Determinationn of gasket load drop at welding neck flange joints operating at medium high temperature

Size: px
Start display at page:

Download "Determinationn of gasket load drop at welding neck flange joints operating at medium high temperature"

Transcription

1 Determnatonn of gasket load drop at large sze weldng neck flange onts operatng at medum hgh temperature A. agy * and B. Dudnszky * * Department of Buldng Servces and Process Engneerng, aculty of Mechancal Engneerng, Budapest Unversty of Technology and Economcs, Budapest, Hungary drnagyandras@freemal.hu, dudnszky@vegyelgep.bme.hu Abstract ths paper nvestgates the development of loosenng at flange onts owng to creep and relaxaton of gaskets at medum hgh temperature. The model presented here s able to descrbe the nteracton of gasket and flange addton to the vscoelastc behavor of non-metallc gasket. The tme-dependent materal characterstcs of the nvestgated gasket [5] were determnedd by standard tests whlst the relablty and precsenesss of the derved equatons are proved by test results. The paper deals wth the dmensonng of flange onts on leak tghtness operatng at medum hgh temperatures. I. ITRODUCTIO gure. Sketch of the nvestgated flange ont The reducton of gasket load at flange onts operatng at medum-hgh temperature s manly due to loosenng effects that arse from nternal pressure and addtonal external moments and forces [3] as well as from creep and relaxaton of the non-metallc gasket materals. Ths drop n gasket load arsng from the nternal pressure and external loads s dscussed n the lterature by lnear and non-lnear gasket model [4]. The only dffculty n determnng the resdual gasket load under pressurzed condton s the tme-dependent creep and relaxaton of non-metallc gasket. There was sgnfcant work done already n the 95 s to determne, by means of test, the tme-dependent characterstcs of gasket [], []. At that tme a test method sutable to determne the long term load carryng capacty of gasket had been nvented and standardzed, and ths method s stll n use [7], [8]. The strength characterstcs determned by ths way cannot be regarded as pure materal characterstcs s of the gasket, because ths s nfluenced by the nteractonn between the bolted ont and the gasket. Thus the prevous mentoned test method s sutable to compare dfferent gasket materal. II. AALITICAL MODEL O LAE JOIT The model presented heree enables the mentoned standardzed method to determned the true characterstcs of the gasket materals. Usng the newly developed model and applyng the mentoned test method, the tme dependent characterstcs (that s creep and relaxaton of gasket materal can be predcted atany arbtrary ont. The basc assumpton of the model presentng the correlaton of actng loads and caused dsplacements are the follows: Heat actng of the flange onts comes only from the medum to be sealed, characterzed by ts pressure p and temperature T U. The effect of the yeld strength reducton and the change of elastcty modulus owng to the temperature ncrement both at flange and bolts can be neglected. Creep and relaxaton at flange and at bolts can also be neglected, so the rotatonal sprng stffness of flange as well as sprng stffness of bolts are ndependent from tme and from dsplacements. Another underlyng assumpton of the model s that durng equalzaton of temperatures among dfferent elements of the flange ont nternal forces and stresses are generated by the dfferent heat expanson not nfluencng the creep and relaxaton of gasket, therefore the two phenomena can be nvestgated ndependently from each other. At flange ont presented n ths g., the dsplacements caused by smultaneous heat and mechancal loads and the changes of nternal forces [4], [6] wll happen accordng to the g., shows.

2 gure. Dsplacements and changes of nternal forces owng to the smultaneous heat and mechancal loads In ths fgure the dsplacements W and angular dsplacements κ can be seen whch are together responsble for the reducton of gasket load. The flanges themselves are replaced by corner rgd skeletons, havng and rotatonal sprng stffness. As the fgure shows both the dsplacements and angular dsplacements and gasket load drop can be dvded nto parts and they can be nvestgated separately from each other. In ths fgure mean the gasket load drop arsng V P from the pressure nduced header end load P and s the unknown gasket load drop caused by creep and relaxaton of the gasket. In order to nvestgate the loosenng effect caused by gasket relaxaton, the gasket should be modelled and the nteracton of gasket and flange should be analysed. To create ts vscoelastc model, the typcal non-lnear characterstcs of non-metallc gasket materals should be taken nto consderaton, as well as the fact that durng the standardzed relaxaton test of frequently appled gasket materals non-zero resdual compresson stress appears. The developed rheologcal analogue model whch s the bass of further nvestgatons can be seen n the next g. 3. As the fgure shows the model fulfls both requrements. The non-lnear characterstcs of the gasket are produced by the sprngs of the elementary Maxwell-model connected n parallel, and the nteracton of gasket and flange s symbolzed by the sprng connected to the gasket model havng the modulus calculated from ths equaton ( where A s the surface area whle s the thckness of the gasket, s the sprng stffness of bolts. ε V A U = = kc + h V [ ( U U + z Ths fgure presents the state belongng to the startng compresson stress. The determnaton of the total decrease of gasket load orgnated from the relaxaton of the gasket s possble only n several steps usng the equatons belongng to the dfferent lnearzed ranges of the compresson characterstc curve. The g. 4, shows the range. of the loosenng process. In ths range the gasket compresson stress can be expressed as a functon of tme wth the followng dfferental equaton (. + E d ( + + E V + E d V = dt dt ( E gure 3. Rheologcal analogue model of flange ont gure 4. The range. of the relaxaton process = = ] h (

3 Its soluton regardng the boundary condtons s: V ( t = = + ( E E E + ( E + E E ε = + E + E ( ( [ exp λ t ] where ε = means the total compressons of = the gasket and the coeffcent λ can be calculated from ths equaton (4. λ = = [ + ( ] + E E E = ( + E The actual range of valdty for ths functon s a short tme perod t t where ts upper lmt s determned by equaton (5. t = = = ( + E [ + ( + ] E E E (3 (4 ε ln (5 ε The relaxaton and creep of the gasket occurrng durng ths tme perod can be calculated usng these equaton: V V E = = + E + E V ( t ( V = ε = (7 The resultant relaxaton and creep of the gasket consderng the total loosenng process can be calculated by ths way and fnally the followng equatons (8, (9 can be obtaned. E nf ( = = V = V = = + E + E ( (6 (8 d dt V d = dt t= t V t= ( Substtutng ranges of the relaxaton curve after smplfyng the followng recursve formulae can be found. E + E = = + E ( = = E = The factor of vscous flud element at the begnnng as well as sprng constants can be determned by tests. These tests gve the compresson stress-stran characterstc curve that s to be appled parallel to the standardzed long term load carryng capacty test of the gasket whch can be determned by the earler mentoned test method. nowng these test results the searched characterstcs of the model can be calculated usng equatons (, (3, (4. E E nf ( nf ( ( ˆ ˆ V V ˆ nf ( nf ( ( ˆ ˆ V V E + E = ( + ( ( + ˆ ( ( ( E nf nf + ˆ ˆ ˆ V V nf ˆ V (3 = E E ε = d ˆ V (4 = ˆ + E dt t= where devce and relaxaton. assgn the relatve modulus of the testng ˆ V symbolse the measured resultant III. TEST AD CALCULATED RESULT Several experments were carred out to prove the relablty and applcablty of the vscoelastc model. rst several thcknesses of gaskets from dfferent manufacturers were nvestgated to determne characterstcs of the gasket materals ncludng the tme dependent propertes. nf ( nf ( ε = = V = V The characterstcs of sprngs and vscous flud elements can be determned accordng to the followng consderaton. The values of characterstcs of vscous flud element gves the requred contnuty of the resultant relaxaton curve. V (9

