.182A Topic 36 Notes Jeremy Orloff

ES.182A Topic 36 Notes Jeremy Orloff ES.82A Topic 36 Notes Jerem Orloff 36 Vector fields and line integrals in the plane 36. Vector analsis We now will begin our stud of the part of 8.2 called vector analsis. This is the stud of vector fields

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

Mathematica Bohemica

Mathematica Bohemica Mathematica Bohemica Miroslav Kolář; Michal Beneš; Daniel Ševčovič Computational studies of conserved mean-curvature flow Mathematica Bohemica, Vol. 39 (4), No. 4, 677--684 Persistent URL: http://dml.cz/dmlcz/4444

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

Moving Boundaries in Material Science

Moving Boundaries in Material Science Moving Boundaries in Material Science Michal Beneš Department of Mathematics Faculty of Nuclear Sciences and Physical Engineering Czech Technical University in Prague Mathematical Modelling Group Workshop

More information

PHYSICS PART II SECTION- I. Straight objective Type

PHYSICS PART II SECTION- I. Straight objective Type PHYSICS PAT II SECTION- I Straight objective Tpe This section contains 9 multiple choice questions numbered to 1. Each question has choices,, (C) and, out of which ONLY ONE is correct.. A parallel plate

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

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

Data Repository Hampel et al., page 1/5

Data Repository Hampel et al., page 1/5 GSA DATA REPOSITORY 2138 Data Repositor Hampel et al., page 1/5 SETUP OF THE FINITE-ELEMENT MODEL The finite-element models were created with the software ABAQUS and consist of a 1-km-thick lithosphere,

More information

UNIVERSITY OF SASKATCHEWAN ME MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 20, 2011 Professor A. Dolovich

UNIVERSITY OF SASKATCHEWAN ME MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 20, 2011 Professor A. Dolovich UNIVERSITY OF SASKATCHEWAN ME 313.3 MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 20, 2011 Professor A. Dolovich A CLOSED BOOK EXAMINATION TIME: 3 HOURS LAST NAME (printed): FIRST NAME (printed): STUDENT

More information

Space frames. b) R z φ z. R x. Figure 1 Sign convention: a) Displacements; b) Reactions

Space frames. b) R z φ z. R x. Figure 1 Sign convention: a) Displacements; b) Reactions Lecture notes: Structural Analsis II Space frames I. asic concepts. The design of a building is generall accomplished b considering the structure as an assemblage of planar frames, each of which is designed

More information

Simplified Fast Multipole Methods for Micromagnetic Modeling

Simplified Fast Multipole Methods for Micromagnetic Modeling implified Fast Multipole Methods for Micromagnetic Modeling D. M. Apalkov and P. B.Visscher Department of Phsics and Astronom and MIT Center The Universit of Alabama This project was supported b F grants

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

Module 1 : The equation of continuity. Lecture 4: Fourier s Law of Heat Conduction

Module 1 : The equation of continuity. Lecture 4: Fourier s Law of Heat Conduction 1 Module 1 : The equation of continuit Lecture 4: Fourier s Law of Heat Conduction NPTEL, IIT Kharagpur, Prof. Saikat Chakrabort, Department of Chemical Engineering Fourier s Law of Heat Conduction According

More information

= C. on q 1 to the left. Using Coulomb s law, on q 2 to the right, and the charge q 2 exerts a force F 2 on 1 ( )

= C. on q 1 to the left. Using Coulomb s law, on q 2 to the right, and the charge q 2 exerts a force F 2 on 1 ( ) Phsics Solutions to Chapter 5 5.. Model: Use the charge model. Solve: (a) In the process of charging b rubbing, electrons are removed from one material and transferred to the other because the are relativel

More information

Green s Theorem Jeremy Orloff

Green s Theorem Jeremy Orloff Green s Theorem Jerem Orloff Line integrals and Green s theorem. Vector Fields Vector notation. In 8.4 we will mostl use the notation (v) = (a, b) for vectors. The other common notation (v) = ai + bj runs

