Code_Aster. A finite element of cable-pulley
|
|
- Bertha Cannon
- 6 years ago
- Views:
Transcription
1 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 1/14 A finite element of cable-pulley Summary : The pulleys play an important role in the structures of cables such as the air electric lines. It is thus useful to know to model them in one at the same time realistic and powerful way. One presents the finite element formulation of a length of cable passing by a pulley: expressions of the internal forces and the matrix of rigidity. The pulley can be fixed or supported by a flexible structure. Its position on the cable with balance is not known a priori: this position is that for which on both sides the tension of the cable is the same one.
2 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 2/14 Contents 1 Notations Introduction Assumptions and definition of a finite element of cable - pulley Internal forces of a finite element of cable-pulley Matrix of rigidity Matrix of mass Introduction of the element of cable-pulley into Code_Aster Example of application Conclusion Bibliography Description of the versions of the document...11 Annexe 1 Calculation of the matrix of rigidity...12 Annexe 2 Figure of balance of an inextensible cable weighing subjected to a tension given in the end... 13
3 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 3/14 1 Notations A E F surface of the cross-section of the cable. Young modulus. vector of the internal forces of the element. F n force interns with the node n. H horizontal component of the tension [ An1]. I 3 matrix unit of order 3. K l l 0 l i matrix of rigidity of the element. current length of the element. length at rest. initial length. N 3 N 1 euclidian norm of l 2 N 3 N 2 l 2 euclidian norm of l 2. N N i S s T T i u u n w x n current tension of the cable constituting the element. initial tension (prevoltage). arrow of a range of cable [ An1]. length of a range [ An1]. current temperature. initial temperature. vector-displacement of the nodes compared to the initial position. displacement of the node n compared to its initial position. weight per unit of length. vector-position of the node n in initial configuration. thermal dilation coefficient. current deformation compared to the initial configuration.
4 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 4/14 2 Introduction One uses pulleys, during the construction of the air electric lines, for the operation of installation of the cables. The cable in the course of installation [Figure 2-a] is fixed at the one of the supports of stop of the canton, it rests on pulleys placed at the bottom of the insulators of the supports of alignment and it is retained by a force on the level of the second support of stop. While exploiting this force - or by moving its point of application - one adjusts the arrow of the one of the ranges, that which is subjected to constraints of environment. Then one removes the pulleys and one fixes the cable at the insulators. The length of the cable in the various ranges is then fixed and it determines the later behavior of the line under statical stresses (wind, overload of white frost) and in dynamic mode (movement due to the forces of Laplace created by the currents of short-circuit). Figure 2-a: Pose of a cable in a canton with two ranges The finite element of cable-pulley presented here makes it possible to model the operation of installation and thus to calculate, in a natural way, the length of cable in the various ranges. The idea of this finite element came to us some time after the conversation [bib1] and we presented his formulation in [bib2].
5 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 5/14 3 Assumptions and definition of a finite element of cable - pulley N 3 N 1 N 2 Figure 3-a: Length of cable passing by a pulley - reality Let us take a length of cable N 1 N 2 passing by the pulley N 3 [Figure 3-a]. This pulley is not inevitably fixed and can, for example and as it is the case in the example of [ 8], being assembled at the end of a cable. N 3 N 1 N2 Figure 3-b: Length of cable passing by a pulley - modelled The pulley is supposed to be specific [Figure 3-b]. One makes moreover following assumptions: The position of balance of N 3 is not known, but it is necessarily on the section N 1 N 2 deformed starting from its initial position. In modeling of the lines, the horizontal movements are of low amplitude and this assumption is generally not restrictive; Two bits N 3 N 1 and N 3 N 2 are always rectilinear, like elements of cable of the 1 er order.
6 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 6/14 It rises from this assumption that: =x 1 u 1 x 3 u 3 éq 3-1 l 2 =x 2 u 2 x 3 u 3 = T éq 3-2 l 2 = l 2 T l 2 The overall length of the two bits is: in the current location, where the temperature is T : l= l 2 ; in the initial position, indicated by the index i, where the tension is N i and the temperature T i : l i = i l 2 i ; in a not forced position, indicated by index 0, where the temperature is T 0 : l 0 = 0 l 2 0. The pulley is without friction and thus the tension is the same one in the two bits. It rises from this assumption that the deformation is also the same one and one takes for value of this one the measurement of the relative lengthening of the section compared to the initial state: = l l i l 0 éq 3-3 must remain small, so that the section A is regarded as constant. It will be noted that, within the framework of the finite element method, the linear loads do not prevent the tension from being constant of N 1 with N 2. These forces are indeed concentrated with the nodes N 1 and N 2 and onaxis pulley N 3. The relation of behavior is elastic: N =EA [ e α T T i ] N i éq 3-4 One calls finite element of cable-pulley, a length of cable the preceding assumptions. N 1 N 2 N 3 satisfying
7 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 7/14 4 Internal forces of a finite element of cable-pulley Let us point out the following definition: one calls internal forces of a finite element of structure the forces which it is necessary to exert in its nodes to maintain it in its current deformed configuration. In the case of a finite element of cable-pulley, the internal forces result immediately from statics. One has indeed [Figure 4-a]: F 1 = N éq 4-1 F 2 = N l 2 l 2 and, to ensure balance: F 3 = F 1 F 2. F 1 and F 2 having even module, F 3 is directed according to the bisectrix of the angle N 1 N 3 N 2. F 3 F 1 F 2 N 3 N 1 N 2 F 1 F 1 F 2 Figure 4-a: Internal forces of an element of cable-pulley F 2 F 3 is applied toaxis pulley. The system F internal forces of the element is thus: 1 F={F F 3} 2. F
8 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 8/14 5 Matrix of rigidity The matrix of rigidity K element is derived from Fréchet of F in the direction of displacement u nodes: F=K u. K is calculated by the following classical formula, used intensively in [bib3], [bib4] and [bib5]: F=lim 0 F u u. éq 5-1 K 11 K=[ N I l 3 K 12 K 11 K 12 N I 1 l 3 1 ] T K 12 K 22 N I l 3 K 22 K T 12 N I 2 l 3 2 K 11 K T 12 N I l 3 K 22 K 12 N I 1 l 3 K 11 K 22 K 12 K T l 2 N I 3 éq 5-2 The detail of calculations is given in [ An1] and the final expression of K is the following one: N is given by [éq 3-4] and [éq 3-3]; K 11 = EA N l 0 K 12 = EA l l 0 l T 2 ; 2 K 22 = EA l 0 N l 2 1 l l l T ; 1 1 l l l T K is symmetrical, because of the symmetry of K 11 and of K 22 and of total symmetry per blocks. But K depends on displacements on N 1,N 2 et N 3 via, l 2 et N : the finite element of cablepulley is thus an element nonlinear.