4 gure 7.Measured Measured and calculatedresultantrelaxatonsas a functon of pretghtenngatdfferenttypes of hg = mmthckgasketat5 mm C gure 5. ZWIC-type type unversal tensle machne ZWIC type unversal tensle machne equpped wth programmecontrolled heatng g. 5, was used to determne stress-stran stran characterstcs whle whl the tmedependent propertes were determned by BOSSER-type BOSSER standardzed test devce g. 6. gure 8.Measured and calculated resultant relaxatons at IT3 gaskets of several thcknesses as a functon of pretghtenng at 5 C Durng the experments the tme-dependence tme of the relaxaton axaton process takng place n the test devce was also recorded. The next two fgures g. 9,, shows the calculated and measured relaxaton curves belongng to gaskets skets made of REIZ and IT 3 materals wth. mm thckness. gure 6. BOSSER-type type standardzed test devce Usng the test results, the coeffcent for elastcty and vscous flud can already be numercally calculated. nowng the characterstcs of the model and choosng dfferent values for pretghtenngs the calculaton can ca be carred out. The calculaton refer to a ont havng equal stffness to the standardzed test devce used for determnaton of the tme dependent characterstcs, so the test devce gves a possblty to drectly check the precseness of the model. he measured and calculated values of resultant The relaxaton can be seen n the followng fgures. The g. 7, show the changes of calculated and measured resultant relaxaton at 5 C n the functon of pretghtenngs of dfferent gaskets wth equal. mm thckness. In ths fgure the contnuous curves present the measured results whle the dashed curves show the calculated values.g. 8, show the calculated and measured values of t at 5 C for dfferent fferent thckness of IT-type type gasket materal as a functon of pretghtenng. gure 9. Process of relaxaton at 5 C of REIZ AM34 type gaskets havng hg = mm thckness and pretghtened at dfferent values The test proved that ndependently of the type of gasket, the deal exponental losses characterstc of relaxatons could appear only nthe range of heat-keepng heat perod. d. Increasng pretghtenng n the t range of heatng up lead to the pressure losses on the t gasket growng bgger and bgger and they nclne from exponental one.ths Ths s the reason why at the begnnng of the heat keepng perod the calculated and measured results dffer.

5 gure. Process of relaxaton at 5 C of IT3 type gaskets havng hg = mm thckness and pretghtened at dfferent values gure 3. Temperature of flange and bolts along the heatng-up perod As the fgure shows the decrease of gasket surface pressure was recorded by measurng four bolts elongaton around the crcumference. Durng the test to keep the requred 5 C temperature nsde the vessel a 4 mm thck solaton was used along the whole body. The followng fgures(g. 3-7, show the measured and calculated results referrng to three dfferent type. mm thck gaskets. gure. Effect of heatng-up velocty on relaxaton process g., represents the effect of the heatng-up velocty on relaxaton n the range of heat-keepng. There are three dfferent relaxaton curves representng three dfferent heatng-up veloctes. Ths test were carred out on. mm thckness REIZ-type gasket at 5 C and the pretghtenngs was 3 Mpa. As the fgure show there s no sgnfcant effect of heatng-up velocty on the total gasket pressure losses, as sgnfcant changes (three tmes bgger n heatng-up velocty durng the test resulted n pressure losses dfferng slghtly from each other. gure 4. Measuredelongaton of boltsat5 CrefferngtoREIZ AM 34 Ong. 3, the dashed lne shows the program controlled temperature of flange rng near to the gasket whle the contnuous curve presents the temperature of the centre of bolts recorded by contact thermometer. gure. Sketch of the test devce To testfy the effect of geometrcal sze on the precseness of developed rheologcal analogue model, an automatcally heated test devce was manufactured whch can be seen n g.. gure 5. Total gasketsurfacepressuredrop (LIER 43

6 On g. 4, a typcal measured bolts elongaton can be seen n the functon of tme referrng to the REIZ AM type gasket.the thn curves shows the measured values whle the thck presents the calculated average. Consderng ths fgure t can be stated that the dfference among bolt elongatons are not to much less than % of the average.measurng the bolt elongaton we can calculate the changes of gasket surface pressure.nally n the last three fgures (g. 5-7, the comparson of calculated and measured results can be seen. gure 6. Total gasket surface pressure drop (REIZ AM 34 can be seen n the functon of pretghtenngs. The sngle symbols show the expermental, whle the contnuous and dashed curves present the calculated values by analytcal and EM model. IV. COCLUSIO The results of presented theoretcal and expermental nvestgatons allow the followng statements. Results calculated accordng to the developed model and test concernng gasket relaxaton n case of thckness less than 3. mm and pretghtenng less than 4 Mpa show good correlatons. The effect of gasket stress drop durng the heatng- dfferences at the up perod causes sgnfcant begnnng of nvestgatons between the calculated and measured relaxaton curves n case of pretghtenng by more than Mpa. Concernng the future the developed model should be extended consderng by takng the creep and relaxaton of flanges and bolts nto account. REERECES [] S. Schwagerel, and E. rageloch, Prüfung von Wechdchtungen. BW 95, 4, [] A. E. Johnson, Creep and relaxaton of metals at elevated temperatures. Engneerng, 949, 68, [3] H. J. Bernhard, lange theory and the revsed Standard B. S.: 96-flanges and boltng for ppes, valves and fttngs Proc. Int. ech E., 963, 78, 7-3. [4] A. agy: Determnaton of the asket Load Drop at Large Sze Weldng eck lange Jonts n the Case of onlnear asket Model. Int. J. Pres. Ves. & Ppng. 67 ( [5] A. agy: Tme Dependng Characterstcs of asket at lange Jonts. Int. J. Pres. Ves. & Ppng. (997. [6] L. Varga, A. agy: Optmale orm und neue Analyse von lanschkonstruktonen. onstrukton 49, H. (997. [7] DI 593 Druchstandversuch an IT Dchtungsplatten (99. [8] BS 753: 99 Specfcaton for Compressed on-asbestos bre Jontng. Appendx B. gure 7. Total gasket surface pressure drop (LIER 443 In these fgures the total gasket surface pressure drop

