Chapter 3. Estimation of Earthquake Load Effects

Similar documents
CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE

Structural Dynamics and Earthquake Engineering

Second Order Analysis

Week3, Chapter 4. Position and Displacement. Motion in Two Dimensions. Instantaneous Velocity. Average Velocity

Assessment of Site Amplification Effect from Input Energy Spectra of Strong Ground Motion

9.2 Seismic Loads Using ASCE Standard 7-93

ENGN 40 Dynamics and Vibrations Homework # 7 Due: Friday, April 15

11. Dynamics in Rotating Frames of Reference

EN40: Dynamics and Vibrations. Homework 4: Work, Energy and Linear Momentum Due Friday March 1 st

Irregular vibrations in multi-mass discrete-continuous systems torsionally deformed

Effect of loading frequency on the settlement of granular layer

829. An adaptive method for inertia force identification in cantilever under moving mass

Lecture 8 Modal Analysis

COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD

Indeterminate pin-jointed frames (trusses)

Plan: Fuselages can. multideck

FUZZY FINITE ELEMENT METHOD

DUE: WEDS FEB 21ST 2018

REINFORCED CONCRETE STRUCTURE DESIGN ANALYSIS UNDER EARTHQUAKE LOADING (LATERAL LOAD)

A Mechanics-Based Approach for Determining Deflections of Stacked Multi-Storey Wood-Based Shear Walls

The equation of motion of a dynamical system is given by a set of differential equations. That is (1)

THE EFFECT OF BEAM TO COLUMN CONNECTION IN ARC PORTAL FRAME

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

Chapter 11: Angular Momentum

Introduction to Vapor/Liquid Equilibrium, part 2. Raoult s Law:

Moments of Inertia. and reminds us of the analogous equation for linear momentum p= mv, which is of the form. The kinetic energy of the body is.

Difference Equations

Finite Element Modelling of truss/cable structures

Week 9 Chapter 10 Section 1-5

NONLINEAR NATURAL FREQUENCIES OF A TAPERED CANTILEVER BEAM

November 5, 2002 SE 180: Earthquake Engineering SE 180. Final Project

DESIGN SPECTRUM-BASED SCALING OF STRENGTH REDUCTION FACTORS

ORIGIN 1. PTC_CE_BSD_3.2_us_mp.mcdx. Mathcad Enabled Content 2011 Knovel Corp.

THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS OF A TELESCOPIC HYDRAULIC CYLINDER SUBJECTED TO EULER S LOAD

EXPERIMENTAL STUDY OF A SEISMICALLY ISOLATED BUILDING STRUCTURE SUBJECT TO TRIAXIAL GROUND MOTIONS

Gravitational Acceleration: A case of constant acceleration (approx. 2 hr.) (6/7/11)

( ) = ( ) + ( 0) ) ( )

GEO-SLOPE International Ltd, Calgary, Alberta, Canada Vibrating Beam

Module 11 Design of Joints for Special Loading. Version 2 ME, IIT Kharagpur

NON LINEAR ANALYSIS OF STRUCTURES ACCORDING TO NEW EUROPEAN DESIGN CODE

EN40: Dynamics and Vibrations. Homework 7: Rigid Body Kinematics

Open Systems: Chemical Potential and Partial Molar Quantities Chemical Potential

Physics 5153 Classical Mechanics. D Alembert s Principle and The Lagrangian-1

8.592J: Solutions for Assignment 7 Spring 2005

ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM

Physics 207: Lecture 20. Today s Agenda Homework for Monday

Chapter Eight. Review and Summary. Two methods in solid mechanics ---- vectorial methods and energy methods or variational methods

Physics 53. Rotational Motion 3. Sir, I have found you an argument, but I am not obliged to find you an understanding.

PRATICAL STATIC CALCULATION METHOD FOR ESTIMATING ELASTO-PLASTIC DYNAMIC RESPONSES OF SPACE FRAMES

Excavation Induced Building Response by Laminate Beam Method

Please initial the statement below to show that you have read it

APPENDIX F A DISPLACEMENT-BASED BEAM ELEMENT WITH SHEAR DEFORMATIONS. Never use a Cubic Function Approximation for a Non-Prismatic Beam

I have not received unauthorized aid in the completion of this exam.

Section 8.3 Polar Form of Complex Numbers

MEASUREMENT OF MOMENT OF INERTIA

GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE

Numerical Heat and Mass Transfer

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

Statistical Energy Analysis for High Frequency Acoustic Analysis with LS-DYNA

The optimal delay of the second test is therefore approximately 210 hours earlier than =2.