9 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 9/14 6 Matrix of mass This matrix intervenes obviously only in the dynamic problems. The element of cable - pulley is not used in Code_Aster that for the quasi-static problems of installation of cables [ 7]. Note: One presents nevertheless in [bib2] the example of a dynamic problem comprising a cable-pulley. The matrix of mass of the element N 1 N 2 N 3 is obtained by assembling the coherent matrices of mass of the elements of cable with two nodes N 3 N 1 and N 3 N 2 [bib6] and by adding the specific mass of the pulley. It should be noted that, during a dynamic analysis, this matrix of mass must be updated because the lengths and l 2 vary. 7 Introduction of the element of cable-pulley into Code_Aster The element of cable-pulley is supported by a mesh SEG3. In the order AFFE_MODELE, under the keyword factor AFFE, one must define the arguments of the keywords as follows: keyword GROUP_MA PHENOMENON MODELING argument group of meshs MECHANICAL CABLE_POULIE of cable-pulley The constitutive material must be elastic. In the order AFFE_CARA_ELEM, the cable-pulleys are treated like cables. As the element of cable-pulley is nonlinear [ 5] and that, for the moment, it is used only in statics [ 6], it is accessible only by the operator STAT_NON_LINE. Under the keyword factor BEHAVIOR, the arguments of the keywords are the following: keyword GROUP_MA RELATION DEFORMATION argument group of meshs ELAS GROT_GDEP of cable-pulley Lastly, the force of gravity acting on the nodes N 1 et N 2 of an element of cable-pulley [fig 3 - B] is following because it depends on the length of the bits N 3 N 1 et N 3 N 2. For a structure comprising at least an element of cable-pulley, one must specify this load (following) in STAT_NON_LINE under the keyword factor EXCIT. One finds an example of application in test SSNL100A [V ]. Note: The element of cable-pulley does not make it possible to take into account deformation due to the temperature.
10 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 10/14 8 Example of application This example is that of the installation of a cable with two ranges and imposed tension of adjustment. On [Figure 7-a], O is the anchoring of the cable on the support of stop of left. P 1 is a first pulley placed at the bottom of the lifting chain P 1 C, fixed in C with the support of alignment. P 2 is one second pulley placed on the support of stop of right-hand side. O, P 1 and P 2 are, to simplify, located on horizontal. z O x Q 1 R 1 Q 2 P 2 R2 N p P 1 Q 1 ' C R 1 ' Q 2 ' R 2 ' Figure 7-a: Balance of a cable with two ranges, subjected to a tension of adjustment given. OP 1 = P 1 P 2 =100 m ; w=30 N /m ; E A=5 x10 7 N ; N p =5 000 N In initial position, the cable at rest, supposed in weightlessness, is right: line in feature of axis of [Figure 7-a]. For modeling in finite elements, this line is cut out in: ten elements of cable with two nodes enters O and Q 1 ; an element of cable-pulley Q 1 R 1 P 1 ; nine elements of cable enters R 1 and Q 2 ; an element of cable-pulley Q 2 R 2 P 2. One simultaneously subjects the cable to gravity and the tension of adjustment N p exerted in R 2. The position of balance (line in feature full with [Figure 7-a]) is reached into 11 iterations by the operator STAT_NON_LINE of Code_Aster. The arrows are of m and m, respectively in the range of left and that of right-hand side. For a cable inextensible of a range of 100 m, linear weight 30 N /m and subjected to a tension in the end of N, the theoretical arrow is of m [ An2]. While exploiting the tension of adjustment, one can adjust one of the two arrows to a value fixed in advance.
