Dynamic Response to Harmonic Transverse Excitation of Cantilever Euler-Bernoulli Beam Carrying a Point Mass
|
|
- Dortha Bailey
- 5 years ago
- Views:
Transcription
1 Ante Skoblar Teachng Assstant Unversty of Rjeka aculty of Engneerng Croata Roberto Žgulć ull Professor Unversty of Rjeka aculty of Engneerng Croata Sanjn Braut ull Professor Unversty of Rjeka aculty of Engneerng Croata Sebastjan Blaževć Teachng Assstant Unversty of Rjeka aculty of Engneerng Croata Dynamc Response to Harmonc Transverse Exctaton of Cantlever Euler-Bernoull Beam Carryng a Pont ass In ths paper, the calculaton of the dynamc response to harmonc transverse exctaton of cantlever Euler-Bernoull beam carryng a pont mass wth the mode superposton method s presented. Ths method uses mode shapes and modal coordnate functons whch are calculated by separaton of varables and aplace transformatons. The accuracy of defned expressons s confrmed on examples wth and wthout Raylegh dampng. All calculatons are n good agreement wth the results of commercal software based on fnte element methods. Keywords: dynamc response, Euler-Bernoull beam, pont mass, mode superposton method, Raylegh dampng. 1. INTRODUCTION Dynamc analyss of a structure as contnuum (where nerta, stffness and dampng are evenly dstrbuted throughout the doman has lmted use n practce because of ts mathematcal complexty. However, the analyss of contnuum systems, such as e.g. beam, gves us useful nformaton of complete dynamc behavour of more complex structures, so papers wth dfferent beam boundary condtons as [1], [] and [], beam exctatons (n pont [4], [5], base exctaton [6], etc. or beam materals (composte [7], [8], etc. are publshed. Transverse vbratons of unform slender beam can be calculated usng the Euler-Bernoull theory. Ths paper descrbes specfc combnaton of boundary condtons (cantlever beam wth pont mass and exctaton (harmonc exctaton n one pont whch can be found n practce as n [9] and [1] but ths calculaton procedure can be used for any boundary condtons. In ths paper, natural frequences and mode shapes are calculated usng the method of separaton of varables and aplace transformatons of homogeneous part of dfferental equaton of moton of cantlever beam carryng a pont mass wthout dampng. Then dynamc response of undamped and damped beam, where dampng s defned wth Raylegh theory, s defned by the mode superposton method whch uses mode shapes and modal coordnate functons. Calculaton of modal coordnates functons s based on the orthogonalty characterstc of mode shapes. Analytcal results, calculated by atlab1a on Wndows 8, are compared to numercal results, calculated by software SC.Nastran for Wndows [11] where beam fnte element, based on Tmoshenko beam theory, s used for creaton of fnte element model.. DYNAIC RESPONSE TO HARONIC TRANSVERSE EXCITATION Beam wth the constant rectangular cross-secton wth pont mass on poston x and under the acton of transversal harmonc force on poston x s analysed. gure 1. Sketch of cantlever Euler-Bernoull beam carryng a pont mass wth harmonc transverse exctaton n one pont A dfferental equaton of forced vbratons of beam (see [1] and [1] s defned by usng the Hamltons varatonal prncple: 4 5 cd ρ 4 4 w w w w EI EI c A x ω x t t t w δ x x = Ωt x x t ( sn ( δ ( Receved: September 16, Accepted: November 16 Correspondence to: D. Sc. Ante Skoblar aculty of Engneerng, Unversty of Rjeka Vukovarska 58, 51 Rjeka, Croata E-mal: askoblar@rteh.hr do:1.597/fmet1767s aculty of echancal Engneerng, Belgrade. All rghts reserved E Transactons (17 45, (1 where E s Youngs modulus, I