Homework 2: Kinematics and Dynamics of Particles Due Friday Feb 7, 2014 Max Score 45 Points + 8 Extra Credit

First Law: A body at rest remains at rest, a body in motion continues to move at constant velocity, unless acted upon by an external force.

Amplification and Relaxation of Electron Spin Polarization in Semiconductor Devices

Global Sensitivity. Tuesday 20 th February, 2018

Strength Requirements for Fore Deck Fittings and Equipment

CHAPTER 9 CONCLUSIONS

One Dimensional Axial Deformations

SIMPLIFIED PREDICTION METHOD FOR SEISMIC RESPONSE OF ROCKING STRUCTURAL SYSTEMS WITH YIELDING BASE PLATES

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

χ x B E (c) Figure 2.1.1: (a) a material particle in a body, (b) a place in space, (c) a configuration of the body

Part C Dynamics and Statics of Rigid Body. Chapter 5 Rotation of a Rigid Body About a Fixed Axis

High resolution entropy stable scheme for shallow water equations

Seismic Earth Pressure Development in Sheet Pile Retaining Walls: A Numerical Study

Frame element resists external loads or disturbances by developing internal axial forces, shear forces, and bending moments.

Transfer Functions. Convenient representation of a linear, dynamic model. A transfer function (TF) relates one input and one output: ( ) system

Preliminary Design of Moment-Resisting Frames

Chapter 12 Equilibrium & Elasticity

Lab 2e Thermal System Response and Effective Heat Transfer Coefficient

Chapter 3. r r. Position, Velocity, and Acceleration Revisited

Class: Life-Science Subject: Physics

THE SMOOTH INDENTATION OF A CYLINDRICAL INDENTOR AND ANGLE-PLY LAMINATES

COMPLEX NUMBERS AND QUADRATIC EQUATIONS

How Differential Equations Arise. Newton s Second Law of Motion

STATIC ANALYSIS OF TWO-LAYERED PIEZOELECTRIC BEAMS WITH IMPERFECT SHEAR CONNECTION

SEISMIC ANALYSIS AND DESIGN OF BUILDING STRUCTURES WITH SUPPLEMENTAL LEAD DAMPERS

Frequency dependence of the permittivity

Evaluation of the accuracy of the Multiple Support Response Spectrum (MSRS) method

(Online First)A Lattice Boltzmann Scheme for Diffusion Equation in Spherical Coordinate

Physics 207 Lecture 6

Experimental Study on Ultimate Strength of Flexural-Failure-Type RC Beams under Impact Loading

where v means the change in velocity, and t is the

Adiabatic Sorption of Ammonia-Water System and Depicting in p-t-x Diagram

NEAR-FIELD PULSE-TYPE MOTION OF SMALL EVENTS IN DEEP GOLD MINES: OBSERVATIONS, RESPONSE SPECTRA AND DRIFT SPECTRA.

MODAL ANALYSIS AND TESTING OF ROTATING MACHINES FOR PREDICTIVE MAINTENANCE: EFFECT OF GYROSCOPIC FORCES

8 Derivation of Network Rate Equations from Single- Cell Conductance Equations

Kinematics in 2-Dimensions. Projectile Motion

OFF-AXIS MECHANICAL PROPERTIES OF FRP COMPOSITES

5.04, Principles of Inorganic Chemistry II MIT Department of Chemistry Lecture 32: Vibrational Spectroscopy and the IR

Principles of Food and Bioprocess Engineering (FS 231) Solutions to Example Problems on Heat Transfer

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

Transcription:

Chapter 3. Estmaton of Earthquake Load Effects 3.1 Introducton Sesmc acton on chmneys forms an addtonal source of natural loads on the chmney. Sesmc acton or the earthquake s a short and strong upheaval of the ground. Ths naturally s the cause for loads on any structure. Any structure under sesmc loadng s subjected to cyclcal loadng for a short perod of tme. An earthquake s descrbed by ts ntensty and t epcenter. The ntensty of and earthquake at a place s a measure of the degree of shakng caused durng the earthquake and thus characterzes the effect of the earthquake. Most of the study of earthquakes up to the begnnng of the twenteth century dealt wth the effects of earthquakes and to quanttatvely descrbe these effects a number of ntensty scales were ntroduced. Intally there was the Ross-Forel scale that had ten dvsons. In 1888 Mercall proposed a scale wth 1 subdvsons to permt a clear dstncton n shocks of extreme ntensty. After a number of changes the Modfed Mercall scale or smply the MM scale s generally used by engneers today. Another revson made n 1956 to the MM scale by Rchter s also n use. The focus s the source for the propagaton of sesmc waves. It s also called the hypocenter. The depth of the focus from the surface of the earth drectly above s referred to as the focal depth. The pont on the earth s surface drectly above the focus s known as the epcenter. The structure experences cyclc loadng durng the process of sesmc acton. Ths causes energy to buld up n the system leadng to ts collapse. The frcton wth ar, frcton between partcles that consttute the structure, frcton at junctons of structural elements, yeldng of the structural materal and other processes of energy dsspaton depress the ampltude of moton of a vbratng structure and the vbratons de out n course of tme. When such nternal and or external frcton fully dsspates the energy of the structural system durng ts moton from a dsplaced poston to ts ntal poston of rest, nhbtng oscllatons of the structure, the structure s sad to be crtcally damped. 5

Thus the dampng beyond whch moton wll not be oscllatory s called crtcal dampng. The effect of energy dsspaton n reducng successve ampltude of vbratons of a structure from the poston of statc equlbrum s called dampng and s expressed as a percentage of crtcal dampng. There are other terms that are mportant wth respect to sesmc analyss. Durng earthquakes there occurs a sate n saturated coheson less sol where n the effectve shear strength s reduced to a neglgble value, for all engneerng purposes. Un ths condton the sol tends to behave lke a flud mass. A system s sad to be vbratng n ts normal mode or prncpal mode when all ts masses attan maxmum values of dsplacement smultaneously and they also pass through the equlbrum postons smultaneously. When a system s vbratng n ts normal mode, the ampltude of the masses at any partcular tme expressed as a rato of the ampltude of one of the masses s known as the mode shape coeffcent. Durng an earthquake ground vbrated (moves) n all drectons. The horzontal component of the ground moton s generally more ntense than that of the vertcal components durng strng earthquakes. The ground moton s generally random n nature and generally the random peaks of varous drectons may not occur smultaneously. Hence for desgn purposes, at one tme, t s assumed that only the horzontal component acts n any one drecton. All structures are desgned to wthstand ther own weght. Ths could be deemed as though a vertcal acceleraton of 1g s appled to the varous masses of the system. Snce the desgn vertcal forces proposed n the codes are small as compared to the acceleraton of 1 gravty, the same emphass has not been gven to the vertcal forces as compared to the horzontal forces. However for structures where stablty s a crteron t may become necessary to take nto account these vertcal forces. 3. Estmaton of loads The sesmc acton s descrbed by means of a standardzed acceleraton response spectrum. The CICIND code suggests a general response spectra. The response spectra s a relaton between the maxmum effectve peak ground acceleraton at the locaton of the 6

chmney. Ths s n relaton wth the natural tme perod of the structure and the sol type exstng at the ste. The movement of the chmney s found by calculatng the frst few mode shapes by modal analyss of the chmney. The result of such a modal analyss wll yeld the values for the deflecton, the shear force and the moment. The modal analyss can determne the functons of the deflecton, shear and the moment only up to a constant factor. Thus f the mode shape calculated s known, then a constant tmes the mode shape too s a possble soluton. Hence the actual value of the shear force or the bendng moment s found by multplyng the normalzed response wth a scalng factor. gven by Hence f u s the value of the normalzed mode shape then the true mode shape s u un (3.1) Where they refer to the th mode of vbraton, and N s the scalng factor. The scalng factor s determned by the followng equaton. N pt 4 a ( T ) s (3.) The a s s the response functon descrbed earler. The value of p s obtaned from p h h u ( z) m( z) dz u ( z) m( z) dz (3.3) The code also assumes the vertcal movements to result n a value of resultants that are.3 tmes the horzontal forces. The ACI code also assumes the vertcal component to be neglgble wth respect to the horzontal one. The code also suggests the spectral values for the values of maxmum ground acceleraton. The followng calculatons are based on the IS code. The code used s the IS:1893-1975. 7