EVALUATION OF THE VISCO-ELASTIC PROPERTIES IN ASPHALT RUBBER AND CONVENTIONAL MIXES

EVALUATION OF THE VISCO-ELASTIC PROPERTIES IN ASPHALT RUBBER AND CONVENTIONAL MIXES EVALUATION OF THE VISCO-ELASTIC PROPERTIES IN ASPHALT RUBBER AND CONVENTIONAL MIXES Manuel J. C. Mnhoto Polytechnc Insttute of Bragança, Bragança, Portugal E-mal: mnhoto@pb.pt Paulo A. A. Perera and Jorge

More information

Lifetime prediction of EP and NBR rubber seal by thermos-viscoelastic model

Lifetime prediction of EP and NBR rubber seal by thermos-viscoelastic model ECCMR, Prague, Czech Republc; September 3 th, 2015 Lfetme predcton of EP and NBR rubber seal by thermos-vscoelastc model Kotaro KOBAYASHI, Takahro ISOZAKI, Akhro MATSUDA Unversty of Tsukuba, Japan Yoshnobu

More information

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

THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS OF A TELESCOPIC HYDRAULIC CYLINDER SUBJECTED TO EULER S LOAD Journal of Appled Mathematcs and Computatonal Mechancs 7, 6(3), 7- www.amcm.pcz.pl p-issn 99-9965 DOI:.75/jamcm.7.3. e-issn 353-588 THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS

More information

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

Irregular vibrations in multi-mass discrete-continuous systems torsionally deformed (2) 4 48 Irregular vbratons n mult-mass dscrete-contnuous systems torsonally deformed Abstract In the paper rregular vbratons of dscrete-contnuous systems consstng of an arbtrary number rgd bodes connected

More information

Visco-Rubber Elastic Model for Pressure Sensitive Adhesive

Visco-Rubber Elastic Model for Pressure Sensitive Adhesive Vsco-Rubber Elastc Model for Pressure Senstve Adhesve Kazuhsa Maeda, Shgenobu Okazawa, Koj Nshgch and Takash Iwamoto Abstract A materal model to descrbe large deformaton of pressure senstve adhesve (PSA

More information

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE Analytcal soluton s usually not possble when exctaton vares arbtrarly wth tme or f the system s nonlnear. Such problems can be solved by numercal tmesteppng

More information

Indeterminate pin-jointed frames (trusses)

Indeterminate pin-jointed frames (trusses) Indetermnate pn-jonted frames (trusses) Calculaton of member forces usng force method I. Statcal determnacy. The degree of freedom of any truss can be derved as: w= k d a =, where k s the number of all

More information

OFF-AXIS MECHANICAL PROPERTIES OF FRP COMPOSITES

OFF-AXIS MECHANICAL PROPERTIES OF FRP COMPOSITES ICAMS 204 5 th Internatonal Conference on Advanced Materals and Systems OFF-AXIS MECHANICAL PROPERTIES OF FRP COMPOSITES VLAD LUPĂŞTEANU, NICOLAE ŢĂRANU, RALUCA HOHAN, PAUL CIOBANU Gh. Asach Techncal Unversty

More information

EPR Paradox and the Physical Meaning of an Experiment in Quantum Mechanics. Vesselin C. Noninski

EPR Paradox and the Physical Meaning of an Experiment in Quantum Mechanics. Vesselin C. Noninski EPR Paradox and the Physcal Meanng of an Experment n Quantum Mechancs Vesseln C Nonnsk vesselnnonnsk@verzonnet Abstract It s shown that there s one purely determnstc outcome when measurement s made on

More information

ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM

ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM An elastc wave s a deformaton of the body that travels throughout the body n all drectons. We can examne the deformaton over a perod of tme by fxng our look

More information

COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD

COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD Ákos Jósef Lengyel, István Ecsed Assstant Lecturer, Professor of Mechancs, Insttute of Appled Mechancs, Unversty of Mskolc, Mskolc-Egyetemváros,

More information

Lab 2e Thermal System Response and Effective Heat Transfer Coefficient

Lab 2e Thermal System Response and Effective Heat Transfer Coefficient 58:080 Expermental Engneerng 1 OBJECTIVE Lab 2e Thermal System Response and Effectve Heat Transfer Coeffcent Warnng: though the experment has educatonal objectves (to learn about bolng heat transfer, etc.),

More information

In this section is given an overview of the common elasticity models.

In this section is given an overview of the common elasticity models. Secton 4.1 4.1 Elastc Solds In ths secton s gven an overvew of the common elastcty models. 4.1.1 The Lnear Elastc Sold The classcal Lnear Elastc model, or Hooean model, has the followng lnear relatonshp

More information

Constitutive Modelling of Superplastic AA-5083

Constitutive Modelling of Superplastic AA-5083 TECHNISCHE MECHANIK, 3, -5, (01, 1-6 submtted: September 19, 011 Consttutve Modellng of Superplastc AA-5083 G. Gulano In ths study a fast procedure for determnng the constants of superplastc 5083 Al alloy

More information

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

Module 11 Design of Joints for Special Loading. Version 2 ME, IIT Kharagpur Module 11 Desgn o Jonts or Specal Loadng Verson ME, IIT Kharagpur Lesson 1 Desgn o Eccentrcally Loaded Bolted/Rveted Jonts Verson ME, IIT Kharagpur Instructonal Objectves: At the end o ths lesson, the

More information

APPENDIX 2 FITTING A STRAIGHT LINE TO OBSERVATIONS

APPENDIX 2 FITTING A STRAIGHT LINE TO OBSERVATIONS Unversty of Oulu Student Laboratory n Physcs Laboratory Exercses n Physcs 1 1 APPEDIX FITTIG A STRAIGHT LIE TO OBSERVATIOS In the physcal measurements we often make a seres of measurements of the dependent

More information

NUMERICAL DIFFERENTIATION

NUMERICAL DIFFERENTIATION NUMERICAL DIFFERENTIATION 1 Introducton Dfferentaton s a method to compute the rate at whch a dependent output y changes wth respect to the change n the ndependent nput x. Ths rate of change s called the

More information

3.1 Expectation of Functions of Several Random Variables. )' be a k-dimensional discrete or continuous random vector, with joint PMF p (, E X E X1 E X