More information

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Chapter 8 KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Figure 8.1: 195 196 CHAPTER 8. KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS 8.1 Motivation In Chapter 3, the conservation of linear momentum for a

More information

Mechanics Departmental Exam Last updated November 2013

Mechanics Departmental Exam Last updated November 2013 Mechanics Departmental Eam Last updated November 213 1. Two satellites are moving about each other in circular orbits under the influence of their mutual gravitational attractions. The satellites have

More information

The Plane Stress Problem

The Plane Stress Problem . 4 The Plane Stress Problem 4 Chapter 4: THE PLANE STRESS PROBLEM 4 TABLE OF CONTENTS Page 4.. INTRODUCTION 4 3 4... Plate in Plane Stress............... 4 3 4... Mathematical Model.............. 4 4

More information

CH.7. PLANE LINEAR ELASTICITY. Multimedia Course on Continuum Mechanics

CH.7. PLANE LINEAR ELASTICITY. Multimedia Course on Continuum Mechanics CH.7. PLANE LINEAR ELASTICITY Multimedia Course on Continuum Mechanics Overview Plane Linear Elasticit Theor Plane Stress Simplifing Hpothesis Strain Field Constitutive Equation Displacement Field The

More information

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference Jul 8-23, 999, San Francisco, California FEDSM99-8 UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX

More information

Simultaneous Orthogonal Rotations Angle

Simultaneous Orthogonal Rotations Angle ELEKTROTEHNIŠKI VESTNIK 8(1-2): -11, 2011 ENGLISH EDITION Simultaneous Orthogonal Rotations Angle Sašo Tomažič 1, Sara Stančin 2 Facult of Electrical Engineering, Universit of Ljubljana 1 E-mail: saso.tomaic@fe.uni-lj.si

More information

Introduction to Differential Equations. National Chiao Tung University Chun-Jen Tsai 9/14/2011

Introduction to Differential Equations. National Chiao Tung University Chun-Jen Tsai 9/14/2011 Introduction to Differential Equations National Chiao Tung Universit Chun-Jen Tsai 9/14/011 Differential Equations Definition: An equation containing the derivatives of one or more dependent variables,

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

Aircraft Structures Structural & Loading Discontinuities

Aircraft Structures Structural & Loading Discontinuities Universit of Liège Aerospace & Mechanical Engineering Aircraft Structures Structural & Loading Discontinuities Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/

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

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

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

Pan Pearl River Delta Physics Olympiad 2005

Pan Pearl River Delta Physics Olympiad 2005 1 Jan. 29, 25 Morning Session (9 am 12 pm) Q1 (5 Two identical worms of length L are ling on a smooth and horizontal surface. The mass of the worms is evenl distributed along their bod length. The starting

More information

4 Strain true strain engineering strain plane strain strain transformation formulae

4 Strain true strain engineering strain plane strain strain transformation formulae 4 Strain The concept of strain is introduced in this Chapter. The approimation to the true strain of the engineering strain is discussed. The practical case of two dimensional plane strain is discussed,

More information

MAE4700/5700 Finite Element Analysis for Mechanical and Aerospace Design

MAE4700/5700 Finite Element Analysis for Mechanical and Aerospace Design MAE4700/5700 Finite Element Analsis for Mechanical and Aerospace Design Cornell Universit, Fall 2009 Nicholas Zabaras Materials Process Design and Control Laborator Sible School of Mechanical and Aerospace

More information

Flow and Transport. c(s, t)s ds,

Flow and Transport. c(s, t)s ds, Flow and Transport 1. The Transport Equation We shall describe the transport of a dissolved chemical by water that is traveling with uniform velocity ν through a long thin tube G with uniform cross section

More information

MECHANICS OF SOLIDS - BEAMS TUTORIAL 1 STRESSES IN BEAMS DUE TO BENDING

MECHANICS OF SOLIDS - BEAMS TUTORIAL 1 STRESSES IN BEAMS DUE TO BENDING MCHANICS OF SOLIDS - BAMS TUTOIAL 1 STSSS IN BAMS DU TO BNDING This tutorial covers elements of the following sllabi. o Part of dexcel HNC Mechanical Principles UNIT 21722P outcome2. o Parts of the ngineering