Snce the earthquakes occur wthout any warnng, t s very necessary to avod constructon practces that cause sudden falure or brttle falure. The current phlosophy reles heavly on the acton of members to absorb all the vbratonal energy resultng from strong ground moton by desgnng the member to behave n a ductle manner. In ths manner even f an earthquake occurs that s stronger than that whch has been foreseen, total collapse of the buldng can be avoded. Earthquake resstant desgns are generally performed by pseudo-statc analyss, the earthquake loads on the foundatons are consdered as statc loads and hence capable of producng settlement as dead loads. Therefore as the footngs are generally desgned for equal stresses under them, the footngs for exteror columns wll have to be made wder. Permssble ncrease n safe bearng pressure wll have to depend n the solfoundaton system. Where small settlements are lkely to occur larger ncrease can be allowed and vce versa. 3..1 Desgn sesmc coeffcents for dfferent zones The force attracted by any structure durng an earthquake s dynamc n nature and s a functon of the ground moton and the propertes of the structure tself. the domnant effect s equvalent to a horzontal force varyng over the heght of the structure. Therefore the assumpton of a unform force to be appled along one axs at a tme s an oversmplfcaton whch can be justfed for reasons of savng effort n dynamc analyss. However a large number of structures desgned on ths bass have wthstood earthquake shocks n the past. Ths s a justfcaton of a unform sesmc coeffcent n sesmc desgn. In the code, therefore, t s consdered adequate to provde unform sesmc coeffcents to ordnary structures. The IS code suggests two methods for the purpose of evaluaton of the earthquake loads. Ths s smlar to the two methods suggested for the calculaton of across-wnd loads. Both methods calculate the desgn value of the horzontal coeffcent. Sesmc coeffcent method The value of the horzontal sesmc desgn coeffcent shall be calculated usng the followng expresson. 8

h I (3.4) 1.5. Where s a coeffcent dependng on the sol type. Ths value vares between 1. and I s the mportance factor. s the basc horzontal sesmc coeffcent. The response spectrum method The response acceleraton s frst obtaned for the natural tme perod and dampng of the structure and the desgn value of horzontal sesmc coeffcent s computed usng the followng expresson. S IF a h g (3.5) Here F s a sesmc zone factor. S a /g s the average acceleraton coeffcent dependng on the natural perod and dampng of the structure. 3.3 Calculatons for a typcal case The calculaton of the earthquake load for a typcal chmney s gven below. The assumptons made are also specfed. The weght data for the case has been taken from the STRAP model of the chmney. Perod of vbraton Dameter of the base =.7 m Base Thckness =.649m Inner dameter at the base s 1.4m Area of cross secton at the base s A d out d n 4 (3.6) 9

A = 45. m The moment of nerta at the base s calculated by The value of I = 74.5 m 4 Radus of gyraton r s gven by r = 7.86 I 4 4 (3.7) 64 d out d n Hence the slenderness raton l/r s gven by I r (3.8) A l r 3. (3.9) The coeffcent C T C T 57.8 (3.1) Weght of the chmney Wt D mean TH t (3.11) Weght = 17495583 kg The perod of vbraton s now gven by Wh t ' T C (3.1) T EAg Substtutng the values the value of T = 15.6 Desgn sesmc coeffcent Usng the Response Spectrum method and the equaton ** a h =.3975 the value assumed are = 1. (assumng a hard/medum sols) I = 1. (mportance factor) 3

F =.5 (assumng the chmney to be n the zone IV) Shear force and Bendng moments The desgn shear force at a dstance of X from the top s gven by V 5X ' X ' C W (3.13) V h t 3h' 3h' Where the value of C V has been found to be. for the very large tme perod obtaned. Varyng the value of X from to 5 the profle of the shear force has been calculated. 3 5 15 1 5 5 1 15 kn Fgure 3.1 Shear force due to sesmc loads The bendng moment can be calculated usng the formula M 1 4 X ' X ' hwh t.6.4 h' h' (3.14) 31

Agan the value of X s vared and the expresson evaluated. The resultant graph s gven below. 3 5 15 1 5 4 6 8 1 MNm Fgure 3. Bendng Moment due to sesmc loads As can be seen from the graph, the maxmum moment at the base of the chmney s about 8 MNm. 3.4 Conclusons The reasons and assumptons nvolved n the evaluaton of earthquake loads have been studed. The codal provsons for the calculaton of the same have been understood. A sample calculaton has been done to calculate the shear force and bendng moment caused due to earthquake loadng on chmneys. The loads n ths case have been found to be sgnfcantly lower that those obtaned n the wnd analyss. Hence earthquake loads do not normally form the man loads to be consdered for desgn. 3