3.1 Expectation of Functions of Several Random Variables. )' be a k-dimensional discrete or continuous random vector, with joint PMF p (, E X E X1 E X Statstcs 1: Probablty Theory II 37 3 EPECTATION OF SEVERAL RANDOM VARIABLES As n Probablty Theory I, the nterest n most stuatons les not on the actual dstrbuton of a random vector, but rather on a number

More information

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

ORIGIN 1. PTC_CE_BSD_3.2_us_mp.mcdx. Mathcad Enabled Content 2011 Knovel Corp. Clck to Vew Mathcad Document 2011 Knovel Corp. Buldng Structural Desgn. homas P. Magner, P.E. 2011 Parametrc echnology Corp. Chapter 3: Renforced Concrete Slabs and Beams 3.2 Renforced Concrete Beams -

More information

PERFORMANCE OF HEAVY-DUTY PLANETARY GEARS

PERFORMANCE OF HEAVY-DUTY PLANETARY GEARS THE INTERNATIONAL CONFERENCE OF THE CARPATHIAN EURO-REGION SPECIALISTS IN INDUSTRIAL SYSTEMS 6 th edton PERFORMANCE OF HEAVY-DUTY PLANETARY GEARS Attla Csobán, Mhály Kozma 1, 1 Professor PhD., Eng. Budapest

More information

Torsion Stiffness of Thin-walled Steel Beams with Web Holes

Torsion Stiffness of Thin-walled Steel Beams with Web Holes Torson Stffness of Thn-walled Steel Beams wth Web Holes MARTN HORÁČEK, JNDŘCH MELCHER Department of Metal and Tmber Structures Brno Unversty of Technology, Faculty of Cvl Engneerng Veveří 331/95, 62 Brno

More information

NUMERICAL RESULTS QUALITY IN DEPENDENCE ON ABAQUS PLANE STRESS ELEMENTS TYPE IN BIG DISPLACEMENTS COMPRESSION TEST

NUMERICAL RESULTS QUALITY IN DEPENDENCE ON ABAQUS PLANE STRESS ELEMENTS TYPE IN BIG DISPLACEMENTS COMPRESSION TEST Appled Computer Scence, vol. 13, no. 4, pp. 56 64 do: 10.23743/acs-2017-29 Submtted: 2017-10-30 Revsed: 2017-11-15 Accepted: 2017-12-06 Abaqus Fnte Elements, Plane Stress, Orthotropc Materal Bartosz KAWECKI

More information

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

Transfer Functions. Convenient representation of a linear, dynamic model. A transfer function (TF) relates one input and one output: ( ) system Transfer Functons Convenent representaton of a lnear, dynamc model. A transfer functon (TF) relates one nput and one output: x t X s y t system Y s The followng termnology s used: x y nput output forcng

More information

One Dimensional Axial Deformations

One Dimensional Axial Deformations One Dmensonal al Deformatons In ths secton, a specfc smple geometr s consdered, that of a long and thn straght component loaded n such a wa that t deforms n the aal drecton onl. The -as s taken as the

More information

Physics 181. Particle Systems

Physics 181. Particle Systems Physcs 181 Partcle Systems Overvew In these notes we dscuss the varables approprate to the descrpton of systems of partcles, ther defntons, ther relatons, and ther conservatons laws. We consder a system

More information

Finite Element Modelling of truss/cable structures

Finite Element Modelling of truss/cable structures Pet Schreurs Endhoven Unversty of echnology Department of Mechancal Engneerng Materals echnology November 3, 214 Fnte Element Modellng of truss/cable structures 1 Fnte Element Analyss of prestressed structures

More information

CHAPTER IV RESEARCH FINDING AND ANALYSIS

CHAPTER IV RESEARCH FINDING AND ANALYSIS CHAPTER IV REEARCH FINDING AND ANALYI A. Descrpton of Research Fndngs To fnd out the dfference between the students who were taught by usng Mme Game and the students who were not taught by usng Mme Game

More information

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

The optimal delay of the second test is therefore approximately 210 hours earlier than =2. THE IEC 61508 FORMULAS 223 The optmal delay of the second test s therefore approxmately 210 hours earler than =2. 8.4 The IEC 61508 Formulas IEC 61508-6 provdes approxmaton formulas for the PF for smple

More information

Answers Problem Set 2 Chem 314A Williamsen Spring 2000

Answers Problem Set 2 Chem 314A Williamsen Spring 2000 Answers Problem Set Chem 314A Wllamsen Sprng 000 1) Gve me the followng crtcal values from the statstcal tables. a) z-statstc,-sded test, 99.7% confdence lmt ±3 b) t-statstc (Case I), 1-sded test, 95%

More information

FUZZY FINITE ELEMENT METHOD

FUZZY FINITE ELEMENT METHOD FUZZY FINITE ELEMENT METHOD RELIABILITY TRUCTURE ANALYI UING PROBABILITY 3.. Maxmum Normal tress Internal force s the shear force, V has a magntude equal to the load P and bendng moment, M. Bendng moments

More information

NONLINEAR NATURAL FREQUENCIES OF A TAPERED CANTILEVER BEAM

NONLINEAR NATURAL FREQUENCIES OF A TAPERED CANTILEVER BEAM Advanced Steel Constructon Vol. 5, No., pp. 59-7 (9) 59 NONLINEAR NATURAL FREQUENCIES OF A TAPERED CANTILEVER BEAM M. Abdel-Jaber, A.A. Al-Qasa,* and M.S. Abdel-Jaber Department of Cvl Engneerng, Faculty

More information

NON LINEAR ANALYSIS OF STRUCTURES ACCORDING TO NEW EUROPEAN DESIGN CODE

NON LINEAR ANALYSIS OF STRUCTURES ACCORDING TO NEW EUROPEAN DESIGN CODE October 1-17, 008, Bejng, Chna NON LINEAR ANALYSIS OF SRUCURES ACCORDING O NEW EUROPEAN DESIGN CODE D. Mestrovc 1, D. Czmar and M. Pende 3 1 Professor, Dept. of Structural Engneerng, Faculty of Cvl Engneerng,

More information

ASSOCIATION POUR LA CERTIFICATION DES MATERIAUX ISOLANTS

ASSOCIATION POUR LA CERTIFICATION DES MATERIAUX ISOLANTS Revson ndex Date of mplementaton C 15/03/017 Techncal Specfcaton E ASSOCIATIO POUR LA CERTIFICATIO DES MATERIAUX ISOLATS 4, avenue du Recteur-Poncaré, 7578 Pars Cedex 16 Tel. 33.(0)1.64.68.84.97 Fax. 33.(0)1.64.68.83.45

