RESPONSE OF A SINGLE-DEGREE-OF-FREEDOM SYSTEM SUBJECTED TO A TERMINAL SAWTOOTH APPLIED FORCE

Size: px
Start display at page:

Download "RESPONSE OF A SINGLE-DEGREE-OF-FREEDOM SYSTEM SUBJECTED TO A TERMINAL SAWTOOTH APPLIED FORCE"

Transcription

1 RESPONSE OF A SINGLE-DEGREE-OF-FREEDOM SYSTEM SUBJECTED TO A TERMINAL SAWTOOTH APPLIED FORCE By Tom Irvie Emil: tomirvie@ol.om Ferury 5, 6 Itroutio Coier the igle-egree-of-freeom ytem i Figure. F(t) x m k Figure. where m i the m i the viou mpig oeffiiet k i the tiffe x i the olute iplemet of the m F(t) i the pplie fore A free-oy igrm i how i Figure.

2 F(t) m kx x& Figure. Summtio of fore i the vertil iretio F m & x () m & x x& kx F(t) () mx && x& k x F(t) () && k x x x F(t) m & m m (4) By ovetio ( m) ξω (k m) ω where ω i the turl frequey i (rie), ξ i the mpig rtio. Sutitute the ovetio term ito equtio (5). & x ξωx& ω x F(t) (5) m

3 Termil Swtooth Pule Coier the pule give y equtio (6). F (t) Fˆ t T,, t T t > T (6) The equtio of motio eome ˆF t && x ξω x& ω x, m T t T (7) Now tke the Lple trform. { } ˆF t L && x ξω x& ω x L m T (8) X() x() x() & ξω X() ξωx() Fˆ ω X() (9) { } { } { } Fˆ ξω ω X() x() & ξω x() () { } { } Fˆ ξω ω X() x() & ξω x() ()

4 { } ˆ x() & ξω x() F X() ξω ω ξω ω () Let X () X () X f () () where { ξω } x() & x() X () ξω ω (4) Fˆ X f () ξω ω (5) Coier the eomitor term, ( ) ( ) ξω ω ξω ω ξω (6) ( ) ( ) ξω ω ξω ω ξ (7) Now efie the mpe turl frequey, ω ω ξ (8) Sutitute equtio (8) ito (7), ξω ( ) ω ξω ω (9) Sutitute equtio (9) ito (5). 4

5 x() & X () { ξω } x() ( ξω ) ω () Rerrge the term ito oveiet formt prior to the ivere Lple trform. X () ( ξω ) ( ξω ) x() ω x() & ( ξω ) x() ( ξω ) ω () X () ( ξω ) ( ξω ) ( ξω ) x() & x() ω x() ω ω ( ξω ) ω () Tke the ivere Lple trform uig Referee. x (t) x() exp ( ξω ) o( ω ) t t ( ξω ) x() & ω x() exp ( ξω ) x() ( ξω ) ( ω ) x() t i t t & x (t) exp x() o ω ( ξω ) i( ω ) t ( ω ) t () (4) Rell equtio (5). Fˆ X f () ξω ω (5) Exp ito prtil frtio uig Appeix A. (6) 5

6 ξω (7) ω (8) X () f ˆ F ξω ω ξω ξω ω 4 ω ξω ω ( ) (9) X () f ˆ F ξ ω ξ ξ ω ω ω ξω ω ( ) () X () f ˆ F ξ ω ξ ξ ω ω ω ξω ω ( ) () ( ξω ) ω ξω ω () X () f ˆ ( F ξ ω ξ ξ ) ω ω ω ( ξω ) ω () X () f ξ ω ( ξ) ˆF ξ ω ω ( ξω ) ω (4) 6

7 ( ) Fˆ ω ξ ξ ω ξ X f () [ ] ξ ω ( ξω ) ω (5) ω ( ) ξ ˆF ξ ω ξ X f () [ ] ξ ω ( ) ξω ω (6) ω ( ) ξ ˆF ξ ω ξ X f () [ ] ξ ( ) ω ξω ω (7) ˆ F ξ ω ξω X () ω f ξ ( ) ( ω ξω ω ξω ) ω (8) ˆ F ξ ω ξω X () ω f ξ ( ) ( ω ξω ω ξω ) ω (9) ˆ F ξ ω X () ξω ξ ω ω f ξ ( ) ( ω ξω ω ξω ) ω (4) 7

8 ˆ F ξ ω ξω ξ X f () ξ ω ( ) ( ω ξω ω ξω ) ω (4) X () f ˆ F ξ ξ ξω ξ ω ω ω ( ) ( ) ξω ω ξω ω (4) X () f ˆ F ξ ξ ξω ξ ω ω ( ) ( ) ω ξω ω ξω ω (4) Tke the ivere Lple trform uig Referee. The iplemet i ˆF ξ ξ x (t) t exp f ( t) o( t) ( ) i ( t) ξω ω ξ ω ω ω ω ω (44) ( ξω ) x() ( ξω ) ( ω ) x() t i t t & x (t) exp x() o ω ( ω ) (45) 8

9 The totl iplemet i ( ) x() & ξω x() x(t) exp( ξωt ) x() o( ω t) i ( ωt ) ω ˆF ξ ξ t exp ( t) o( t) ( ) i ( t ), ξω ω ξ ω ω ω ω ω t T (46) The olutio for t > T i the free virtio olutio. The totl veloity i ( ) x() & ξω x() x(t) & ξω exp( ξωt) x()o( ω t) i( ωt) ω { } ( ) ( ) & ( ) ( ) exp ξωt x() ωi ω t x() ξω x() o ωt ˆF ξ exp( t) o( t) ( ) i ( t) ξω ξω ω ξ ω ω ω ω ˆF ξω { ( ) exp t } i ( t) ω ξω ω ( ξ ) o( ωt ), ω t T (47) 9