11 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 11/14 9 Conclusion The finite element of cable-pulley presented in this note, of a very simple mechanical formulation, has performances comparable to those of an element of ordinary cable. It is very convenient and even essential for a realistic modeling of the air electric lines. It should find other applications, in particular in Robotics. 10 Bibliography 1) J.L. LILIEN : Private communication. 2) Mr. AUFAURE : With finite element of cable passing through has pulley. Computers & Structures 46, (1993). 3) J.C. SIMO, L. CONSIDERING-QUOC : With three-dimensional finite-strain rod model. Share II: computational aspects. Comput. Meth. appl. Mech. Engng 58, (1986). 4) A.CARDONA, Mr. GERADIN : With beam finite element nonlinear theory with finite rotations. Int. J. Numer. Meth. Engng. 26, (1988). 5) A. CARDONA : Year integrated approach to mechanism analysis. Thesis, University of Liege, Belgium (1989). 6) Mr. AUFAURE : Modeling of the cables in Code_Aster, in the course of drafting. 7) H. MAX IRVINE : Cable Structures. MIT Close (1981). 11 Description of the versions of the document Author (S) Aster Organization (S) 3 MR. AUFAURE (EDF/IMA/MMN) 10,1 J.M.PROIX (EDF- R&D/AMA) Description of the modifications Initial text Modification of GREEN in GROT_GDEP
12 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 12/14 Annexe 1Calculation of the matrix of rigidity One shows here how applies the formula [éq 5-1] to the calculation of the first three lines of the matrix K [éq 5-2], those which are relating to the force F 1. The other lines are obtained either by permutation of the indices, or by summation of two preceding lines. The first lines are thus obtained by calculating the derivative: lim e 0 d de F 1 u ed u éq An1-1 and by putting in factor the vector u. According to the relations [éq 4-1], [éq 3-4] and [éq 3-3], one a: ={ F 1 u u EA [ u d u l 2 u u l i ] i} T T l i N u u 0 u u with, according to [éq 3-1]: and, according to [éq 3-2]: Consequently: u u =x 1 u 1 u 1 x 3 u 3 u 3 lim 0 u u = T u u u u. lim 0 and by permutation of indices 1 and 2: Finally: lim 0 lim 0 d d u u = u 1 u 3 d d u u = 1 l T u 1 u u 1 u 3 d d l 2 u u = 1 l 2 u l T 2 u u 2 u 3 d d u u = 1 3 u l T 1 u u 1 u 3 While carrying the preceding expressions in [éq An1-1] and by putting in factor the vector u, one easily obtains the first three lines of K.
13 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 13/14 Annexe 2Figure of balance of an inextensible cable weighing subjected to a tension given in the end Let us take a cable [An2-a Figure] whose end is fixed at the point O and of which the other end P is subjected to the tension N p. O and P are on same horizontal and distant ones of s. The linear weight is w. The arrow is sought S. z O (0, 0) x S P s, 0 N p An2-a figure: Heavy cable in balance One finds in [bib7], p 6, the following well-known formulas: figure of balance of the cable: z x = H w [ cosh w H s 2 x ws cosh 2H ] ; éq An2-1 tension: N x = H cosh w H s 2 x. éq An2-2 H is the horizontal, constant tension along the cable since the external force distributed - the weight - is vertical. H is calculated by [éq An2-2] written in P : cosh ws 2H 2N p ws ws 2H =0. ws 2H is thus root of the transcendent equation: cosh X = 2N p ws X.
14 Titre : Un élément fini de câble-poulie Date : 09/12/2013 Page : 14/14 This equation has two roots [An2-b Figure] if: with: and: 2N p ws p 0, p 0 =sinh x 0 x 0 =cotanh x 0 x 0 0. cosh X 1 2 N p w s w s 2 H X An2-b figure: Calculation of ws 2H The smallest root, which corresponds to the greatest tension of the cable, is only useful. The other root corresponds to a sag of the considerable cable, of about size of its range. ws 2H being calculated, the arrow results from [éq An2-1]: S= s 2 2H ws ws cosh 2H 1.
Code_Aster. Reaction of the steel subjected to corrosion
Titre : Comportement de l acier soumis à la corrosion Date : 16/0/01 Page : 1/1 Reaction of the steel subjected to corrosion Summarized: This documentation the model presents steel reaction of subjected
More informationSDLV121 - Wave planes shearing in an elastic column
Titre : SDLV121 - Onde plane de cisaillement dans une colo[...] Date : 08/11/2013 Page : 1/8 SDLV121 - Wave planes shearing in an elastic column Summary One tests the application of a loading in transient
More informationLaw of behavior very-rubber band: almost incompressible material
Titre : Loi de comportement hyperélastique : matériau pres[...] Date : 25/09/2013 Page : 1/9 Law of behavior very-rubber band: almost incompressible material Summary: One describes here the formulation
More informationSSNV137 - Cable of prestressed in a Summarized concrete straight beam
Titre : SSNV137 - Câble de précontrainte dans une poutre d[...] Date : 23/10/2012 Page : 1/10 SSNV137 - Cable of prestressed in a Summarized concrete straight beam One considers a concrete straight beam,
More informationSSNP110 - Crack of edge in a rectangular plate finished in elastoplasticity
Titre : SSNP110 - Fissure de bord dans une plaque rectangu[...] Date : 21/07/2017 Page : 1/14 SSNP110 - Crack of edge in a rectangular plate finished in elastoplasticity Summary: This test is a CAS-test