More information

Lecture Note 3. Eshelby s Inclusion II

Lecture Note 3. Eshelby s Inclusion II ME340B Elastcty of Mcroscopc Structures Stanford Unversty Wnter 004 Lecture Note 3. Eshelby s Incluson II Chrs Wenberger and We Ca c All rghts reserved January 6, 004 Contents 1 Incluson energy n an nfnte

More information

Module 3 LOSSY IMAGE COMPRESSION SYSTEMS. Version 2 ECE IIT, Kharagpur

Module 3 LOSSY IMAGE COMPRESSION SYSTEMS. Version 2 ECE IIT, Kharagpur Module 3 LOSSY IMAGE COMPRESSION SYSTEMS Verson ECE IIT, Kharagpur Lesson 6 Theory of Quantzaton Verson ECE IIT, Kharagpur Instructonal Objectves At the end of ths lesson, the students should be able to:

More information

APPROXIMATE ANALYSIS OF RIGID PLATE LOADING ON ELASTIC MULTI-LAYERED SYSTEMS

APPROXIMATE ANALYSIS OF RIGID PLATE LOADING ON ELASTIC MULTI-LAYERED SYSTEMS 6th ICPT, Sapporo, Japan, July 008 APPROXIMATE ANALYSIS OF RIGID PLATE LOADING ON ELASTIC MULTI-LAYERED SYSTEMS James MAINA Prncpal Researcher, Transport and Infrastructure Engneerng, CSIR Bult Envronment

More information

JAB Chain. Long-tail claims development. ASTIN - September 2005 B.Verdier A. Klinger

JAB Chain. Long-tail claims development. ASTIN - September 2005 B.Verdier A. Klinger JAB Chan Long-tal clams development ASTIN - September 2005 B.Verder A. Klnger Outlne Chan Ladder : comments A frst soluton: Munch Chan Ladder JAB Chan Chan Ladder: Comments Black lne: average pad to ncurred

More information

DUE: WEDS FEB 21ST 2018

DUE: WEDS FEB 21ST 2018 HOMEWORK # 1: FINITE DIFFERENCES IN ONE DIMENSION DUE: WEDS FEB 21ST 2018 1. Theory Beam bendng s a classcal engneerng analyss. The tradtonal soluton technque makes smplfyng assumptons such as a constant

More information

LINEAR REGRESSION ANALYSIS. MODULE IX Lecture Multicollinearity

LINEAR REGRESSION ANALYSIS. MODULE IX Lecture Multicollinearity LINEAR REGRESSION ANALYSIS MODULE IX Lecture - 31 Multcollnearty Dr. Shalabh Department of Mathematcs and Statstcs Indan Insttute of Technology Kanpur 6. Rdge regresson The OLSE s the best lnear unbased

More information

Influential Factors Affecting Inherent Deformation during Plate Forming by Line Heating (Report 1)

Influential Factors Affecting Inherent Deformation during Plate Forming by Line Heating (Report 1) Transactons of JWRI, Vol.36 (2007), No.1 Influental Factors Affectng Inherent Deformaton durng Plate Formng by Lne Heatng (Report 1) The Effect of Plate Sze and Edge Effect VEGA Adan*, RASHED Sherf**,

More information

Solution Thermodynamics

Solution Thermodynamics Soluton hermodynamcs usng Wagner Notaton by Stanley. Howard Department of aterals and etallurgcal Engneerng South Dakota School of nes and echnology Rapd Cty, SD 57701 January 7, 001 Soluton hermodynamcs

More information

Chapter 11: Simple Linear Regression and Correlation

Chapter 11: Simple Linear Regression and Correlation Chapter 11: Smple Lnear Regresson and Correlaton 11-1 Emprcal Models 11-2 Smple Lnear Regresson 11-3 Propertes of the Least Squares Estmators 11-4 Hypothess Test n Smple Lnear Regresson 11-4.1 Use of t-tests

More information

Determination of the response distributions of cantilever beam under sinusoidal base excitation

Determination of the response distributions of cantilever beam under sinusoidal base excitation Journal of Physcs: Conference Seres OPEN ACCESS Determnaton of the response dstrbutons of cantlever beam under snusodal base exctaton To cte ths artcle: We Sun et al 13 J. Phys.: Conf. Ser. 448 11 Vew

More information

The internal structure of natural numbers and one method for the definition of large prime numbers

The internal structure of natural numbers and one method for the definition of large prime numbers The nternal structure of natural numbers and one method for the defnton of large prme numbers Emmanul Manousos APM Insttute for the Advancement of Physcs and Mathematcs 3 Poulou str. 53 Athens Greece Abstract

More information

FREQUENCY DISTRIBUTIONS Page 1 of The idea of a frequency distribution for sets of observations will be introduced,

FREQUENCY DISTRIBUTIONS Page 1 of The idea of a frequency distribution for sets of observations will be introduced, FREQUENCY DISTRIBUTIONS Page 1 of 6 I. Introducton 1. The dea of a frequency dstrbuton for sets of observatons wll be ntroduced, together wth some of the mechancs for constructng dstrbutons of data. Then

More information

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

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 Secton.. Moton.. The Materal Body and Moton hyscal materals n the real world are modeled usng an abstract mathematcal entty called a body. Ths body conssts of an nfnte number of materal partcles. Shown

More information

NON-CENTRAL 7-POINT FORMULA IN THE METHOD OF LINES FOR PARABOLIC AND BURGERS' EQUATIONS

NON-CENTRAL 7-POINT FORMULA IN THE METHOD OF LINES FOR PARABOLIC AND BURGERS' EQUATIONS IJRRAS 8 (3 September 011 www.arpapress.com/volumes/vol8issue3/ijrras_8_3_08.pdf NON-CENTRAL 7-POINT FORMULA IN THE METHOD OF LINES FOR PARABOLIC AND BURGERS' EQUATIONS H.O. Bakodah Dept. of Mathematc

More information

METHOD OF NETWORK RELIABILITY ANALYSIS BASED ON ACCURACY CHARACTERISTICS

METHOD OF NETWORK RELIABILITY ANALYSIS BASED ON ACCURACY CHARACTERISTICS METHOD OF NETWOK ELIABILITY ANALYI BAED ON ACCUACY CHAACTEITIC ławomr Łapńsk hd tudent Faculty of Geodesy and Cartography Warsaw Unversty of Technology ABTACT Measurements of structures must be precse

More information

#64. ΔS for Isothermal Mixing of Ideal Gases

#64. ΔS for Isothermal Mixing of Ideal Gases #64 Carnot Heat Engne ΔS for Isothermal Mxng of Ideal Gases ds = S dt + S T V V S = P V T T V PV = nrt, P T ds = v T = nr V dv V nr V V = nrln V V = - nrln V V ΔS ΔS ΔS for Isothermal Mxng for Ideal Gases