10 ω ( ) x(t) & exp ξωt x() & o( ω t) [ ξx() & ω x() ] i ( ωt ) ω Fˆ ξω exp ( t) o ω ξω ( ω t) ( ξ ) i ( ωt ) ω ω ω, t T (48) ω x(t) exp( t) x() o( t) & ξω & ω [ ξx() & ω x() ] i ( ωt ) ω ˆF ξω exp( t ) o( t) ( ) ( ) i ( t) ξω ω ξ ξ ω ω ω, t T (49)

11 ω x(t) exp( t) x() o( t) & ξω & ω [ ξx() & ω x() ] i ( ωt ) ω ˆF ξω exp( t) o( t) i ( t ), ξω ω ω ω ω t T (5)

12 Exmple APPLIED FORCE TERMINAL SAWTOOTH PULSE (, N,. e ) 8 FORCE (N) Figure. TIME (SEC) DISPLACEMENT TIME HISTORY ( m5 kg, f 8 Hz, Q ) 5 DISP (mm) TIME (SEC) Figure 4. A igle-egree-of-freeom ytem i ujete to the pplie fore i Figure. The repoe i give i Figure 4. The hrteriti of the ytem re give i the plot title.

13 Exmple NON-DIMENSIONAL SRS APPLIED FORCE TERMINAL SAWTOOTH PULSE Q 5 Negtive Poitive K X F.5... DURATION PERIOD Figure 5. A o-imeiol iplemet SRS i give i Figure 5. The perio i the ivere of the turl frequey. Referee. T. Irvie, Tle of Lple Trform, Virtiot, T. Irvie, Prtil Frtio i Shok Virtio Alyi, Virtiot, 999.

14 4 APPENDIX A Prtil Frtio Expio (A-) [ ] [ ] (A-) (A-) [ ] [ ] [ ] (A-4) (A-5) (A-6)

15 5 (A-7) (A-8) (A-9) ( ) (A-) ( ) [ ] (A-)

16 6 [ ] (A-) (A-) (A-4) (A-5)

All the Laplace Transform you will encounter has the following form: Rational function X(s)

All the Laplace Transform you will encounter has the following form: Rational function X(s) EE G Note: Chpter Itructor: Cheug Pge - - Iverio of Rtiol Fuctio All the Lplce Trform you will ecouter h the followig form: m m m m e τ 0...... Rtiol fuctio Dely Why? Rtiol fuctio come out turlly from

More information

Chap8 - Freq 1. Frequency Response

Chap8 - Freq 1. Frequency Response Chp8 - Freq Frequecy Repoe Chp8 - Freq Aged Prelimirie Firt order ytem Frequecy repoe Low-p filter Secod order ytem Clicl olutio Frequecy repoe Higher order ytem Chp8 - Freq 3 Frequecy repoe Stedy-tte

More information

SHOCK RESPONSE OF MULTI-DEGREE-OF-FREEDOM SYSTEMS Revision F By Tom Irvine May 24, 2010

SHOCK RESPONSE OF MULTI-DEGREE-OF-FREEDOM SYSTEMS Revision F By Tom Irvine   May 24, 2010 SHOCK RESPONSE OF MULTI-DEGREE-OF-FREEDOM SYSTEMS Revision F By Tom Irvine Email: tomirvine@aol.com May 4, 010 Introduction The primary purpose of this tutorial is to present the Modal Transient method

More information

Solutions for homework 5

Solutions for homework 5 1 Section 4.3 Solutions for homework 5 17. The following equation has repeated, real, characteristic roots. Find the general solution. y 4y + 4y = 0. The characteristic equation is λ 4λ + 4 = 0 which has

More information

Dynamics of Structures

Dynamics of Structures Dynamics of Structures Elements of structural dynamics Roberto Tomasi 11.05.2017 Roberto Tomasi Dynamics of Structures 11.05.2017 1 / 22 Overview 1 SDOF system SDOF system Equation of motion Response spectrum

More information

ROUTH-HURWITZ CRITERION

ROUTH-HURWITZ CRITERION Automti Cotrol Sytem, Deprtmet of Mehtroi Egieerig, Germ Jordi Uiverity Routh-Hurwitz Criterio ite.google.om/ite/ziydmoud 7 ROUTH-HURWITZ CRITERION The Routh-Hurwitz riterio i lytil proedure for determiig

More information

Chapter #2 EEE Subsea Control and Communication Systems

Chapter #2 EEE Subsea Control and Communication Systems EEE 87 Chpter # EEE 87 Sube Cotrol d Commuictio Sytem Trfer fuctio Pole loctio d -ple Time domi chrcteritic Extr pole d zero Chpter /8 EEE 87 Trfer fuctio Lplce Trform Ued oly o LTI ytem Differetil expreio

More information

Some Aspects of Structural Dynamics

Some Aspects of Structural Dynamics Appendix B Some Aspects of Structural Dynamics This Appendix deals with some aspects of the dynamic behavior of SDOF and MDOF. It starts with the formulation of the equation of motion of SDOF systems.

More information

The Performance of Feedback Control Systems

The Performance of Feedback Control Systems The Performace of Feedbac Cotrol Sytem Objective:. Secify the meaure of erformace time-domai the firt te i the deig roce Percet overhoot / Settlig time T / Time to rie / Steady-tate error e. ut igal uch

More information

TWO-STAGE ISOLATION FOR HARMONIC BASE EXCITATION Revision A. By Tom Irvine February 25, 2008

TWO-STAGE ISOLATION FOR HARMONIC BASE EXCITATION Revision A. By Tom Irvine   February 25, 2008 TWO-STAGE ISOLATION FOR HARMONIC BASE EXCITATION Revision A By Tom Irvine Email: tomirvine@aol.com February 5, 008 Introduction Consider a base plate mass m and an avionics mass m modeled as two-degree-of-freedom.

More information

F = ma, F R + F S = mx.