More informationCode_Aster. HSNV120 - Tension hyper elastic of a bar under thermal loading
Titre : HSNV - Traction hperélastique d'un barreau sou[...] Date : 4/8/ Page : / HSNV - Tension hper elastic of a bar under thermal loading Abstract: This quasi-static thermomechanical test consists in
More informationSSNL141 - P multifibre and multimatériaux goatskin bottles
Titre : SSNL141 - Poutres multifibres et multimatériaux Date : 17/07/2014 Page : 1/7 SSNL141 - P multifibre and multimatériaux goatskin bottles Summary: The objective this test is to validate the use of
More informationZZZZ120 - Calculation of an assembly pin-attaches
Titre : ZZZZ120 - Calcul d un assemblage goujon-bride Date : 01/08/2011 Page : 1/16 ZZZZ120 - Calculation of an assembly pin-attaches Summary: The purpose of these two tests are to validate the two macro-orders
More informationCode_Aster. HSNV129 - Test of compression-dilation for study of the coupling thermics-cracking
Titre : HSNV129 - Essai de compression-dilatation pour étu[...] Date : 28/2/218 Page : 1/8 HSNV129 - Test of compression-dilation for study of the coupling thermics-cracking Summary: One applies to an
More informationSSNA109 - Tensile test with the model VISC_CIN2_CHAB
Titre : SSNA109 Essai de traction avec le modèle VISC_CI[...] Date : 03/08/2011 Page : 1/6 SSNA109 - Tensile test with the model VISC_CIN2_CHAB Summary: This test of nonlinear quasi-static mechanics makes
More informationCode_Aster. Law of behavior BETON_REGLE_PR
Titre : Loi de comportement BETON_REGLE_PR Date : 21/07/2017 Page : 1/5 Law of behavior BETON_REGLE_PR Summary: This documentation presents the law BETON_REGLE_PR established by the company Sixense-NECS
More informationSSNL141 beams multifibre and multimatériaux
Titre : SSNL141 - poutres multifibres et multimatériaux Date : 04/04/2013 Page : 1/7 SSNL141 beams multifibre and multimatériaux Abstract: The purpose of this test is to validate the use of multimatériaux
More informationGyroscopic matrixes of the straight beams and the discs
Titre : Matrice gyroscopique des poutres droites et des di[...] Date : 29/05/2013 Page : 1/12 Gyroscopic matrixes of the straight beams and the discs Summarized: This document presents the formulation
More informationSSNV221 Hydrostatic test with a behavior DRUCK_PRAGER linear and parabolic
Titre : SSNV221 - Essai hydrostatique avec un comportement[...] Date : 08/08/2011 Page : 1/10 SSNV221 Hydrostatic test with a behavior DRUCK_PRAGER linear and parabolic Summary: The case test proposes
More informationVirtual distortions applied to structural modelling and sensitivity analysis. Damage identification testing example
AMAS Workshop on Smart Materials and Structures SMART 03 (pp.313 324) Jadwisin, September 2-5, 2003 Virtual distortions applied to structural modelling and sensitivity analysis. Damage identification testing
More informationHPLP300 - Plate with Young modulus function of the temperature
Titre : HPLP300 - Plaque aec module d Young fonction de l[...] Date : 04/08/2011 Page : 1/6 HPLP300 - Plate with Young modulus function of the temperature Summarized: This thermoelastic test makes it possible
More informationSSNS106 Damage of a reinforced concrete plate under requests varied with model GLRC_DM
Titre : SSNS106 - Endommagement d une plaque plane sous so[...] Date : 01/03/2013 Page : 1/67 SSNS106 Damage of a reinforced concrete plate under requests varied with model GLRC_DM Summarized: This test
More informationCode_Aster. SHLL100 - Harmonic response of a bar per dynamic substructuring
Titre : SHLL100 - Réponse harmonique d'une barre par sous-[...] Date : 03/08/2011 Page : 1/5 SHLL100 - Harmonic response of a bar per dynamic substructuring Abstract: The scope of application of this test
More informationEquilibrium & Elasticity
PHYS 101 Previous Exam Problems CHAPTER 12 Equilibrium & Elasticity Static equilibrium Elasticity 1. A uniform steel bar of length 3.0 m and weight 20 N rests on two supports (A and B) at its ends. A block
More informationCode_Aster. SDLV123 - Computation of G elastodynamic in infinite medium for a plane crack finite length
Titre : SDLV123 - Calcul de G élastodynamique en milieu i[...] Date : 27/05/2013 Page : 1/7 SDLV123 - Computation of G elastodynamic in infinite medium for a plane crack finite length Summarized It acts
More informationComputational non-linear structural dynamics and energy-momentum integration schemes
icccbe 2010 Nottingham University Press Proceedings of the International Conference on Computing in Civil and Building Engineering W Tizani (Editor) Computational non-linear structural dynamics and energy-momentum
More informationFLEXIBILITY METHOD FOR INDETERMINATE FRAMES
UNIT - I FLEXIBILITY METHOD FOR INDETERMINATE FRAMES 1. What is meant by indeterminate structures? Structures that do not satisfy the conditions of equilibrium are called indeterminate structure. These
More informationStress analysis of a stepped bar
Stress analysis of a stepped bar Problem Find the stresses induced in the axially loaded stepped bar shown in Figure. The bar has cross-sectional areas of A ) and A ) over the lengths l ) and l ), respectively.