More information

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

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates 5.3.3 The general solution for plane waves incident on a laered halfspace The general solution to the elmhol equation in rectangular coordinates The vector propagation constant Vector relationships between

More information

Fluid Mechanics II. Newton s second law applied to a control volume

Fluid Mechanics II. Newton s second law applied to a control volume Fluid Mechanics II Stead flow momentum equation Newton s second law applied to a control volume Fluids, either in a static or dnamic motion state, impose forces on immersed bodies and confining boundaries.

More information

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are: Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements

More information

2.2 SEPARABLE VARIABLES

2.2 SEPARABLE VARIABLES 44 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 6 Consider the autonomous DE 6 Use our ideas from Problem 5 to find intervals on the -ais for which solution curves are concave up and intervals for which

More information

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted.

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted. 4.1 Strain If an object is placed on a table and then the table is moved, each material particle moves in space. The particles undergo a displacement. The particles have moved in space as a rigid bod.

More information

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

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 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 Relation Between the Petch "Friction,' Stress and the Thermal Activation Rate Equation*

More information

Multiple Integration

Multiple Integration Contents 7 Multiple Integration 7. Introduction to Surface Integrals 7. Multiple Integrals over Non-rectangular Regions 7. Volume Integrals 4 7.4 Changing Coordinates 66 Learning outcomes In this Workbook

More information

LESSON #12 - FORMS OF A LINE COMMON CORE ALGEBRA II

LESSON #12 - FORMS OF A LINE COMMON CORE ALGEBRA II LESSON # - FORMS OF A LINE COMMON CORE ALGEBRA II Linear functions come in a variet of forms. The two shown below have been introduced in Common Core Algebra I and Common Core Geometr. TWO COMMON FORMS

More information

Functions of Several Variables

Functions of Several Variables Chapter 1 Functions of Several Variables 1.1 Introduction A real valued function of n variables is a function f : R, where the domain is a subset of R n. So: for each ( 1,,..., n ) in, the value of f is

More information

ENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force]

ENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force] ENGI 44 Advanced Calculus for Engineering Facult of Engineering and Applied Science Problem Set Solutions [Multiple Integration; Lines of Force]. Evaluate D da over the triangular region D that is bounded

More information

Towards Higher-Order Schemes for Compressible Flow

Towards Higher-Order Schemes for Compressible Flow WDS'6 Proceedings of Contributed Papers, Part I, 5 4, 6. ISBN 8-867-84- MATFYZPRESS Towards Higher-Order Schemes for Compressible Flow K. Findejs Charles Universit, Facult of Mathematics and Phsics, Prague,

More information

Two-sided Mullins-Sekerka flow does not preserve convexity

Two-sided Mullins-Sekerka flow does not preserve convexity Differential Equations and Computational Simulations III J. Graef, R. Shivaji, B. Soni, & J. Zhu (Editors) Electronic Journal of Differential Equations, Conference 01, 1997, pp. 171 179. ISSN: 1072-6691.

More information

Finite elements for plates and shells. Advanced Design for Mechanical System LEC 2008/11/04

Finite elements for plates and shells. Advanced Design for Mechanical System LEC 2008/11/04 Finite elements for plates and shells Sstem LEC 008/11/04 1 Plates and shells A Midplane The mid-surface of a plate is plane, a curved geometr make it a shell The thickness is constant. Ma be isotropic,

More information

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element Avaiable online at www.banglaol.info angladesh J. Sci. Ind. Res. (), 77-86, 008 ANGLADESH JOURNAL OF SCIENTIFIC AND INDUSTRIAL RESEARCH CSIR E-mail: bsir07gmail.com Abstract Applications of Gauss-Radau

More information

Stress-strain relations

Stress-strain relations SICLLY INDRMIN SRSS SYSMS staticall determinate stress sstem simple eample of this is a bar loaded b a weight, hanging in tension. he solution for the stress is simpl W/ where is the cross sectional area.