F = ma, F R + F S = mx. Mechanical Vibrations As we mentioned in Section 3.1, linear equations with constant coefficients come up in many applications; in this section, we will specifically study spring and shock absorber systems

More information

Physics 214 Spring 1997 PROBLEM SET 2. Solutions

Physics 214 Spring 1997 PROBLEM SET 2. Solutions Physics 214 Spring 1997 PROBLEM SET 2 Solutions 1. Tipler, Chapter 13, p.434, Problem 6 The general expression for the displacement field associated with a traveling wave is y(x,t) = f(x vt) in which v

More information

Mathematical modeling of dynamic systems: Chapter 3: Mathematical modeling of dynamic systems. Linearization of nonlinear systems:

Mathematical modeling of dynamic systems: Chapter 3: Mathematical modeling of dynamic systems. Linearization of nonlinear systems: hpter : themticl modelig of dymic ytem Itructor: S. Frhdi themticl modelig of dymic ytem: Simplicity veru ccurcy: it i poible to improve the ccurcy of mthemticl model by icreig it compleity. Lier ytem:

More information

Mechanical Translational Systems

Mechanical Translational Systems QUESTION 1 For the system in Figure 1.1, the springs are at their free lengths when the mass displacements are zero. Complete the following: Figure 1.1 QUESTION 2 For the system in Figure 2.1, the mass

More information

Dynamic Modeling. For the mechanical translational system shown in Figure 1, determine a set of first order

Dynamic Modeling. For the mechanical translational system shown in Figure 1, determine a set of first order QUESTION 1 For the mechanical translational system shown in, determine a set of first order differential equations describing the system dynamics. Identify the state variables and inputs. y(t) x(t) k m

More information

z 0 > 0 z = 0 h; (x, 0)

z 0 > 0 z = 0 h; (x, 0) n = (q 1,..., q n ) T (,, t) V (,, t) L(,, t) = T V d dt ( ) L q i L q i = 0, i = 1,..., n. l l 0 l l 0 l > l 0 {x} + = max(0, x) x = k{l l 0 } +ˆ, k > 0 ˆ (x, z) x z (0, z 0 ) (0, z 0 ) z 0 > 0 x z =

More information

SHOCK AND VIBRATION RESPONSE SPECTRA COURSE Unit 1B. Damping

SHOCK AND VIBRATION RESPONSE SPECTRA COURSE Unit 1B. Damping SHOCK AND VIBRATION RESPONSE SPECTRA COURSE Unit 1B. Damping By Tom Irvine Introduction Recall the homework assignment from Unit 1A. The data.txt time history represented a rocket vehicle dropped from

More information

Chapter 5 Design. D. J. Inman 1/51 Mechanical Engineering at Virginia Tech

Chapter 5 Design. D. J. Inman 1/51 Mechanical Engineering at Virginia Tech Chapter 5 Design Acceptable vibration levels (ISO) Vibration isolation Vibration absorbers Effects of damping in absorbers Optimization Viscoelastic damping treatments Critical Speeds Design for vibration

More information

2. The Laplace Transform

2. The Laplace Transform . The Lplce Trnform. Review of Lplce Trnform Theory Pierre Simon Mrqui de Lplce (749-87 French tronomer, mthemticin nd politicin, Miniter of Interior for 6 wee under Npoleon, Preident of Acdemie Frncie

More information

Lecture Notes on. BST004: Structural Dynamics. M. Tech Structural Engineering

Lecture Notes on. BST004: Structural Dynamics. M. Tech Structural Engineering Lecture Notes on BST004: Structural Dynamics M. Tech Structural Engineering Department of Civil Engineering INSTITUTE OF AERONAUTICAL ENGINEERING Dundigal, Hyderabad Disclaimer This document does not claim

More information

Using Simulink to analyze 2 degrees of freedom system

Using Simulink to analyze 2 degrees of freedom system Using Simulink to analyze 2 degrees of freedom system Nasser M. Abbasi Spring 29 page compiled on June 29, 25 at 4:2pm Abstract A two degrees of freedom system consisting of two masses connected by springs

More information

SHOCK AND VIBRATION RESPONSE SPECTRA COURSE Unit 6A. The Fourier Transform. By Tom Irvine

SHOCK AND VIBRATION RESPONSE SPECTRA COURSE Unit 6A. The Fourier Transform. By Tom Irvine SHOCK ND VIBRTION RESPONSE SPECTR COURSE Unit 6. The Fourier Transform By Tom Irvine Introduction Stationary vibration signals can be placed along a continuum in terms of the their qualitative characteristics.

More information

Session 1 : Fundamental concepts

Session 1 : Fundamental concepts BRUFACE Vibrations and Acoustics MA1 Academic year 17-18 Cédric Dumoulin (cedumoul@ulb.ac.be) Arnaud Deraemaeker (aderaema@ulb.ac.be) Exercise 1 Session 1 : Fundamental concepts Consider the following

More information

Superposition of electromagnetic waves

Superposition of electromagnetic waves Superposition of electromagnetic waves February 9, So far we have looked at properties of monochromatic plane waves. A more complete picture is found by looking at superpositions of many frequencies. Many

More information

2 SKEE/SKEU v R(t) - Figure Q.1(a) Evaluate the transfer function of the network as

2 SKEE/SKEU v R(t) - Figure Q.1(a) Evaluate the transfer function of the network as SKEE/SKEU 073 PART A Q. ) A trfer futio i ued to deribe the reltiohi betwee the iut d outut igl of ytem. Figure Q.) how RC etwork ued to form filter futio. V it) R + v Rt) - C + v t) - Figure Q.) i) ii)

More information

CHAPTER 15 Wave Motion. 1. The speed of the wave is

CHAPTER 15 Wave Motion. 1. The speed of the wave is CHAPTER 15 Wave Motion 1. The speed of the wave is v = fλ = λ/t = (9.0 m)/(4.0 s) = 2.3 m/s. 7. We find the tension from the speed of the wave: v = [F T /(m/l)] 1/2 ; (4.8 m)/(0.85 s) = {F T /[(0.40 kg)/(4.8