More information

PARTICIPATION FACTOR IN MODAL ANALYSIS OF POWER SYSTEMS STABILITY

PARTICIPATION FACTOR IN MODAL ANALYSIS OF POWER SYSTEMS STABILITY POZNAN UNIVE RSITY OF TE CHNOLOGY ACADE MIC JOURNALS No 86 Electrcal Engneerng 6 Volodymyr KONOVAL* Roman PRYTULA** PARTICIPATION FACTOR IN MODAL ANALYSIS OF POWER SYSTEMS STABILITY Ths paper provdes a

More information

An identification algorithm of model kinetic parameters of the interfacial layer growth in fiber composites

An identification algorithm of model kinetic parameters of the interfacial layer growth in fiber composites IOP Conference Seres: Materals Scence and Engneerng PAPER OPE ACCESS An dentfcaton algorthm of model knetc parameters of the nterfacal layer growth n fber compostes o cte ths artcle: V Zubov et al 216

More information

Color Rendering Uncertainty

Color Rendering Uncertainty Australan Journal of Basc and Appled Scences 4(10): 4601-4608 010 ISSN 1991-8178 Color Renderng Uncertanty 1 A.el Bally M.M. El-Ganany 3 A. Al-amel 1 Physcs Department Photometry department- NIS Abstract:

More information

Department of Statistics University of Toronto STA305H1S / 1004 HS Design and Analysis of Experiments Term Test - Winter Solution

Department of Statistics University of Toronto STA305H1S / 1004 HS Design and Analysis of Experiments Term Test - Winter Solution Department of Statstcs Unversty of Toronto STA35HS / HS Desgn and Analyss of Experments Term Test - Wnter - Soluton February, Last Name: Frst Name: Student Number: Instructons: Tme: hours. Ads: a non-programmable

More information

Chapter 13: Multiple Regression

Chapter 13: Multiple Regression Chapter 13: Multple Regresson 13.1 Developng the multple-regresson Model The general model can be descrbed as: It smplfes for two ndependent varables: The sample ft parameter b 0, b 1, and b are used to

More information

1 Rabi oscillations. Physical Chemistry V Solution II 8 March 2013

1 Rabi oscillations. Physical Chemistry V Solution II 8 March 2013 Physcal Chemstry V Soluton II 8 March 013 1 Rab oscllatons a The key to ths part of the exercse s correctly substtutng c = b e ωt. You wll need the followng equatons: b = c e ωt 1 db dc = dt dt ωc e ωt.

More information

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

A Mechanics-Based Approach for Determining Deflections of Stacked Multi-Storey Wood-Based Shear Walls A Mechancs-Based Approach for Determnng Deflectons of Stacked Mult-Storey Wood-Based Shear Walls FPINNOVATIONS Acknowledgements Ths publcaton was developed by FPInnovatons and the Canadan Wood Councl based

More information

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

Please initial the statement below to show that you have read it EN40: Dynamcs and Vbratons Mdterm Examnaton Thursday March 5 009 Dvson of Engneerng rown Unversty NME: Isaac Newton General Instructons No collaboraton of any knd s permtted on ths examnaton. You may brng

More information

Second Order Analysis

Second Order Analysis Second Order Analyss In the prevous classes we looked at a method that determnes the load correspondng to a state of bfurcaton equlbrum of a perfect frame by egenvalye analyss The system was assumed to

More information

Laboratory 1c: Method of Least Squares

Laboratory 1c: Method of Least Squares Lab 1c, Least Squares Laboratory 1c: Method of Least Squares Introducton Consder the graph of expermental data n Fgure 1. In ths experment x s the ndependent varable and y the dependent varable. Clearly

More information

An Algorithm to Solve the Inverse Kinematics Problem of a Robotic Manipulator Based on Rotation Vectors

An Algorithm to Solve the Inverse Kinematics Problem of a Robotic Manipulator Based on Rotation Vectors An Algorthm to Solve the Inverse Knematcs Problem of a Robotc Manpulator Based on Rotaton Vectors Mohamad Z. Al-az*, Mazn Z. Othman**, and Baker B. Al-Bahr* *AL-Nahran Unversty, Computer Eng. Dep., Baghdad,

More information

Assignment 4. Adsorption Isotherms

Assignment 4. Adsorption Isotherms Insttute of Process Engneerng Assgnment 4. Adsorpton Isotherms Part A: Compettve adsorpton of methane and ethane In large scale adsorpton processes, more than one compound from a mxture of gases get adsorbed,

More information

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

Introduction to Vapor/Liquid Equilibrium, part 2. Raoult s Law: CE304, Sprng 2004 Lecture 4 Introducton to Vapor/Lqud Equlbrum, part 2 Raoult s Law: The smplest model that allows us do VLE calculatons s obtaned when we assume that the vapor phase s an deal gas, and

More information

2016 Wiley. Study Session 2: Ethical and Professional Standards Application

2016 Wiley. Study Session 2: Ethical and Professional Standards Application 6 Wley Study Sesson : Ethcal and Professonal Standards Applcaton LESSON : CORRECTION ANALYSIS Readng 9: Correlaton and Regresson LOS 9a: Calculate and nterpret a sample covarance and a sample correlaton

More information

Lecture 8 Modal Analysis

Lecture 8 Modal Analysis Lecture 8 Modal Analyss 16.0 Release Introducton to ANSYS Mechancal 1 2015 ANSYS, Inc. February 27, 2015 Chapter Overvew In ths chapter free vbraton as well as pre-stressed vbraton analyses n Mechancal

More information

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

APPENDIX F A DISPLACEMENT-BASED BEAM ELEMENT WITH SHEAR DEFORMATIONS. Never use a Cubic Function Approximation for a Non-Prismatic Beam APPENDIX F A DISPACEMENT-BASED BEAM EEMENT WITH SHEAR DEFORMATIONS Never use a Cubc Functon Approxmaton for a Non-Prsmatc Beam F. INTRODUCTION { XE "Shearng Deformatons" }In ths appendx a unque development

More information

Negative Binomial Regression

Negative Binomial Regression STATGRAPHICS Rev. 9/16/2013 Negatve Bnomal Regresson Summary... 1 Data Input... 3 Statstcal Model... 3 Analyss Summary... 4 Analyss Optons... 7 Plot of Ftted Model... 8 Observed Versus Predcted... 10 Predctons...