second moment of area, w transversal dsplacement, x beam longtudnal coordnate, c d stffness proportonal and c mass proportonal Raylegh dampng coeffcent, ρ beam materal densty, A cross-secton area, value of pont mass, x coordnate of pont mass, exctaton force ampltude and Ω angular frequency of harmonc exctaton. Parts of (1 are flexural stffness, nner dampng, external dampng [1] and nerta of beam, nerta of pont mass and external force, respectvely. It s known that undamped lnear dynamc systems have natural mode shapes, and that n every mode shape
2 dfferent parts of the system are vbratng n phase, passng through equlbrum n the same moment. In the damped systems, however, ths characterstc generally does not apply [14]. Raylegh [1] has shown that there s a group of damped systems whch have classcal mode shapes. In ths paper a Raylegh defnton of dampng s used and uncoupled functons of modal coordnates are defned as a basc part of mode superposton method..1 Natural frequences and mode shapes The objectve of ths chapter s to defne natural frequences and mode shapes from homogeneous part of dfferental equaton of cantlever beam carryng a pont mass wthout dampng []: 4 w w w EI ρ A δ ( x x 4 =. ( x t t Boundary condtons for cantlever beam are: ( ( ( ( w, t = w, t = w, t = w, t = ( where s dervatve wth respect to x. Condton w(,t= s vald f the free beam end s not loaded wth external force or pont mass. Dfferental equaton ( s solved by the method of separaton of varables by whch dsplacement s defned wth the product of two separated functons of poston and tme: (, ψ ( sn( ω w x t = x t, (4 where ψ(x s mode shape and sn(ωt represents harmonc vbratons wth angular natural frequency ω. After ncluson of (4 nto ( and dvson of the whole expresson wth sn(ωt an expresson s obtaned: ( ( ε ( x EIψ ρ A δ x x ψω =, (5 where functon ε(x s so called weghtng functon. Boundary condtons has to be satsfed after applcaton of method of separaton of varables whch s possble f: ( ( ( ( ψ = ψ = ψ = ψ =. (6 Equatons (5 and (6 defne egenvalue problem whch s solved by aplace transformatons wth respect to x coordnate so equaton (5 now has the form: ( A ( EI ψ ρ ψ ω. (7 ω ( ψδ ( x x = aplace transformaton for functon ψ (x s: 4 ( ψ ( = ( ψ ( ψ ( x s x s ( s ( ( s ψ ψ ψ (8 where boundary condtons ψ ( and ψ ( are equal to zero (see (6, whle aplace transformaton for equaton part ψδ ( x x s: sx ( ψ ( δ ( ψ ( x x x e x =. (9 After ncluson of (8 and (9 nto (7 we obtan expresson: s 1 ( ψ ( x = ψ ( ψ ( s k s k, (1 ω ψ sx ( x e EI 4 4 s k where wave number k s calculated from expresson: ω ρ A k = EI Inverse aplace follows: ( ψ = ψ cosh.5 ( kx cos( kx k. (11 ( kx sn ( kx ω ψ ( x snh ψ ( k snh U ( x x k ( k ( x x sn ( k ( x x and wth the rest of the boundary condtons ψ (=ψ (= functons ψ ( and ψ ( are calculated and mode shape functon s defned as: ( x EI ω ψ ψ ( x = ( A kx kx 4EIk B kx kx u x x ( sn ( snh ( ( cos( cosh ( ( ( kx kx snh ( kx kx ( sn (1, (1 where values of A and B are calculated from expressons [9]: cos A = sn B = ( k kx cosh ( k kx sn ( k snh ( k sn ( k kx snh ( k kx cos( k cosh ( k cos( k cosh ( k sn ( k snh ( k sn ( k snh ( k cos( k cosh ( k ( kx snh ( kx cos( k kx snh ( k cosh ( k kx sn ( k sn ( k kx cosh ( k snh ( k kx cos( k cos( k cosh ( k 1, (14. (15 By nsertng condton x=x n (1, the expresson for calculaton of natural frequences ω s obtaned: ( sn snh ( ( ( ( ( ( ω A kx kx. (16 B cos kx cosh kx 4EIk = 68 VO. 45, No, 17 E Transactons