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

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

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

More information

Mathematical aspects of mechanical systems eigentones

Mathematical aspects of mechanical systems eigentones Seminar: Vibrations and Structure-Borne Sound in Civil Engineering Theor and Applications Mathematical aspects of mechanical sstems eigentones Andre Kuzmin April st 6 Abstract Computational methods of

More information

SEPARABLE EQUATIONS 2.2

SEPARABLE EQUATIONS 2.2 46 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 4. Chemical Reactions When certain kinds of chemicals are combined, the rate at which the new compound is formed is modeled b the autonomous differential equation

More information

RESEARCH ON PIEZOELECTRIC QUARTZ UNDER MULTIDIMENSIONAL FORCES

RESEARCH ON PIEZOELECTRIC QUARTZ UNDER MULTIDIMENSIONAL FORCES aterials Phsics and echanics (015) 94-100 eceived: October 31, 014 ESEACH ON PIEZOELECTIC QUATZ UNDE ULTIDIENSIONAL OCES ei Wang *, uji Wang, Zongjin en, Zhenuan Jia, Liqi Zhao, Dong Li Ke Laborator for

More information

4452 Mathematical Modeling Lecture 13: Chaos and Fractals

4452 Mathematical Modeling Lecture 13: Chaos and Fractals Math Modeling Lecture 13: Chaos and Fractals Page 1 442 Mathematical Modeling Lecture 13: Chaos and Fractals Introduction In our tetbook, the discussion on chaos and fractals covers less than 2 pages.

More information

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x 5A galler of graphs Objectives To recognise the rules of a number of common algebraic relations: = = = (rectangular hperbola) + = (circle). To be able to sketch the graphs of these relations. To be able

More information

Consideration of Shock Waves in Airbag Deployment Simulations

Consideration of Shock Waves in Airbag Deployment Simulations Consideration of Shock Waves in Airbag Deploment Simulations Doris Rieger BMW Group ABSTRACT When the inflation process of a simple flat airbag was simulated with the MADYMO gas flow module, the resulting

More information

Numerical Analysis of Heat Transfer in the Unsteady Flow of a non- Newtonian Fluid over a Rotating cylinder

Numerical Analysis of Heat Transfer in the Unsteady Flow of a non- Newtonian Fluid over a Rotating cylinder Bulletin of Environment, Pharmacolog and Life Sciences Bull. Env.Pharmacol. Life Sci., Vol 4 [Spl issue 1] 215: 318-323 214 Academ for Environment and Life Sciences, India Online ISSN 2277-188 Journal

More information

1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM

1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM 1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM 23 How does this wave-particle dualit require us to alter our thinking about the electron? In our everda lives, we re accustomed to a deterministic world.

More information

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 4 Pure Bending

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 4 Pure Bending EA 3702 echanics & aterials Science (echanics of aterials) Chapter 4 Pure Bending Pure Bending Ch 2 Aial Loading & Parallel Loading: uniform normal stress and shearing stress distribution Ch 3 Torsion:

More information

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve:

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve: .2 INITIAL-VALUE PROBLEMS 3.2 INITIAL-VALUE PROBLEMS REVIEW MATERIAL Normal form of a DE Solution of a DE Famil of solutions INTRODUCTION We are often interested in problems in which we seek a solution

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

3 Stress internal forces stress stress components Stress analysis stress transformation equations principal stresses stress invariants

3 Stress internal forces stress stress components Stress analysis stress transformation equations principal stresses stress invariants 3 Stress orces acting at the surfaces of components were considered in the previous chapter. The task now is to eamine forces arising inside materials, internal forces. Internal forces are described using

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

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

Stability Analysis of Laminated Composite Thin-Walled Beam Structures

Stability Analysis of Laminated Composite Thin-Walled Beam Structures Paper 224 Civil-Comp Press, 2012 Proceedings of the Eleventh International Conference on Computational Structures echnolog, B.H.V. opping, (Editor), Civil-Comp Press, Stirlingshire, Scotland Stabilit nalsis