More informationThe centroid of an area is defined as the point at which (12-2) The distance from the centroid of a given area to a specified axis may be found by
Unit 12 Centroids Page 12-1 The centroid of an area is defined as the point at which (12-2) The distance from the centroid of a given area to a specified axis may be found by (12-5) For the area shown
More informationReduction of model in linear and non-linear dynamics: Method of RITZ
Titre : Réduction de modèle en dynamique linéaire et non-l[...] Date : 7/05/206 Page : /6 Reduction of model in linear and non-linear dynamics: Method of RITZ Summary: This document presents the principle
More informationDynamics of assembled structures of rotor systems of aviation gas turbine engines of type two-rotor
Dynamics of assembled structures of rotor systems of aviation gas turbine engines of type two-rotor Anatoly А. Pykhalov 1, Mikhail А. Dudaev 2, Mikhail Ye. Kolotnikov 3, Paul V. Makarov 4 1 Irkutsk State
More informationCode_Aster. SDNV114 Simulation of benchmark SAFE - T5 veil out of reinforced concrete
Titre : SDNV114 Simulation du benchmark SAFE - voile T5 [...] Date : 03/05/2016 Page : 1/11 SDNV114 Simulation of benchmark SAFE - T5 veil out of reinforced concrete Summary: This test represents a simplified
More informationChapter 12. Static Equilibrium and Elasticity
Chapter 12 Static Equilibrium and Elasticity Static Equilibrium Equilibrium implies that the object moves with both constant velocity and constant angular velocity relative to an observer in an inertial
More informationFinite Element Nonlinear Analysis for Catenary Structure Considering Elastic Deformation
Copyright 21 Tech Science Press CMES, vol.63, no.1, pp.29-45, 21 Finite Element Nonlinear Analysis for Catenary Structure Considering Elastic Deformation B.W. Kim 1, H.G. Sung 1, S.Y. Hong 1 and H.J. Jung
More informationRealization of a study civil engineer with cables of prestressing
Titre : Réalisation d'une étude génie civil avec câbles de[...] Date : 11/07/2012 Page : 1/13 Realization of a study civil engineer with cables of prestressing Summarized: The purpose of this document
More informationCode_Aster. Operator PROJ_MESU_MODAL. 1 Goal
Titre : Opérateur PROJ_MESU_MODAL Date : 27/07/2015 Page : 1/10 Operator PROJ_MESU_MODAL 1 Goal To extrapolate experimental measurements on a digital model in dynamics. The experimental data can be displacements,
More informationImplicit integration and clarifies nonlinear relations of behaviors
Titre : Intégration implicite et explicite des relations d[...] Date : 25/09/2013 Page : 1/14 Implicit integration and clarifies nonlinear relations of behaviors Summary This document describes two methods
More informationMITOCW MITRES2_002S10nonlinear_lec15_300k-mp4
MITOCW MITRES2_002S10nonlinear_lec15_300k-mp4 The following content is provided under a Creative Commons license. Your support will help MIT OpenCourseWare continue to offer high quality educational resources
More informationLarge Thermal Deflections of a Simple Supported Beam with Temperature-Dependent Physical Properties
Large Thermal Deflections of a Simple Supported Beam with Temperature-Dependent Physical Properties DR. ŞEREF DOĞUŞCAN AKBAŞ Civil Engineer, Şehit Muhtar Mah. Öğüt Sok. No:2/37, 34435 Beyoğlu- Istanbul,
More informationCode_Aster. Calculation algorithm of the densities of reinforcement
Titre : Algorithme de calcul des densités de ferraillage Date : 05/08/2013 Page : 1/11 Calculation algorithm of the densities of reinforcement Summary: One presents the calculation algorithm of the densities
More information2/28/2006 Statics ( F.Robilliard) 1
2/28/2006 Statics (.Robilliard) 1 Extended Bodies: In our discussion so far, we have considered essentially only point masses, under the action of forces. We now broaden our considerations to extended
More informationExam 3 PREP Chapters 6, 7, 8
PHY241 - General Physics I Dr. Carlson, Fall 2013 Prep Exam 3 PREP Chapters 6, 7, 8 Name TRUE/FALSE. Write 'T' if the statement is true and 'F' if the statement is false. 1) Astronauts in orbiting satellites
More informationNUMERICAL SIMULATION OF STEEL CATENARY RISER
SIMMEC/EMMCOMP 214 XI Simpósio de Mecânica Computacional II Encontro Mineiro de Modelagem Computacional Juiz De Fora, MG, 28-3 de Maio De 214 NUMERICAL SIMULATION OF STEEL CATENARY RISER Marcus V. S. Casagrande
More informationStatics. Phys101 Lectures 19,20. Key points: The Conditions for static equilibrium Solving statics problems Stress and strain. Ref: 9-1,2,3,4,5.
Phys101 Lectures 19,20 Statics Key points: The Conditions for static equilibrium Solving statics problems Stress and strain Ref: 9-1,2,3,4,5. Page 1 The Conditions for Static Equilibrium An object in static
More informationSDNV114 Simulation of benchmark SAFE - T5 veil
Titre : SDNV114 - Simulation du benchmark SAFE - voile T5 Date : 30/07/2014 Page : 1/9 SDNV114 Simulation of benchmark SAFE - T5 veil Summary: This test represents a simplified modeling of a study SAFE
More informationBack Analysis of Measured Displacements of Tunnels
Rock Mechanics and Rock Engineering 16, 173--180 (1983) Rock Mechanics and Rock Engineering 9 by Springer-Verlag 1983 Back Analysis of Measured Displacements of Tunnels By S. Sakurai and K. Takeuchi Kobe
More informationLoad, Stress and Strain Chapter 30
Load, Stress and Strain Chapter 30 Dr. BassamTayeh Engineering Technical English Islamic University of Gaza April, 2017 A. Load When engineers design a machine or structure, they need to know what forces
More informationNUMERICAL INVESTIGATION OF CABLE PARAMETRIC VIBRATIONS
11 th International Conference on Vibration Problems Z. Dimitrovová et al. (eds.) Lisbon, Portugal, 9-1 September 013 NUMERICAL INVESTIGATION OF CABLE PARAMETRIC VIBRATIONS Marija Nikolić* 1, Verica Raduka
More informationNUMERICAL SIMULATION OF THE INELASTIC SEISMIC RESPONSE OF RC STRUCTURES WITH ENERGY DISSIPATORS
NUMERICAL SIMULATION OF THE INELASTIC SEISMIC RESPONSE OF RC STRUCTURES WITH ENERGY DISSIPATORS ABSTRACT : P Mata1, AH Barbat1, S Oller1, R Boroschek2 1 Technical University of Catalonia, Civil Engineering
More informationA NOTE ON RELATIONSHIP BETWEEN FIXED-POLE AND MOVING-POLE APPROACHES IN STATIC AND DYNAMIC ANALYSIS OF NON-LINEAR SPATIAL BEAM STRUCTURES