More information

sin m a d F m d F m h F dy a dy a D h m h m, D a D a c1cosh c3cos 0

sin m a d F m d F m h F dy a dy a D h m h m, D a D a c1cosh c3cos 0 Q1. The free vibrtio of the plte is give by By ssumig h w w D t, si cos w W x y t B t Substitutig the deflectio ito the goverig equtio yields For the plte give, the mode shpe W hs the form h D W W W si

More information

Automatic Control Systems

Automatic Control Systems Automatic Cotrol Sytem Lecture-5 Time Domai Aalyi of Orer Sytem Emam Fathy Departmet of Electrical a Cotrol Egieerig email: emfmz@yahoo.com Itrouctio Compare to the implicity of a firt-orer ytem, a eco-orer

More information

Physics 2101 S c e t c i cti n o 3 n 3 March 31st Announcements: Quiz today about Ch. 14 Class Website:

Physics 2101 S c e t c i cti n o 3 n 3 March 31st Announcements: Quiz today about Ch. 14 Class Website: Physics 2101 Section 3 March 31 st Announcements: Quiz today about Ch. 14 Class Website: http://www.phys.lsu.edu/classes/spring2010/phys2101 3/ http://www.phys.lsu.edu/~jzhang/teaching.html Simple Harmonic

More information

SHOCK RESPONSE SPECTRUM ANALYSIS VIA THE FINITE ELEMENT METHOD Revision C

SHOCK RESPONSE SPECTRUM ANALYSIS VIA THE FINITE ELEMENT METHOD Revision C SHOCK RESPONSE SPECTRUM ANALYSIS VIA THE FINITE ELEMENT METHOD Revision C By Tom Irvine Email: tomirvine@aol.com November 19, 2010 Introduction This report gives a method for determining the response of

More information

Date: 1 April (1) The only reference material you may use is one 8½x11 crib sheet and a calculator.

Date: 1 April (1) The only reference material you may use is one 8½x11 crib sheet and a calculator. PH1140: Oscillations and Waves Name: Solutions Conference: Date: 1 April 2005 EXAM #1: D2005 INSTRUCTIONS: (1) The only reference material you may use is one 8½x11 crib sheet and a calculator. (2) Show

More information

Topic 4 Fourier Series. Today

Topic 4 Fourier Series. Today Topic 4 Fourier Series Toy Wves with repetig uctios Sigl geertor Clssicl guitr Pio Ech istrumet is plyig sigle ote mile C 6Hz) st hrmoic hrmoic 3 r hrmoic 4 th hrmoic 6Hz 5Hz 783Hz 44Hz A sigle ote will

More information

Old Exams - Questions Ch-16

Old Exams - Questions Ch-16 Old Exams - Questions Ch-16 T081 : Q1. The displacement of a string carrying a traveling sinusoidal wave is given by: y( x, t) = y sin( kx ω t + ϕ). At time t = 0 the point at x = 0 m has a displacement

More information

kg meter ii) Note the dimensions of ρ τ are kg 2 velocity 2 meter = 1 sec 2 We will interpret this velocity in upcoming slides.

kg meter ii) Note the dimensions of ρ τ are kg 2 velocity 2 meter = 1 sec 2 We will interpret this velocity in upcoming slides. II. Generalizing the 1-dimensional wave equation First generalize the notation. i) "q" has meant transverse deflection of the string. Replace q Ψ, where Ψ may indicate other properties of the medium that

More information

Date: 31 March (1) The only reference material you may use is one 8½x11 crib sheet and a calculator.

Date: 31 March (1) The only reference material you may use is one 8½x11 crib sheet and a calculator. PH1140: Oscillations and Waves Name: SOLUTIONS AT END Conference: Date: 31 March 2005 EXAM #1: D2006 INSTRUCTIONS: (1) The only reference material you may use is one 8½x11 crib sheet and a calculator.

More information

SOLUTIONS OF RECURRENCES WITH VARIABLE COEFFICIENTS FOR SLIDE BEARING WEAR DETERMINATION

SOLUTIONS OF RECURRENCES WITH VARIABLE COEFFICIENTS FOR SLIDE BEARING WEAR DETERMINATION Jourl o KONE Powertri Trsport Vol. 0 No. 03 OLUTION OF REURRENE ITH VARIABLE OEFFIIENT FOR LIDE BEARING EAR DETERMINATION Krzyszto ierzcholsi Techicl Uiversity o Koszli Istitute o Techology Euctio iecich

More information

Thomas Whitham Sixth Form

Thomas Whitham Sixth Form Thoms Whithm ith Form Pure Mthemtis Uit lger Trigoometr Geometr lulus lger equees The ifiite sequee of umers U U U... U... is si to e () overget if U L fiite limit s () iverget to if U s Emple The sequee...

More information

Each of these functions represents a signal in terms of its spectral components in the frequency domain.

Each of these functions represents a signal in terms of its spectral components in the frequency domain. N INTRODUCTION TO SPECTRL FUNCTIONS Revision B By Tom Irvine Email: tomirvine@aol.com March 3, 000 INTRODUCTION This tutorial presents the Fourier transform. It also discusses the power spectral density

More information

Direct Fatigue Damage Spectrum Calculation for a Shock Response Spectrum

Direct Fatigue Damage Spectrum Calculation for a Shock Response Spectrum Direct Fatigue Damage Spectrum Calculation for a Shock Response Spectrum By Tom Irvine Email: tom@vibrationdata.com June 25, 2014 Introduction A fatigue damage spectrum (FDS) was calculated for a number

More information

ME203 Section 4.1 Forced Vibration Response of Linear System Nov 4, 2002 (1) kx c x& m mg

ME203 Section 4.1 Forced Vibration Response of Linear System Nov 4, 2002 (1) kx c x& m mg ME3 Setio 4.1 Fored Vibratio Respose of Liear Syste Nov 4, Whe a liear ehaial syste is exited by a exteral fore, its respose will deped o the for of the exitatio fore F(t) ad the aout of dapig whih is

More information

Thursday, August 4, 2011

Thursday, August 4, 2011 Chapter 16 Thursday, August 4, 2011 16.1 Springs in Motion: Hooke s Law and the Second-Order ODE We have seen alrealdy that differential equations are powerful tools for understanding mechanics and electro-magnetism.