More information

Simulation and Experimental Validation of Chaotic Behavior of Airflow in a Ventilated Room

Simulation and Experimental Validation of Chaotic Behavior of Airflow in a Ventilated Room Simulation and Eperimental Validation of Chaotic Behavior of Airflow in a Ventilated Room Jos van Schijndel, Assistant Professor Eindhoven Universit of Technolog, Netherlands KEYWORDS: Airflow, chaos,

More information

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA)

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA) LETURE Third Edition BEMS: SHER ND MOMENT DGRMS (FORMUL). J. lark School of Engineering Department of ivil and Environmental Engineering 1 hapter 5.1 5. b Dr. brahim. ssakkaf SPRNG 00 ENES 0 Mechanics

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

Research Article Chaos and Control of Game Model Based on Heterogeneous Expectations in Electric Power Triopoly

Research Article Chaos and Control of Game Model Based on Heterogeneous Expectations in Electric Power Triopoly Discrete Dnamics in Nature and Societ Volume 29, Article ID 469564, 8 pages doi:.55/29/469564 Research Article Chaos and Control of Game Model Based on Heterogeneous Epectations in Electric Power Triopol

More information

Symmetry Arguments and the Role They Play in Using Gauss Law

Symmetry Arguments and the Role They Play in Using Gauss Law Smmetr Arguments and the Role The la in Using Gauss Law K. M. Westerberg (9/2005) Smmetr plas a ver important role in science in general, and phsics in particular. Arguments based on smmetr can often simplif

More information

DEVELOPING A MICRO-SCALE MODEL OF SOIL FREEZING

DEVELOPING A MICRO-SCALE MODEL OF SOIL FREEZING Proceedings of ALGORITMY 2016 pp. 234 243 DEVELOPING A MICRO-SCALE MODEL OF SOIL FREEZING A. ŽÁK, M. BENEŠ, AND T.H. ILLANGASEKARE Abstract. In this contribution, we analyze thermal and mechanical effects

More information

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY 4. Newton s Method 99 4. Newton s Method HISTORICAL BIOGRAPHY Niels Henrik Abel (18 189) One of the basic problems of mathematics is solving equations. Using the quadratic root formula, we know how to

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

LESSON #11 - FORMS OF A LINE COMMON CORE ALGEBRA II

LESSON #11 - FORMS OF A LINE COMMON CORE ALGEBRA II LESSON # - FORMS OF A LINE COMMON CORE ALGEBRA II Linear functions come in a variet of forms. The two shown below have been introduced in Common Core Algebra I and Common Core Geometr. TWO COMMON FORMS

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

Chapter 3: Three faces of the derivative. Overview

Chapter 3: Three faces of the derivative. Overview Overview We alread saw an algebraic wa of thinking about a derivative. Geometric: zooming into a line Analtic: continuit and rational functions Computational: approimations with computers 3. The geometric

More information

Second-Order Linear Differential Equations C 2

Second-Order Linear Differential Equations C 2 C8 APPENDIX C Additional Topics in Differential Equations APPENDIX C. Second-Order Homogeneous Linear Equations Second-Order Linear Differential Equations Higher-Order Linear Differential Equations Application

More information

Equilibrium at a Point

Equilibrium at a Point Equilibrium at a Point Never slap a man who's chewing tobacco. - Will Rogers Objec3ves Understand the concept of sta3c equilibrium Understand the use of the free- bod diagram to isolate a sstem for analsis

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

Analysis of Effects of Rebounds and Aerodynamics for Trajectory of Table Tennis Ball

Analysis of Effects of Rebounds and Aerodynamics for Trajectory of Table Tennis Ball SICE Annual Conference 21 August 18-21, 21, The Grand Hotel, Taipei, Taiwan Analsis of Effects of Reounds and Aerodnamics for Trajector of Tale Tennis Junko Nonomura Mechanical Science and Engineering,