European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 212) J. Eberhardsteiner et.al. (eds.) Vienna, Austria, September 1-14, 212 A NOTE ON RELATIONSHIP BETWEEN FIXED-POLE
More informationLaboratory 4 Topic: Buckling
Laboratory 4 Topic: Buckling Objectives: To record the load-deflection response of a clamped-clamped column. To identify, from the recorded response, the collapse load of the column. Introduction: Buckling
More informationProcedure for Performing Stress Analysis by Means of Finite Element Method (FEM)
Procedure for Performing Stress Analysis by Means of Finite Element Method (FEM) Colaboração dos engºs Patrício e Ediberto da Petrobras 1. Objective This Technical Specification sets forth the minimum
More informationModal Analysis: What it is and is not Gerrit Visser
Modal Analysis: What it is and is not Gerrit Visser What is a Modal Analysis? What answers do we get out of it? How is it useful? What does it not tell us? In this article, we ll discuss where a modal
More informationChapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING )
Chapter 5 CENTRIC TENSION OR COMPRESSION ( AXIAL LOADING ) 5.1 DEFINITION A construction member is subjected to centric (axial) tension or compression if in any cross section the single distinct stress
More informationCode_Aster. Finite elements in acoustics
Titre : Éléments finis en acoustique Date : 03/06/2016 Page : 1/10 Finite elements in acoustics Summary: This document describes in low frequency stationary acoustics the equations used, the variational
More informationThomas Whitham Sixth Form Mechanics in Mathematics
Thomas Whitham Sixth Form Mechanics in Mathematics 6/0/00 Unit M Rectilinear motion with constant acceleration Vertical motion under gravity Particle Dynamics Statics . Rectilinear motion with constant
More informationUNIVERSITY PHYSICS I. Professor Meade Brooks, Collin College. Chapter 12: STATIC EQUILIBRIUM AND ELASTICITY
UNIVERSITY PHYSICS I Professor Meade Brooks, Collin College Chapter 12: STATIC EQUILIBRIUM AND ELASTICITY Two stilt walkers in standing position. All forces acting on each stilt walker balance out; neither
More informationMethods of Analysis. Force or Flexibility Method
INTRODUCTION: The structural analysis is a mathematical process by which the response of a structure to specified loads is determined. This response is measured by determining the internal forces or stresses
More informationModelling and numerical simulation of the wrinkling evolution for thermo-mechanical loading cases
Modelling and numerical simulation of the wrinkling evolution for thermo-mechanical loading cases Georg Haasemann Conrad Kloß 1 AIMCAL Conference 2016 MOTIVATION Wrinkles in web handling system Loss of
More informationCode_Aster. SDNL112 - Vibratory damage of origin of a clotheshanger of steam generator
Titre : SDNL112 - Endommagement d'origine vibratoire d'un [...] Date : 23/04/2012 Page : 1/9 SDNL112 - Vibratory damage of origin of a clotheshanger of steam generator Summarized This case of validation
More informationComputational Stiffness Method
Computational Stiffness Method Hand calculations are central in the classical stiffness method. In that approach, the stiffness matrix is established column-by-column by setting the degrees of freedom
More informationEffect of Angular movement of Lifting Arm on Natural Frequency of Container Lifting Mechanism using Finite Element Modal Analysis
Effect of Angular movement of Lifting Arm on Natural Frequency of Container Lifting Mechanism using Finite Element Modal Analysis Khodu M Dhameliya, 2 Utpal V Shah, 3 Dhaval Makwana, 4 Mansi Yadav, 5 Ishankumar
More informationIMPROVING LATERAL STIFFNESS ESTIMATION IN THE DIAGONAL STRUT MODEL OF INFILLED FRAMES
IMPROVING LATERAL STIFFNESS ESTIMATION IN THE DIAGONAL STRUT MODEL OF INFILLED FRAMES I.N. Doudoumis 1 1 Professor, Dept. of Civil Engineering, Aristotle University of Thessaloniki, Thessaloniki, Greece
More informationVibration of Thin Beams by PIM and RPIM methods. *B. Kanber¹, and O. M. Tufik 1
APCOM & ISCM -4 th December, 23, Singapore Vibration of Thin Beams by PIM and RPIM methods *B. Kanber¹, and O. M. Tufik Mechanical Engineering Department, University of Gaziantep, Turkey. *Corresponding
More informationA model for predicting lateral buckling in rails
A model for predicting lateral buckling in rails D. H. Allen Texas A&M University, College Station, TX, U.S.A. G. T. Fry TTCI, Pueblo, CO, U.S.A. ABSTRACT: This paper presents a computational model for
More informationTHE INFLUENCE OF THERMAL ACTIONS AND COMPLEX SUPPORT CONDITIONS ON THE MECHANICAL STATE OF SANDWICH STRUCTURE
Journal of Applied Mathematics and Computational Mechanics 013, 1(4), 13-1 THE INFLUENCE OF THERMAL ACTIONS AND COMPLEX SUPPORT CONDITIONS ON THE MECHANICAL STATE OF SANDWICH STRUCTURE Jolanta Błaszczuk
More informationFig. 1. Circular fiber and interphase between the fiber and the matrix.
Finite element unit cell model based on ABAQUS for fiber reinforced composites Tian Tang Composites Manufacturing & Simulation Center, Purdue University West Lafayette, IN 47906 1. Problem Statement In
More informationSDLV302 Modal analysis by under-structuring: bi-- supported beam
Titre : SDLV302 Analyse modale par sous-structuration : [...] Date : 21/07/2017 age : 1/10 SDLV302 Modal analysis by under-structuring: bi-- supported beam Summary: This test validates the modal analysis
More informationNonlinear Theory of Elasticity. Dr.-Ing. Martin Ruess
Nonlinear Theory of Elasticity Dr.-Ing. Martin Ruess geometry description Cartesian global coordinate system with base vectors of the Euclidian space orthonormal basis origin O point P domain of a deformable
More informationSSLL104 - Predeformations in a straight beam
Titre : SSLL104 - Déformations initiales dans une poutre d[...] Date : 07/08/2012 Page : 1/6 SSLL104 - Predeformations in a straight beam Summarized: This test validates the taking into account of predeformations
More informationSSNP102 - Rate of energy restitution for a plate notched in elastoplasticity: approaches Summarized
Titre : SSNP102 - Taux de restitution d'énergie pour une p[...] Date : 09/08/2010 Page : 1/9 SSNP102 - Rate of energy restitution for a plate notched in elastoplasticity: approaches Summarized GTP: This
More informationName. ME 270 Fall 2005 Final Exam PROBLEM NO. 1. Given: A distributed load is applied to the top link which is, in turn, supported by link AC.