More information

ON A DETERMINATION OF THE INITIAL FUNCTIONS FROM THE OBSERVED VALUES OF THE BOUNDARY FUNCTIONS FOR THE SECOND-ORDER HYPERBOLIC EQUATION

ON A DETERMINATION OF THE INITIAL FUNCTIONS FROM THE OBSERVED VALUES OF THE BOUNDARY FUNCTIONS FOR THE SECOND-ORDER HYPERBOLIC EQUATION Advanced Mathematcal Models & Applcatons Vol.3, No.3, 2018, pp.215-222 ON A DETERMINATION OF THE INITIAL FUNCTIONS FROM THE OBSERVED VALUES OF THE BOUNDARY FUNCTIONS FOR THE SECOND-ORDER HYPERBOLIC EUATION

More information

The Finite Element Method

The Finite Element Method The Fnte Element Method GENERAL INTRODUCTION Read: Chapters 1 and 2 CONTENTS Engneerng and analyss Smulaton of a physcal process Examples mathematcal model development Approxmate solutons and methods of

More information

CHAPTER 9 CONCLUSIONS

CHAPTER 9 CONCLUSIONS 78 CHAPTER 9 CONCLUSIONS uctlty and structural ntegrty are essentally requred for structures subjected to suddenly appled dynamc loads such as shock loads. Renforced Concrete (RC), the most wdely used

More information

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

Week3, Chapter 4. Position and Displacement. Motion in Two Dimensions. Instantaneous Velocity. Average Velocity Week3, Chapter 4 Moton n Two Dmensons Lecture Quz A partcle confned to moton along the x axs moves wth constant acceleraton from x =.0 m to x = 8.0 m durng a 1-s tme nterval. The velocty of the partcle

More information

Numerical Heat and Mass Transfer

Numerical Heat and Mass Transfer Master degree n Mechancal Engneerng Numercal Heat and Mass Transfer 06-Fnte-Dfference Method (One-dmensonal, steady state heat conducton) Fausto Arpno f.arpno@uncas.t Introducton Why we use models and

More information

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

MODAL ANALYSIS AND TESTING OF ROTATING MACHINES FOR PREDICTIVE MAINTENANCE: EFFECT OF GYROSCOPIC FORCES MODAL ANALYSIS AND TESTING OF ROTATING MACHINES FOR PREDICTIVE MAINTENANCE: EFFECT OF GYROSCOPIC FORCES A. Vansteenkste; M. Loccufer; B. Vervsch; P. De Baets; Ghent Unversty, Belgum Abstract Through the

More information

System in Weibull Distribution

System in Weibull Distribution Internatonal Matheatcal Foru 4 9 no. 9 94-95 Relablty Equvalence Factors of a Seres-Parallel Syste n Webull Dstrbuton M. A. El-Dacese Matheatcs Departent Faculty of Scence Tanta Unversty Tanta Egypt eldacese@yahoo.co

More information

Statistics for Managers Using Microsoft Excel/SPSS Chapter 13 The Simple Linear Regression Model and Correlation

Statistics for Managers Using Microsoft Excel/SPSS Chapter 13 The Simple Linear Regression Model and Correlation Statstcs for Managers Usng Mcrosoft Excel/SPSS Chapter 13 The Smple Lnear Regresson Model and Correlaton 1999 Prentce-Hall, Inc. Chap. 13-1 Chapter Topcs Types of Regresson Models Determnng the Smple Lnear

More information

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

STATIC ANALYSIS OF TWO-LAYERED PIEZOELECTRIC BEAMS WITH IMPERFECT SHEAR CONNECTION STATIC ANALYSIS OF TWO-LERED PIEZOELECTRIC BEAMS WITH IMPERFECT SHEAR CONNECTION Ákos József Lengyel István Ecsed Assstant Lecturer Emertus Professor Insttute of Appled Mechancs Unversty of Mskolc Mskolc-Egyetemváros

More information

Chapter 12. Ordinary Differential Equation Boundary Value (BV) Problems

Chapter 12. Ordinary Differential Equation Boundary Value (BV) Problems Chapter. Ordnar Dfferental Equaton Boundar Value (BV) Problems In ths chapter we wll learn how to solve ODE boundar value problem. BV ODE s usuall gven wth x beng the ndependent space varable. p( x) q(

More information

MEASUREMENT OF MOMENT OF INERTIA

MEASUREMENT OF MOMENT OF INERTIA 1. measurement MESUREMENT OF MOMENT OF INERTI The am of ths measurement s to determne the moment of nerta of the rotor of an electrc motor. 1. General relatons Rotatng moton and moment of nerta Let us

More information

LAB 4: Modulus of elasticity

LAB 4: Modulus of elasticity LAB 4: Modulus of elastcty 1. Preparaton: modulus of elastcty (chapter15, p.79) Hook s law graphcal determnaton of modulus of elastcty (p.8) determnaton of modulus of elastcty n tenson and flexural stress

More information

Econ107 Applied Econometrics Topic 3: Classical Model (Studenmund, Chapter 4)

Econ107 Applied Econometrics Topic 3: Classical Model (Studenmund, Chapter 4) I. Classcal Assumptons Econ7 Appled Econometrcs Topc 3: Classcal Model (Studenmund, Chapter 4) We have defned OLS and studed some algebrac propertes of OLS. In ths topc we wll study statstcal propertes

More information

Supplementary Notes for Chapter 9 Mixture Thermodynamics

Supplementary Notes for Chapter 9 Mixture Thermodynamics Supplementary Notes for Chapter 9 Mxture Thermodynamcs Key ponts Nne major topcs of Chapter 9 are revewed below: 1. Notaton and operatonal equatons for mxtures 2. PVTN EOSs for mxtures 3. General effects

More information

Note 10. Modeling and Simulation of Dynamic Systems

Note 10. Modeling and Simulation of Dynamic Systems Lecture Notes of ME 475: Introducton to Mechatroncs Note 0 Modelng and Smulaton of Dynamc Systems Department of Mechancal Engneerng, Unversty Of Saskatchewan, 57 Campus Drve, Saskatoon, SK S7N 5A9, Canada

More information

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

Assessment of Site Amplification Effect from Input Energy Spectra of Strong Ground Motion Assessment of Ste Amplfcaton Effect from Input Energy Spectra of Strong Ground Moton M.S. Gong & L.L Xe Key Laboratory of Earthquake Engneerng and Engneerng Vbraton,Insttute of Engneerng Mechancs, CEA,

More information

Laboratory 3: Method of Least Squares

Laboratory 3: Method of Least Squares Laboratory 3: Method of Least Squares Introducton Consder the graph of expermental data n Fgure 1. In ths experment x s the ndependent varable and y the dependent varable. Clearly they are correlated wth

More information

Psychology 282 Lecture #24 Outline Regression Diagnostics: Outliers

Psychology 282 Lecture #24 Outline Regression Diagnostics: Outliers Psychology 282 Lecture #24 Outlne Regresson Dagnostcs: Outlers In an earler lecture we studed the statstcal assumptons underlyng the regresson model, ncludng the followng ponts: Formal statement of assumptons.