More information

Initial Value Problems for. Ordinary Differential Equations

Initial Value Problems for. Ordinary Differential Equations Initial Value Problems for Ordinar Differential Equations INTRODUCTION Equations which are composed of an unnown function and its derivatives are called differential equations. It becomes an initial value

More information

AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES *

AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES * Journal of Computational Mathematics, Vol.27, No.2-3, 29, 388 399. AN EFFICIENT MOVING MESH METHOD FOR A MODEL OF TURBULENT FLOW IN CIRCULAR TUBES * Yin Yang Hunan Ke Laborator for Computation and Simulation

More information

The Control-Volume Finite-Difference Approximation to the Diffusion Equation

The Control-Volume Finite-Difference Approximation to the Diffusion Equation The Control-Volume Finite-Difference Approimation to the Diffusion Equation ME 448/548 Notes Gerald Recktenwald Portland State Universit Department of Mechanical Engineering gerr@mepdedu ME 448/548: D

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

8. BOOLEAN ALGEBRAS x x

8. BOOLEAN ALGEBRAS x x 8. BOOLEAN ALGEBRAS 8.1. Definition of a Boolean Algebra There are man sstems of interest to computing scientists that have a common underling structure. It makes sense to describe such a mathematical

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

RANGE CONTROL MPC APPROACH FOR TWO-DIMENSIONAL SYSTEM 1

RANGE CONTROL MPC APPROACH FOR TWO-DIMENSIONAL SYSTEM 1 RANGE CONTROL MPC APPROACH FOR TWO-DIMENSIONAL SYSTEM Jirka Roubal Vladimír Havlena Department of Control Engineering, Facult of Electrical Engineering, Czech Technical Universit in Prague Karlovo náměstí

More information

Methods of Solving Ordinary Differential Equations (Online)

Methods of Solving Ordinary Differential Equations (Online) 7in 0in Felder c0_online.te V3 - Januar, 05 0:5 A.M. Page CHAPTER 0 Methods of Solving Ordinar Differential Equations (Online) 0.3 Phase Portraits Just as a slope field (Section.4) gives us a wa to visualize

More information

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin. THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water

More information

BASE VECTORS FOR SOLVING OF PARTIAL DIFFERENTIAL EQUATIONS

BASE VECTORS FOR SOLVING OF PARTIAL DIFFERENTIAL EQUATIONS BASE VECTORS FOR SOLVING OF PARTIAL DIFFERENTIAL EQUATIONS J. Roubal, V. Havlena Department of Control Engineering, Facult of Electrical Engineering, Czech Technical Universit in Prague Abstract The distributed

More information

Bending Analysis of Isotropic Rectangular Plate with All Edges Clamped: Variational Symbolic Solution

Bending Analysis of Isotropic Rectangular Plate with All Edges Clamped: Variational Symbolic Solution Journal of Emerging Trends in Engineering and pplied Sciences (JETES) (5): 86-85 Scholarlink Research Institute Journals, 0 (ISSN: -706) jeteas.scholarlinkresearch.org Journal of Emerging Trends in Engineering

More information

Einstein s Lorentz Transformation is a Mathematical Game

Einstein s Lorentz Transformation is a Mathematical Game No. Einstein s Lorentz Transformation is a Mathematical Game Zeng Qingping Air Force Radar Academ ( th Department) Room 8-A-, No.88, Huangpu Street, Wuhan, Hubei, China [Abstract]: This paper indicates

More information

TABLES, GRAPHS, AND RULES

TABLES, GRAPHS, AND RULES TABLES, GRAPHS, AND RULES 3.1.1 3.1.7 Three was to write relationships for data are tables, words (descriptions), and rules. The pattern in tables between input () and output () values usuall establishes

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

ME 7502 Lecture 2 Effective Properties of Particulate and Unidirectional Composites

ME 7502 Lecture 2 Effective Properties of Particulate and Unidirectional Composites ME 75 Lecture Effective Properties of Particulate and Unidirectional Composites Concepts from Elasticit Theor Statistical Homogeneit, Representative Volume Element, Composite Material Effective Stress-

More information