3 It s observed that equaton (16 has the form f(k= after ncluson of (11 so ts zero ponts (see fgure defne wave numbers k. Then natural frequences from (11 and mode shapes from (1 can be obtaned. gure. Zero ponts of equaton (16 The accuracy of calculated mode shapes are confrmed wth (5.. unctons of modal coordnates The equaton (1 s solved by mode superposton method where the soluton s assumed n form:, n n n= 1 ( ( ψ ( w x t = q t x (17 where q n (t are the functons of modal coordnates and ψ n (x are the mode shapes (1. After ncluson of (17 nto (1 and defnton of stffness proportonal (c d =βω and mass proportonal Raylegh dampng (c=αε(x [1], equaton (1 has a form ɺ ( ɺ ( x qɺɺ sn ( t ( x x EIψ q EI βψ q αε x ψ q ε ψ = Ω δ. (18 Now, an orthogonalty characterstc of normalzed mode shapes s used to get uncoupled functons of modal coordnates. Normalzed mass of mode shape s defned wth expresson: ( ψ ( = ε x x dx (19 and mass normalzed mode shape can be determned from expresson: ψ ψ =. ( ass normalzed mode shape functons satsfy expressons: and ( ε ( x ψ ( x d x = 1 (1 ε ( x ψ ( x ψ j ( x d x = ( whch makes them orthogonal wth respect to the weghtng functon ε (x. After ncluson of expresson (5 nto (18, multplyng expresson (18 wth mode shape functon ψ j and dvdng t wth the product of square roots of normalzed masses ( j an dfferental equaton s obtaned: ( x jq ( x jqɺ αε ( x ψ ψ jqɺ ε ( x ψ ψ jqɺɺ ψ j ( x = sn ( Ωt δ ( x x ε ω ψ ψ βε ω ψ ψ. ( After ntegraton of eq. ( over the beam doman for all mode shapes the followng expresson s obtaned: ( jd ɺ ( j ω q ε x ψ ψ x βω q ε x ψ ψ dx ( d ɺɺ ( αqɺ ε x ψ ψ x q ε x ψ ψ dx j j ( x ψ j = sn ( Ωt δ x x (, (4 where all combnatons of ndexes and j of normalzed mode shapes are under ntegral. Integrals n expresson (4 wth dfferent ndexes and j are equal to zero whle ntegrals wth equal ndexes =j are equal to one. As a result, a number of uncoupled expressons for functons of modal coordnates are gven: ( ( ɺ ( ω q t α βω q t ( x ψ qɺɺ ( t = sn ( Ωt. (5 urthermore, modal dampng rato ζ of -th mode shape based on Raylegh theory [1] s defned wth: so expresson (5 has a new form: wth a soluton: α βω ζ = (6 ω ( ζ ωɺ ( ω q t q t ( x ψ qɺɺ ( t = sn ( Ωt ζ ωt qɺ ζ ωq ( sn ( ω q t = e t ω ψ ( x q ( ωt ω cos t ζ ωτ sn ( τ e sn ( ω ( t τ dτ Ω (7 (8 E Transactons VO. 45, No, 17 69
4 where ω = ω 1 ζ s natural damped frequency of -th mode shape.. EXAPE 1 In ths example, natural frequences and mode shapes for a beam whch can be modelled by Euler-Bernoull theory are verfed by Nastran. Also, numercal overflow whch appears at hgher natural frequences s analysed. Beam dmensons are.46m*.m*.7m and beam materal s galvanzed steel wth Youngs modulus E=.1*1 11 Pa, the densty ρ=778 kg/m and the Possons coeffcent ν=.. The accuracy of the analytcal results wll be confrmed usng the software Nastran [11] by comparson of natural frequences and mode shapes. Beam fnte elements wth two nodes and unconnected fnte element degrees of freedom T y (dsplacement parallel to x axs and R z (rotaton parallel to z axs, see fgure 1 and an opton of coupled mass are used. After confrmaton of convergence of the results, 5 fnte elements of the same sze s used for modellng of the beam whch gves, approxmately, 1 fnte elements along one mode shape peak of the hghest mode shape. Pont mass wth.1 kg s postoned at 6. node (on coordnate x=. m and natural frequences are calculated. In table 1, a good agreement between analytcal results calculated from zero ponts of equaton (16 and expresson (11 (see fgure and Nastran results can be seen. Table 1. Natural frequences Natural frequency No. Analytc expressons, Hz Nastran, Hz In fgures and 4 a good agreement between mode