More information

ENGI 2422 Appendix A Formulæ Page A-01

ENGI 2422 Appendix A Formulæ Page A-01 ENGI 4 Appei A Formlæ Pge A- ENGI 4 Egieerig Mhemi Poiiliie for or Forml Shee Yo m ele iem from hi ome for pleme o or forml hee. However eigig or ow forml hee e vlle reviio eerie i ielf.. Fmel Eqio of

More information

Chapter 3 Mathematical Methods

Chapter 3 Mathematical Methods Chapter 3 Mathematical Methods Slides to accompany lectures in Vibro-Acoustic Design in Mechanical Systems 0 by D. W. Herrin Department of Mechanical Engineering Lexington, KY 40506-0503 Tel: 859-8-0609

More information

MEEN 363. EXAMPLE of ANALYSIS (1 DOF) Luis San Andrés

MEEN 363. EXAMPLE of ANALYSIS (1 DOF) Luis San Andrés MEEN 363. EAMPLE of ANALYSIS (1 DOF) Luis San Anrés Objectives: a) To erive EOM for a 1-DOF (one egree of freeom) system b) To unerstan concept of static equilibrium c) To learn the correct usage of physical

More information

AUTOMATIC CONTROL SYSTEMS

AUTOMATIC CONTROL SYSTEMS 9 HE UO ONROL SYSES OSVE SLE RELZONS OF ONNUOUS-E LNER SYSES deuz Kzore trt: he rolem for exitee d determitio of the et of oitive ymtotilly tle reliztio of roer trfer futio of lier otiuou-time ytem i formulted

More information

Truncation Errors Numerical Integration Multiple Support Excitation

Truncation Errors Numerical Integration Multiple Support Excitation Errors Numerical Integration Multiple Support Excitation http://intranet.dica.polimi.it/people/boffi-giacomo Dipartimento di Ingegneria Civile Ambientale e Territoriale Politecnico di Milano April 10,

More information

BENDING FREQUENCIES OF BEAMS, RODS, AND PIPES Revision S

BENDING FREQUENCIES OF BEAMS, RODS, AND PIPES Revision S BENDING FREQUENCIES OF BEAMS, RODS, AND PIPES Revisio S By Tom Irvie Email: tom@vibratioata.com November, Itrouctio The fuametal frequecies for typical beam cofiguratios are give i Table. Higher frequecies

More information

Section 4.9; Section 5.6. June 30, Free Mechanical Vibrations/Couple Mass-Spring System

Section 4.9; Section 5.6. June 30, Free Mechanical Vibrations/Couple Mass-Spring System Section 4.9; Section 5.6 Free Mechanical Vibrations/Couple Mass-Spring System June 30, 2009 Today s Session Today s Session A Summary of This Session: Today s Session A Summary of This Session: (1) Free

More information

Dynamics of Structures: Theory and Analysis

Dynamics of Structures: Theory and Analysis 1. Free vibrations 2. Forced vibrations 3. Transient response 4. Damping mechanisms Dynamics of Structures: Theory and Analysis Steen Krenk Technical University of Denmark 5. Modal analysis I: Basic idea

More information

2C9 Design for seismic and climate changes. Jiří Máca

2C9 Design for seismic and climate changes. Jiří Máca 2C9 Design for seismic and climate changes Jiří Máca List of lectures 1. Elements of seismology and seismicity I 2. Elements of seismology and seismicity II 3. Dynamic analysis of single-degree-of-freedom

More information

Data Compression Techniques (Spring 2012) Model Solutions for Exercise 4

Data Compression Techniques (Spring 2012) Model Solutions for Exercise 4 58487 Dt Compressio Tehiques (Sprig 0) Moel Solutios for Exerise 4 If you hve y fee or orretios, plese ott jro.lo t s.helsii.fi.. Prolem: Let T = Σ = {,,, }. Eoe T usig ptive Huffm oig. Solutio: R 4 U

More information

ME242 Vibrations- Mechatronics Experiment

ME242 Vibrations- Mechatronics Experiment ME4 Vibratios- Mechatroics Experimet Daiel. S. Stutts Associate Professor of Mechaical Egieerig ad Egieerig Mechaics Wedesday, September 16, 009 Purpose of Experimet Lear some basic cocepts i vibratios

More information

is a What you Hear The Pressure Wave sets the Ear Drum into Vibration.

is a What you Hear The Pressure Wave sets the Ear Drum into Vibration. is a What you Hear The ear converts sound energy to mechanical energy to a nerve impulse which is transmitted to the brain. The Pressure Wave sets the Ear Drum into Vibration. electroencephalogram v S

More information

Section 11.5 Notes Page Partial Fraction Decomposition. . You will get: +. Therefore we come to the following: x x

Section 11.5 Notes Page Partial Fraction Decomposition. . You will get: +. Therefore we come to the following: x x Setio Notes Pge Prtil Frtio Deompositio Suppose we were sked to write the followig s sigle frtio: We would eed to get ommo deomitors: You will get: Distributig o top will give you: 8 This simplifies to:

More information

Vibrations and Waves MP205, Assignment 4 Solutions

Vibrations and Waves MP205, Assignment 4 Solutions Vibrations and Waves MP205, Assignment Solutions 1. Verify that x = Ae αt cos ωt is a possible solution of the equation and find α and ω in terms of γ and ω 0. [20] dt 2 + γ dx dt + ω2 0x = 0, Given x