More information

MECHANICS OF MATERIALS

MECHANICS OF MATERIALS Fourth Edton CHTER MECHNICS OF MTERIS Ferdnand. Beer E. Russell Johnston, Jr. John T. DeWolf ecture Notes: J. Walt Oler Texas Tech Unversty Stress and Stran xal oadng Contents Stress & Stran: xal oadng

More information

DYNAMIC BEHAVIOR OF PILE GROUP CONSIDERING SOIL-PILE-CAP INTERACTION

DYNAMIC BEHAVIOR OF PILE GROUP CONSIDERING SOIL-PILE-CAP INTERACTION October 1-17, 8, Bejng, Chna DYNAMIC BEHAVIOR OF PILE GROUP CONSIDERING SOIL-PILE-CAP INTERACTION A. M. Halaban 1 and M. Malek 1 Professor, Faculty of Cvl Engneerng, Isfahan Unversty of Technology, Isfahan,

More information

STATISTICAL MECHANICS

STATISTICAL MECHANICS STATISTICAL MECHANICS Thermal Energy Recall that KE can always be separated nto 2 terms: KE system = 1 2 M 2 total v CM KE nternal Rgd-body rotaton and elastc / sound waves Use smplfyng assumptons KE of

More information

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

Physics 5153 Classical Mechanics. D Alembert s Principle and The Lagrangian-1 P. Guterrez Physcs 5153 Classcal Mechancs D Alembert s Prncple and The Lagrangan 1 Introducton The prncple of vrtual work provdes a method of solvng problems of statc equlbrum wthout havng to consder the

More information

Suppose that there s a measured wndow of data fff k () ; :::; ff k g of a sze w, measured dscretely wth varable dscretzaton step. It s convenent to pl

Suppose that there s a measured wndow of data fff k () ; :::; ff k g of a sze w, measured dscretely wth varable dscretzaton step. It s convenent to pl RECURSIVE SPLINE INTERPOLATION METHOD FOR REAL TIME ENGINE CONTROL APPLICATIONS A. Stotsky Volvo Car Corporaton Engne Desgn and Development Dept. 97542, HA1N, SE- 405 31 Gothenburg Sweden. Emal: astotsky@volvocars.com

More information

PVP DETERMINATION OF GIMBAL AND HINGED EXPANSION JOINTS REACTION MOMENTS

PVP DETERMINATION OF GIMBAL AND HINGED EXPANSION JOINTS REACTION MOMENTS Proceedngs of the ASME 21 Pressure Vessel & Ppng Dvson / K-PVP Conference PVP21 July 18-22, 21, Bellevue, Washngton, USA PVP21-25223 DETERMINATION OF GIMBAL AND HINGED EXPANSION JOINTS REACTION MOMENTS

More information

Lectures - Week 4 Matrix norms, Conditioning, Vector Spaces, Linear Independence, Spanning sets and Basis, Null space and Range of a Matrix

Lectures - Week 4 Matrix norms, Conditioning, Vector Spaces, Linear Independence, Spanning sets and Basis, Null space and Range of a Matrix Lectures - Week 4 Matrx norms, Condtonng, Vector Spaces, Lnear Independence, Spannng sets and Bass, Null space and Range of a Matrx Matrx Norms Now we turn to assocatng a number to each matrx. We could

More information

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force.

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force. The fundamental prncples of classcal mechancs were lad down by Galleo and Newton n the 16th and 17th centures. In 1686, Newton wrote the Prncpa where he gave us three laws of moton, one law of gravty,

More information

Lecture 10 Support Vector Machines II

Lecture 10 Support Vector Machines II Lecture 10 Support Vector Machnes II 22 February 2016 Taylor B. Arnold Yale Statstcs STAT 365/665 1/28 Notes: Problem 3 s posted and due ths upcomng Frday There was an early bug n the fake-test data; fxed

More information

Over-Temperature protection for IGBT modules

Over-Temperature protection for IGBT modules Over-Temperature protecton for IGBT modules Ke Wang 1, Yongjun Lao 2, Gaosheng Song 1, Xanku Ma 1 1 Mtsubsh Electrc & Electroncs (Shangha) Co., Ltd., Chna Room2202, Tower 3, Kerry Plaza, No.1-1 Zhongxns

More information

THE EFFECT OF BEAM TO COLUMN CONNECTION IN ARC PORTAL FRAME

THE EFFECT OF BEAM TO COLUMN CONNECTION IN ARC PORTAL FRAME THE EFFECT OF BEAM TO COLUMN CONNECTON N ARC PORTAL FRAME Asko Keronen Rakenteden Mekankka, Vol. 26 No 2 1993, ss. 35-5 SUMMARY A full scale rc (renforced concrete) portal frame has been bult n order to

More information

Normally, in one phase reservoir simulation we would deal with one of the following fluid systems:

Normally, in one phase reservoir simulation we would deal with one of the following fluid systems: TPG4160 Reservor Smulaton 2017 page 1 of 9 ONE-DIMENSIONAL, ONE-PHASE RESERVOIR SIMULATION Flud systems The term sngle phase apples to any system wth only one phase present n the reservor In some cases

More information

Chapter 2 - The Simple Linear Regression Model S =0. e i is a random error. S β2 β. This is a minimization problem. Solution is a calculus exercise.

Chapter 2 - The Simple Linear Regression Model S =0. e i is a random error. S β2 β. This is a minimization problem. Solution is a calculus exercise. Chapter - The Smple Lnear Regresson Model The lnear regresson equaton s: where y + = β + β e for =,..., y and are observable varables e s a random error How can an estmaton rule be constructed for the

More information

/ n ) are compared. The logic is: if the two

/ n ) are compared. The logic is: if the two STAT C141, Sprng 2005 Lecture 13 Two sample tests One sample tests: examples of goodness of ft tests, where we are testng whether our data supports predctons. Two sample tests: called as tests of ndependence

More information

One-sided finite-difference approximations suitable for use with Richardson extrapolation

One-sided finite-difference approximations suitable for use with Richardson extrapolation Journal of Computatonal Physcs 219 (2006) 13 20 Short note One-sded fnte-dfference approxmatons sutable for use wth Rchardson extrapolaton Kumar Rahul, S.N. Bhattacharyya * Department of Mechancal Engneerng,

More information

Assignment 5. Simulation for Logistics. Monti, N.E. Yunita, T.

Assignment 5. Simulation for Logistics. Monti, N.E. Yunita, T. Assgnment 5 Smulaton for Logstcs Mont, N.E. Yunta, T. November 26, 2007 1. Smulaton Desgn The frst objectve of ths assgnment s to derve a 90% two-sded Confdence Interval (CI) for the average watng tme

More information