Name ME 270 Fall 2005 Final Exam PROBLEM NO. 1 Given: A distributed load is applied to the top link which is, in turn, supported by link AC. Find: a) Draw a free body diagram of link BCDE and one of link
More informationMechatronics. MANE 4490 Fall 2002 Assignment # 1
Mechatronics MANE 4490 Fall 2002 Assignment # 1 1. For each of the physical models shown in Figure 1, derive the mathematical model (equation of motion). All displacements are measured from the static
More informationTransactions on Engineering Sciences vol 14, 1997 WIT Press, ISSN
On the Computation of Elastic Elastic Rolling Contact using Adaptive Finite Element Techniques B. Zastrau^, U. Nackenhorst*,J. Jarewski^ ^Institute of Mechanics and Informatics, Technical University Dresden,
More informationTopology Optimization of Compliant Mechanism with Geometrical Advantage
610 Topology Optimization of Compliant Mechanism with Geometrical Advantage Seungjae MIN and Younggi KIM A compliant mechanism is a mechanism that produces its motion by the flexibility of some or all
More informationChapter 10 Lecture Outline. Copyright The McGraw-Hill Companies, Inc. Permission required for reproduction or display.
Chapter 10 Lecture Outline Copyright The McGraw-Hill Companies, Inc. Permission required for reproduction or display. 1 Chapter 10: Elasticity and Oscillations Elastic Deformations Hooke s Law Stress and
More informationLinear & Non-linear SSI Calculations: Methods used in EDF to determine raft uplift
Linear & Non-linear SSI Calculations: Methods used in EDF to determine raft uplift Pauline BILLION Frédéric ALLAIN Georges DEVESA Nicolas HUMBERT Ilie PETRE-LAZAR OECD workshop, 8th oct. 2010 OECD Workshop
More informationVortex-induced vibration of a slender single-span cylinder
Vortex-induced vibration of a slender single-span cylinder N. Oikou Delft University of Technology, the Netherlands The goal of this paper is to study the vortex-induced vibration of slender cylindrical
More informationInternational Journal of Advanced Engineering Technology E-ISSN
Research Article INTEGRATED FORCE METHOD FOR FIBER REINFORCED COMPOSITE PLATE BENDING PROBLEMS Doiphode G. S., Patodi S. C.* Address for Correspondence Assistant Professor, Applied Mechanics Department,
More informationStatic Pile Head Impedance using 3D Nonlinear FEM Analysis
Static Pile Head Impedance using 3D Nonlinear FEM Analysis Ichiro NAGASHIMA Technology Center, Taisei Corporation, 344-1 Nasecho, Totsuka-ku, Yokohama 245-51, Japan, ichiro.nagashima@sakura.taisei.co.jp
More information, follows from these assumptions.
Untangling the mechanics and topology in the frictional response of long overhand elastic knots Supplemental Information M.K. Jawed, P. Dieleman, B. Audoly, P. M. Reis S1 Experimental details In this section,
More informationNon-linear and time-dependent material models in Mentat & MARC. Tutorial with Background and Exercises
Non-linear and time-dependent material models in Mentat & MARC Tutorial with Background and Exercises Eindhoven University of Technology Department of Mechanical Engineering Piet Schreurs July 7, 2009
More informationExample-3. Title. Description. Cylindrical Hole in an Infinite Mohr-Coulomb Medium
Example-3 Title Cylindrical Hole in an Infinite Mohr-Coulomb Medium Description The problem concerns the determination of stresses and displacements for the case of a cylindrical hole in an infinite elasto-plastic
More informationVector Mechanics: Statics
PDHOnline Course G492 (4 PDH) Vector Mechanics: Statics Mark A. Strain, P.E. 2014 PDH Online PDH Center 5272 Meadow Estates Drive Fairfax, VA 22030-6658 Phone & Fax: 703-988-0088 www.pdhonline.org www.pdhcenter.com
More informationFinite Element Method in Geotechnical Engineering
Finite Element Method in Geotechnical Engineering Short Course on + Dynamics Boulder, Colorado January 5-8, 2004 Stein Sture Professor of Civil Engineering University of Colorado at Boulder Contents Steps
More informationChapter 7 FORCES IN BEAMS AND CABLES
hapter 7 FORES IN BEAMS AN ABLES onsider a straight two-force member AB subjected at A and B to equal and opposite forces F and -F directed along AB. utting the member AB at and drawing the free-body B
More informationBENCHMARK LINEAR FINITE ELEMENT ANALYSIS OF LATERALLY LOADED SINGLE PILE USING OPENSEES & COMPARISON WITH ANALYTICAL SOLUTION
BENCHMARK LINEAR FINITE ELEMENT ANALYSIS OF LATERALLY LOADED SINGLE PILE USING OPENSEES & COMPARISON WITH ANALYTICAL SOLUTION Ahmed Elgamal and Jinchi Lu October 07 Introduction In this study: I) The response
More informationANALYSIS AND NUMERICAL MODELLING OF CERAMIC PIEZOELECTRIC BEAM BEHAVIOR UNDER THE EFFECT OF EXTERNAL SOLICITATIONS
Third International Conference on Energy, Materials, Applied Energetics and Pollution. ICEMAEP016, October 30-31, 016, Constantine,Algeria. ANALYSIS AND NUMERICAL MODELLING OF CERAMIC PIEZOELECTRIC BEAM
More informationThe effect of restraints type on the generated stresses in gantry crane beam