More information

ME260W Mid-Term Exam Instructor: Xinyu Huang Date: Mar

ME260W Mid-Term Exam Instructor: Xinyu Huang Date: Mar ME60W Mid-Term Exam Istrutor: Xiyu Huag Date: Mar-03-005 Name: Grade: /00 Problem. A atilever beam is to be used as a sale. The bedig momet M at the gage loatio is P*L ad the strais o the top ad the bottom

More information

STRUCTURAL PARAMETERS IDENTIFICATION BASED ON DIFFERENTIAL EVOLUTION AND PARTICLE SWARM OPTIMIZATION

STRUCTURAL PARAMETERS IDENTIFICATION BASED ON DIFFERENTIAL EVOLUTION AND PARTICLE SWARM OPTIMIZATION STRUCTURAL PARAMETERS IDENTIFICATION BASED ON DIFFERENTIAL EVOLUTION AND PARTICLE SWARM OPTIMIZATION Wang Yanwei MEE08167 Supervisor : Xue Songtao Tang Hesheng ABSTRACT Civil structures always suffer many

More information

APPENDIX 2 LAPLACE TRANSFORMS

APPENDIX 2 LAPLACE TRANSFORMS APPENDIX LAPLACE TRANSFORMS Thi ppendix preent hort introduction to Lplce trnform, the bic tool ued in nlyzing continuou ytem in the frequency domin. The Lplce trnform convert liner ordinry differentil

More information

Non-stationary Ambient Response Data Analysis for Modal Identification Using Improved Random Decrement Technique

Non-stationary Ambient Response Data Analysis for Modal Identification Using Improved Random Decrement Technique 9th International Conference on Advances in Experimental Mechanics Non-stationary Ambient Response Data Analysis for Modal Identification Using Improved Random Decrement Technique Chang-Sheng Lin and Tse-Chuan

More information

Application of Simple Harmonics Modeling a Shock

Application of Simple Harmonics Modeling a Shock Undergraduate Journal of Mathematical Modeling: One + Two Volume 8 2017 Fall 2017 Issue 1 Article 1 Application of Simple Harmonics Modeling a Shock Kai Raymond University of South Florida Advisors: Thomas

More information

f (x)dx = f(b) f(a). a b f (x)dx is the limit of sums

f (x)dx = f(b) f(a). a b f (x)dx is the limit of sums Green s Theorem If f is funtion of one vrible x with derivtive f x) or df dx to the Fundmentl Theorem of lulus, nd [, b] is given intervl then, ording This is not trivil result, onsidering tht b b f x)dx

More information

5 Trigonometric Functions

5 Trigonometric Functions 5 Trigonometric Functions 5.1 The Unit Circle Definition 5.1 The unit circle is the circle of radius 1 centered at the origin in the xyplane: x + y = 1 Example: The point P Terminal Points (, 6 ) is on

More information

Prob. 1 SDOF Structure subjected to Ground Shaking

Prob. 1 SDOF Structure subjected to Ground Shaking Prob. 1 SDOF Structure subjected to Ground Shaking What is the maximum relative displacement and the amplitude of the total displacement of a SDOF structure subjected to ground shaking? magnitude of ground

More information

Oscillatory Motion and Wave Motion

Oscillatory Motion and Wave Motion Oscillatory Motion and Wave Motion Oscillatory Motion Simple Harmonic Motion Wave Motion Waves Motion of an Object Attached to a Spring The Pendulum Transverse and Longitudinal Waves Sinusoidal Wave Function

More information

1. [30] Y&F a) Assuming a small angle displacement θ max < 0.1 rad, the period is very nearly

1. [30] Y&F a) Assuming a small angle displacement θ max < 0.1 rad, the period is very nearly PH1140 D09 Homework 3 Solution 1. [30] Y&F 13.48. a) Assuming a small angle displacement θ max < 0.1 rad, the period is very nearly T = π L =.84 s. g b) For the displacement θ max = 30 = 0.54 rad we use

More information

APPLICATIONS OF SECOND-ORDER DIFFERENTIAL EQUATIONS

APPLICATIONS OF SECOND-ORDER DIFFERENTIAL EQUATIONS APPLICATIONS OF SECOND-ORDER DIFFERENTIAL EQUATIONS Second-order linear differential equations have a variety of applications in science and engineering. In this section we explore two of them: the vibration

More information

Problem 1. Problem Engineering Dynamics Problem Set 9--Solution. Find the equation of motion for the system shown with respect to:

Problem 1. Problem Engineering Dynamics Problem Set 9--Solution. Find the equation of motion for the system shown with respect to: 2.003 Egieerig Dyamics Problem Set 9--Solutio Problem 1 Fid the equatio of motio for the system show with respect to: a) Zero sprig force positio. Draw the appropriate free body diagram. b) Static equilibrium

More information

COURSE OUTLINE. Introduction Signals and Noise Filtering: OPF2 Optimum Filtering2 Sensors and associated electronics. Sensors, Signals and Noise 1

COURSE OUTLINE. Introduction Signals and Noise Filtering: OPF2 Optimum Filtering2 Sensors and associated electronics. Sensors, Signals and Noise 1 ensors, ignals and Noise 1 OURE OUTINE Introduction ignals and Noise Filtering: OPF Optimum Filtering ensors and associated electronics ignal Recovery, 017/018 Optimum filter Optimum Filtering for High-Impedae

More information

AMS 216 Stochastic Differential Equations Lecture 03 Copyright by Hongyun Wang, UCSC

AMS 216 Stochastic Differential Equations Lecture 03 Copyright by Hongyun Wang, UCSC Lecture 03 Copyright by Hongyun Wang, UCSC Review of probability theory (Continued) We show that Sum of independent normal random variable normal random variable Characteristic function (CF) of a random

More information

ENGI 9420 Lecture Notes 7 - Fourier Series Page 7.01

ENGI 9420 Lecture Notes 7 - Fourier Series Page 7.01 ENGI 940 ecture Notes 7 - Fourier Series Pge 7.0 7. Fourier Series nd Fourier Trnsforms Fourier series hve multiple purposes, including the provision of series solutions to some liner prtil differentil