shapes calculated wth (1 and (9 and wth Nastran can be seen. The descrbed approach gves exact natural frequences and mode shapes for 1-st to 5-th mode shape, but the error s observed for 6-th and hgher mode shapes. The values of equaton (16 whose zero ponts gve natural frequences start to oscllate (see fgure 5 whch grows for hgher natural frequences. Ths error s caused by a numercal overflow [9] whch appears n expressons (14 and (15 because hyperbolc functons wth hgh values are n ratos. gure 4. ode shapes calculated wth expressons (1 and (9 ( and wth Nastran ( *. gure 5. Value of functon (16 around zero pont of 5-th natural frequency As a result a group of ncorrect natural frequences can be calculated n the vcnty of the exact natural frequency (see fgure 6. gure. ode shapes 1.-. calculated wth expressons (1 and (9 ( and wth Nastran ( *. gure 6. Value of functon (16 around zero pont for 6-th natural frequency 7 VO. 45, No, 17 E Transactons
5 urthermore, t was shown that wth reducton of the pont mass the natural frequency of the beam wth pont mass converge toward natural frequency of beam wthout mass (see table. nfluence on response because ts frequency (44.65 Hz s close to exctaton frequency (45 Hz. Table. Values of natural frequences wth reducton of pont mass Natural frequency Natural frequences of beam wth pont mass, Hz No..1 kg.1kg.1kg Beam natural freq., Hz EXAPE The objectve of example s the comparson of numercal and analytcal results of equaton (7.e. the functon of modal coordnates and comparson of dynamc response wthout dampng calculated by mode superposton method and by drect transent method wth Nastran [11]. The harmonc transversal force have the ampltude 1 N and frequency of 45 Hz whch s more than four tmes lower than the hghest calculated 6-th natural frequency (17 Hz n order to get more accurate results [9]. orce s actng at. node (on coordnate x=. m. Good agreement of results for functon of modal coordnate can be seen on fgure 7 whch confrms the accuracy of analytc soluton. An overflow also occurs n the functon of modal coordnates but t can be avoded by the procedure explaned n [9]. gure 8. Dynamc response of undamped beam at node 46. calculated wth expresson (17 ( and wth software Nastran (* gure 9. Dynamc response of damped beam calculated wth mode superposton method ( and wth Nastran( * 5. EXAPE gure 7. Comparson of 1.(,.(o and.( * functon of modal coordnates calculated by numercal soluton of dfferental equaton (7 and by expresson (8 ( In ths example beam dynamc response n node 46. (at coordnate x=.41 m s also calculated usng mode superposton method and by drect transent method n Nastran [11] and calculated results are n good agreement whch can be seen on fgure 8. uncton of modal coordnate for. mode shape have largest The objectve of example s the comparson of results of dynamc response for damped beam by usng mode superposton method wth results of software Nastran. Overall structural dampng coeffcent G s used n Nastran for defnton of dampng n drect transent method. Structural dampng s connected wth dsplacement and t has constant value e.g. t does not depend up on frequency. In presented theory of mode superposton method we use Raylegh dampng whch depends up on frequency. Wth the am of comparng analytc results wth Nastran, we wll use the equvalent vscous dampng to defne G. Equvalent vscous dampng grows lnearly wth the frequency and t can be equal wth Raylegh dampng f Raylegh mass proportonal coeffcent s equal to zero. In that case overall structural coeffcent G can be calculated from the value of Raylegh stffness proportonal coeffcent E Transactons VO. 45, No, 17 71