The effect of restraints type on the generated stresses in gantry crane beam Leszek Sowa 1,*, Wiesława Piekarska 1, Tomasz Skrzypczak 1, Paweł Kwiatoń 1 1 Czestochowa University of Technology, Institute
More informationHSNV140 - Thermoplasticity with restoration of work hardening: test of blocked dilatometry
Titre : HSNV140 - Thermo-plasticité avec restauration d'éc[...] Date : 29/06/2015 Page : 1/11 HSNV140 - Thermoplasticity with restoration of work hardening: test of blocked dilatometry Summary: This test
More informationPhysics. Assignment-1(UNITS AND MEASUREMENT)
Assignment-1(UNITS AND MEASUREMENT) 1. Define physical quantity and write steps for measurement. 2. What are fundamental units and derived units? 3. List the seven basic and two supplementary physical
More informationBAR ELEMENT WITH VARIATION OF CROSS-SECTION FOR GEOMETRIC NON-LINEAR ANALYSIS
Journal of Computational and Applied Mechanics, Vol.., No. 1., (2005), pp. 83 94 BAR ELEMENT WITH VARIATION OF CROSS-SECTION FOR GEOMETRIC NON-LINEAR ANALYSIS Vladimír Kutiš and Justín Murín Department
More informationModels of Bordet and Rice and Tracey
Titre : Modèles de Bordet et de Rice et Tracey Date : 10/01/2018 Page : 1/11 Models of Bordet and Rice and Tracey Summary Lbe bases ofs models of local approach of the rupture who allowing to model brittle
More informationBiaxial Analysis of General Shaped Base Plates
Biaxial Analysis of General Shaped Base Plates R. GONZALO ORELLANA 1 Summary: A linear model is used for the contact stresses calculation between a steel base plate and a concrete foundation. It is also
More informationM.S Comprehensive Examination Analysis
UNIVERSITY OF CALIFORNIA, BERKELEY Spring Semester 2014 Dept. of Civil and Environmental Engineering Structural Engineering, Mechanics and Materials Name:......................................... M.S Comprehensive
More informationIntroduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams.
Outline of Continuous Systems. Introduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams. Vibrations of Flexible Strings. Torsional Vibration of Rods. Bernoulli-Euler Beams.
More informationSOIL-STRUCTURE INTERACTION, WAVE PASSAGE EFFECTS AND ASSYMETRY IN NONLINEAR SOIL RESPONSE
SOIL-STRUCTURE INTERACTION, WAVE PASSAGE EFFECTS AND ASSYMETRY IN NONLINEAR SOIL RESPONSE Mihailo D. Trifunac Civil Eng. Department University of Southern California, Los Angeles, CA E-mail: trifunac@usc.edu
More informationExpansion of circular tubes by rigid tubes as impact energy absorbers: experimental and theoretical investigation
Expansion of circular tubes by rigid tubes as impact energy absorbers: experimental and theoretical investigation M Shakeri, S Salehghaffari and R. Mirzaeifar Department of Mechanical Engineering, Amirkabir
More informationSelected Topics in Physics a lecture course for 1st year students by W.B. von Schlippe Spring Semester 2007
Selected Topics in Physics a lecture course for st year students by W.B. von Schlippe Spring Semester 7 Lecture : Oscillations simple harmonic oscillations; coupled oscillations; beats; damped oscillations;
More informationALGORITHM FOR NON-PROPORTIONAL LOADING IN SEQUENTIALLY LINEAR ANALYSIS
9th International Conference on Fracture Mechanics of Concrete and Concrete Structures FraMCoS-9 Chenjie Yu, P.C.J. Hoogenboom and J.G. Rots DOI 10.21012/FC9.288 ALGORITHM FOR NON-PROPORTIONAL LOADING
More informationC7047. PART A Answer all questions, each carries 5 marks.
7047 Reg No.: Total Pages: 3 Name: Max. Marks: 100 PJ DUL KLM TEHNOLOGIL UNIVERSITY FIRST SEMESTER.TEH DEGREE EXMINTION, DEEMER 2017 ourse ode: E100 ourse Name: ENGINEERING MEHNIS PRT nswer all questions,
More informationRigid Flexible Contact Analysis of an Inflated Membrane Balloon with Various Contact Conditions
roceedings Rigid Flexible Contact Analysis of an Inflated Membrane Balloon with Various Contact Conditions MengXiong Liu and XiDe Li * Department of Engineering Mechanics, Tghua University, Beijing 100084,
More informationUsing MATLAB and. Abaqus. Finite Element Analysis. Introduction to. Amar Khennane. Taylor & Francis Croup. Taylor & Francis Croup,
Introduction to Finite Element Analysis Using MATLAB and Abaqus Amar Khennane Taylor & Francis Croup Boca Raton London New York CRC Press is an imprint of the Taylor & Francis Croup, an informa business
More informationTorsion Spring Oscillator with Dry Friction
Torsion Spring Oscillator with Dry Friction Manual Eugene Butikov Annotation. The manual includes a description of the simulated physical system and a summary of the relevant theoretical material for students
More informationStatic Equilibrium. University of Arizona J. H. Burge
Static Equilibrium Static Equilibrium Definition: When forces acting on an object which is at rest are balanced, then the object is in a state of static equilibrium. - No translations - No rotations In
More information