More information

Homework 6: Forced Vibrations Due Friday April 6, 2018

Homework 6: Forced Vibrations Due Friday April 6, 2018 EN40: Dyais ad Vibratios Hoework 6: Fored Vibratios Due Friday April 6, 018 Shool of Egieerig Brow Uiversity 1. The vibratio isolatio syste show i the figure has 0kg, k 19.8 kn / 1.59 kns / If the base

More information

Analysis of a Two-Echelon Inventory Model with Lost Sales and Stochastic Demand using Continuous-Time Markov chain

Analysis of a Two-Echelon Inventory Model with Lost Sales and Stochastic Demand using Continuous-Time Markov chain Poceedig of te tetiol ofeece o dutil Egieeig d Opetio Mgemet li doei Juy 7 9 Alyi of Two-Ecelo vetoy Model wit Lot le d toctic Demd uig otiuou-time Mov ci m Vegi Fi d Roul Hi if Uiveity of Tecology Abtct

More information

Identification Methods for Structural Systems. Prof. Dr. Eleni Chatzi Lecture March, 2016

Identification Methods for Structural Systems. Prof. Dr. Eleni Chatzi Lecture March, 2016 Prof. Dr. Eleni Chatzi Lecture 4-09. March, 2016 Fundamentals Overview Multiple DOF Systems State-space Formulation Eigenvalue Analysis The Mode Superposition Method The effect of Damping on Structural

More information

Vibrations Qualifying Exam Study Material

Vibrations Qualifying Exam Study Material Vibrations Qualifying Exam Study Material The candidate is expected to have a thorough understanding of engineering vibrations topics. These topics are listed below for clarification. Not all instructors

More information

AA242B: MECHANICAL VIBRATIONS

AA242B: MECHANICAL VIBRATIONS AA242B: MECHANICAL VIBRATIONS 1 / 50 AA242B: MECHANICAL VIBRATIONS Undamped Vibrations of n-dof Systems These slides are based on the recommended textbook: M. Géradin and D. Rixen, Mechanical Vibrations:

More information

Fourier Series. Topic 4 Fourier Series. sin. sin. Fourier Series. Fourier Series. Fourier Series. sin. b n. a n. sin

Fourier Series. Topic 4 Fourier Series. sin. sin. Fourier Series. Fourier Series. Fourier Series. sin. b n. a n. sin Topic Fourier Series si Fourier Series Music is more th just pitch mplitue it s lso out timre. The richess o sou or ote prouce y musicl istrumet is escrie i terms o sum o umer o istict requecies clle hrmoics.

More information

S12 PHY321: Practice Final

S12 PHY321: Practice Final S12 PHY321: Practice Final Contextual information Damped harmonic oscillator equation: ẍ + 2βẋ + ω0x 2 = 0 ( ) ( General solution: x(t) = e [A βt 1 exp β2 ω0t 2 + A 2 exp )] β 2 ω0t 2 Driven harmonic oscillator

More information

EFFECTIVE MODAL MASS & MODAL PARTICIPATION FACTORS Revision F

EFFECTIVE MODAL MASS & MODAL PARTICIPATION FACTORS Revision F EFFECTIVE MODA MASS & MODA PARTICIPATION FACTORS Revision F By Tom Irvine Email: tomirvine@aol.com March 9, 1 Introduction The effective modal mass provides a method for judging the significance of a vibration

More information

Toolbox for Vibration Analysis of One-DOF Systems

Toolbox for Vibration Analysis of One-DOF Systems Toolbox for Vibration Analysis of One-DOF Systems Description of 1-DOF Systems Equation of motion Initial conitions m = mass or inertia (kg), c = amping coefficient (kg/s) k = spring coefficient or stiffness

More information

Dynamics of structures

Dynamics of structures Dynamics of structures 1.2 Viscous damping Luc St-Pierre October 30, 2017 1 / 22 Summary so far We analysed the spring-mass system and found that its motion is governed by: mẍ(t) + kx(t) = 0 k y m x x

More information

Final Exam April 30, 2013

Final Exam April 30, 2013 Final Exam Instructions: You have 120 minutes to complete this exam. This is a closed-book, closed-notes exam. You are allowed to use a calculator during the exam. Usage of mobile phones and other electronic

More information

The student will experimentally determine the parameters to represent the behavior of a damped oscillatory system of one degree of freedom.

The student will experimentally determine the parameters to represent the behavior of a damped oscillatory system of one degree of freedom. Practice 3 NAME STUDENT ID LAB GROUP PROFESSOR INSTRUCTOR Vibrations of systems of one degree of freedom with damping QUIZ 10% PARTICIPATION & PRESENTATION 5% INVESTIGATION 10% DESIGN PROBLEM 15% CALCULATIONS

More information

CHE302 LECTURE V LAPLACE TRANSFORM AND TRANSFER FUNCTION. Professor Dae Ryook Yang

CHE302 LECTURE V LAPLACE TRANSFORM AND TRANSFER FUNCTION. Professor Dae Ryook Yang CHE3 ECTURE V APACE TRANSFORM AND TRANSFER FUNCTION Profeor Dae Ryook Yang Fall Dept. of Chemical and Biological Engineering Korea Univerity CHE3 Proce Dynamic and Control Korea Univerity 5- SOUTION OF

More information

Oscillation as Rotation. Rate of rotation: ω degrees/sec

Oscillation as Rotation. Rate of rotation: ω degrees/sec Oscillation as Rotation Rate of rotation: ω degrees/sec Oscillation as Rotation Rate of rotation: ω degrees/sec Oscillation as Rotation Oscillation as Rotation y x Oscillation as Rotation y R x Oscillation