6 (e.g. β=.1 n ths example and frst natural angular frequency ω 1 [11] from expresson: G = ξ = βω. (9 The setup parameters n drect transent analyss n Nastran are f 1 =W=.549 Hz and G=.16. At fgure 9 an transversal dynamc response at node 46. can be seen. 6. CONCUSION In ths paper an analytc expresson for dynamc response to transverse harmonc force of Euler-Bernoull cantlever beam wth the pont mass s defned. A procedure for defnng natural frequences, mode shapes and functons of modal coordnates s descrbed and results are used n the modal superposton method. Expressons for natural frequences are tested by reducng the pont mass, whereby natural frequences converged toward natural frequences of cantlever beam wthout pont mass, whch s a confrmaton of expressons accuracy. Durng the analyss of natural frequences t s observed that error occurs when hgher natural frequences are calculated. Errors are caused by numercal overflow whch appears because hyperbolc functons wth hgh values are n ratos. In ths paper dampng s defned wth Rayleghs theory whereby t s possble to calculate uncoupled functons of modal coor dnates, whch s descrbed n detal. or confrmaton of the results a software based on fnte element method was used (Nastran. Structural dampng for the drect transent method n Nastran was defned from equvalent vscous dampng whch correspond to Raylegh stffness proportonal dampng whle mass proportonal dampng was set to zero. All calculated results are n good agreement. ACKNOWEDGENT AdraHub s a collaboratve project funded by the European Unon (EU nsde the Adratc IPA CBC Programme, an Instrument for the Pre-Accesson Assstance (IPA of neghbourng countres of the Western Balkans, thanks to the nvestments n Cross- Border Cooperaton (CBC amng at jont economc and socal development. Detals n Savoa et al. [15]. Ths study s also supported by Unversty of Rjeka Grants (No and No ovng oads, Structural Engneerng and echancs, Vol. 44, No. 5, pp , 1. [5] Hamdan,.N. et al.: orce and orced Vbratons of a Restraned Cantlever Beam Carryng a Concentrated ass, Eng. Sc., Vol., pp. 71-8, [6] Erturk, A., Inman, D.J.: On echancal modelng of Cantlevered Pezoelectrc Vbraton Energy Harvesters, Journal of Intellgent ateral Systems and Structures, Vol. 19, p.p , 8. [7] Žvkovć, I., Pavlovć, A., ragassa, C.: Improvements n Wood Thermoplastc atrx Composte aterals Propertes by Physcal and Chemcal Treatments, Int J Qual Res, Vol. 1, No., pp. 5-18, 16. [8] Saghaf, H., Brugo, T.., Zucchell, A., ragassa, C., nak, G.: Comparson of the Effect of Preload and Curvature of Composte amnate under Impact oadng, E Transactons, Vol. 44, No. 4, p.p. 5-57, 16. [9] Skoblar, A., Žgulć, R., Braut, S.: Numercal Illcondtonng n evaluaton of the dynamc response of structures wth mode superposton method, Proc IechE Part C: J echancal Engneerng Scence, n press, DOI: / , 16. [1] Pavlovć, A., ragassa, C.: Analyss of lexble Barrers Used as Safety Protecton n Wood workng, Int J Qual Res, Vol. 1, No. 1, pp , 16. [11] SC. Nastran Verson 68. Basc dynamc analyss user s gude. SC. Software Corporaton, 4. [1] Banks, H.T., Inman, D.J.: On dampng mechansms n beams, Journal of Appled echancs, Vol. 58, pp , [1] Goel, R.P.: Vbratons of a Beam Carryng a Concentrated ass, Journal of Appled echancs, pp. 81-8, September 197. [14] Caughey, T.K., OKelly,.E.J.: Classcal Normal odes n Damped near Dynamc Systems, J. Appled echancs, p.p , September [15] Savoa,., Stefanovc,. and ragassa, C.: ergng techncal competences and human resources wth