More information

ME 375 EXAM #1 Friday, March 13, 2015 SOLUTION

ME 375 EXAM #1 Friday, March 13, 2015 SOLUTION ME 375 EXAM #1 Friday, March 13, 2015 SOLUTION PROBLEM 1 A system is made up of a homogeneous disk (of mass m and outer radius R), particle A (of mass m) and particle B (of mass m). The disk is pinned

More information

RESPONSE PREDICTION OF STRUCTURAL SYSTEM SUBJECT TO EARTHQUAKE MOTIONS USING ARTIFICIAL NEURAL NETWORK

RESPONSE PREDICTION OF STRUCTURAL SYSTEM SUBJECT TO EARTHQUAKE MOTIONS USING ARTIFICIAL NEURAL NETWORK ASIAN JOURNAL OF CIVIL ENGINEERING (BUILDING AND HOUSING) VOL. 7, NO. 3 (006) PAGES 301-308 RESPONSE PREDICTION OF STRUCTURAL SYSTEM SUBJECT TO EARTHQUAKE MOTIONS USING ARTIFICIAL NEURAL NETWORK S. Chakraverty

More information

UNIT #5 SEQUENCES AND SERIES COMMON CORE ALGEBRA II

UNIT #5 SEQUENCES AND SERIES COMMON CORE ALGEBRA II Awer Key Nme: Dte: UNIT # SEQUENCES AND SERIES COMMON CORE ALGEBRA II Prt I Quetio. For equece defied by f? () () 08 6 6 f d f f, which of the followig i the vlue of f f f f f f 0 6 6 08 (). I the viul

More information

Unit 5 PreCalculus Review

Unit 5 PreCalculus Review Class: Date: Unit 5 PreCalculus Review Multiple Choice Identify the choice that best completes the statement or answers the question. 1. Find the terminal point P (x, y) on the unit circle determined by

More information

Goldstein Problem 2.17 (3 rd ed. # 2.18)

Goldstein Problem 2.17 (3 rd ed. # 2.18) Goldstein Problem.7 (3 rd ed. #.8) The geometry of the problem: A particle of mass m is constrained to move on a circular hoop of radius a that is vertically oriented and forced to rotate about the vertical

More information

TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS

TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS UNIT-I PARTIAL DIFFERENTIAL EQUATIONS PART-A. Elimit th ritrry ott & from = ( + )(y + ) Awr: = ( + )(y + ) Diff prtilly w.r.to & y hr p & q y p = (y + ) ;

More information

Chapter 13. Hooke s Law: F = - kx Periodic & Simple Harmonic Motion Springs & Pendula Waves Superposition. Next Week!

Chapter 13. Hooke s Law: F = - kx Periodic & Simple Harmonic Motion Springs & Pendula Waves Superposition. Next Week! Chapter 13 Hooke s Law: F = - kx Periodic & Simple Harmonic Motion Springs & Pendula Waves Superposition Next Week! Review Physics 2A: Springs, Pendula & Circular Motion Elastic Systems F = kx Small Vibrations

More information

X(t)e 2πi nt t dt + 1 T

X(t)e 2πi nt t dt + 1 T HOMEWORK 31 I) Use the Fourier-Euler formulae to show that, if X(t) is T -periodic function which admits a Fourier series decomposition X(t) = n= c n exp (πi n ) T t, then (1) if X(t) is even c n are all

More information

Physics 1C. Lecture 13B

Physics 1C. Lecture 13B Physics 1C Lecture 13B Speed of Sound! Example values (m/s): Description of a Sound Wave! A sound wave may be considered either a displacement wave or a pressure wave! The displacement of a small element

More information

Lecture 5 Frequency Response of FIR Systems (III)

Lecture 5 Frequency Response of FIR Systems (III) EE3054 Signal and Sytem Lecture 5 Frequency Repone of FIR Sytem (III Yao Wang Polytechnic Univerity Mot of the lide included are extracted from lecture preentation prepared by McClellan and Schafer Licene

More information

Simple harmonic motion the motion of springs is a very important topic in physics.

Simple harmonic motion the motion of springs is a very important topic in physics. Chapter 11 Potential and Kinetic Energy Together: Simple Harmonic Motion In This Chapter Using Hooke s law Working with simple harmonic motion Calculating simple harmonic motion velcoity Finding simple

More information

Theoretical Basis of Modal Analysis

Theoretical Basis of Modal Analysis American Journal of Mechanical Engineering, 03, Vol., No. 7, 73-79 Available online at http://pubs.sciepub.com/ajme//7/4 Science and Education Publishing DOI:0.69/ajme--7-4 heoretical Basis of Modal Analysis

More information

2. Determine whether the following pair of functions are linearly dependent, or linearly independent:

2. Determine whether the following pair of functions are linearly dependent, or linearly independent: Topics to be covered on the exam include: Recognizing, and verifying solutions to homogeneous second-order linear differential equations, and their corresponding Initial Value Problems Recognizing and

More information

Time Response Analysis (Part II)

Time Response Analysis (Part II) Time Response Analysis (Part II). A critically damped, continuous-time, second order system, when sampled, will have (in Z domain) (a) A simple pole (b) Double pole on real axis (c) Double pole on imaginary

More information

TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS

TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS TRANSFORMS AND PARTIAL DIFFERENTIAL EQUATIONS UNIT-I PARTIAL DIFFERENTIAL EQUATIONS PART-A. Elimit th ritrry ott & from = ( + )(y + ) = ( + )(y + ) Diff prtilly w.r.to & y hr p & q p = (y + ) ; q = ( +

More information

WAVES CP4 REVISION LECTURE ON. The wave equation. Traveling waves. Standing waves. Dispersion. Phase and group velocities.

WAVES CP4 REVISION LECTURE ON. The wave equation. Traveling waves. Standing waves. Dispersion. Phase and group velocities. CP4 REVISION LECTURE ON WAVES The wave equation. Traveling waves. Standing waves. Dispersion. Phase and group velocities. Boundary effects. Reflection and transmission of waves. !"#$%&''(%)*%+,-.%/%+,01%

More information