the am at contrbutng to transform the Adratc area n a stable hub for a sustanable technologcal development, Int J Qual Res, 1, pp. 1 1, 16. REERENCES [1] Han S, Benaroya H and We T. Dynamcs of transversely vbratng beams usng four engneerng theores. J Sound Vbrat, 5, pp , [] Chen, Y.: On the vbraton of beams or rods carryng a concentrated mass. J Appl ech,, pp. 1 11, 196. [] Gest, B.: The Effect of Structural Dampng on Nodes for the Euler-Bernoull Beam: A Specfc Case Study, Appl. ath. ett., Vol. 7, No., pp , [4] Pccardo, G., Tubno,.: Dynamc Response of Euler-Bernoull beams to Resonant Harmonc ДИНАМИЧКИ ОДГОВОР НА ХАРМОНИЧНУ ПОПРЕЧНУ ПОБУДУ КОНЗОЛЕ EUER- BERNOUI СА КОНЦЕНТРИЧНИМ МАСАМА А. Скоблар, Р. Жигулић, С. Браут, С. Блажевић У овом раду приказан је прорачун динамичког одговора на хармоничну попречну побуду конзоле Euler-Bernoull са концентричним масама, методом режима суперпозиције. Метод суперпозиције користи режиме облика и координата функције које су изра 7 VO. 45, No, 17 E Transactons
7 чунате одвајањем променљивих и Лаплас трансфор мацијама. Тачност дефинисаних израза су потврђени на примерима са и без Ralegh пригушења. Сви резу лтати су у сагласности са резултатима комерцијал них софтвера на основу метода коначних елемената. E Transactons VO. 45, No, 17 7
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 informationCOMPOSITE 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 informationGEO-SLOPE International Ltd, Calgary, Alberta, Canada Vibrating Beam
GEO-SLOPE Internatonal Ltd, Calgary, Alberta, Canada www.geo-slope.com Introducton Vbratng Beam Ths example looks at the dynamc response of a cantlever beam n response to a cyclc force at the free end.
More information829. An adaptive method for inertia force identification in cantilever under moving mass
89. An adaptve method for nerta force dentfcaton n cantlever under movng mass Qang Chen 1, Mnzhuo Wang, Hao Yan 3, Haonan Ye 4, Guola Yang 5 1,, 3, 4 Department of Control and System Engneerng, Nanng Unversty,
More informationSolution of Equilibrium Equation in Dynamic Analysis. Mode Superposition. Dominik Hauswirth Method of Finite Elements II Page 1
Soluton of Equlbrum Equaton n Dynamc Analyss Mode Superposton Domnk Hauswrth..7 Method of Fnte Elements II Page Contents. Mode Superposton: Idea and Equatons. Example 9.7 3. Modes 4. Include Dampng 5.
More informationCHAPTER 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 informationΔ x. u(x,t) Fig. Schematic view of elastic bar undergoing axial motions
ME67 - Handout 4 Vbratons of Contnuous Systems Axal vbratons of elastc bars The fgure shows a unform elastc bar of length and cross secton A. The bar materal propertes are ts densty ρ and elastc modulus
More informationMEEM 3700 Mechanical Vibrations
MEEM 700 Mechancal Vbratons Mohan D. Rao Chuck Van Karsen Mechancal Engneerng-Engneerng Mechancs Mchgan echnologcal Unversty Copyrght 00 Lecture & MEEM 700 Multple Degree of Freedom Systems (ext: S.S.
More informationSTATIC 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 informationΔ x. u(x,t) Fig. Schematic view of elastic bar undergoing axial motions
ME67 - Handout 4 Vbratons of Contnuous Systems Axal vbratons of elastc bars The fgure shows a unform elastc bar of length and cross secton A. The bar materal propertes are ts densty ρ and elastc modulus
More informationProfessor Terje Haukaas University of British Columbia, Vancouver The Q4 Element
Professor Terje Haukaas Unversty of Brtsh Columba, ancouver www.nrsk.ubc.ca The Q Element Ths document consders fnte elements that carry load only n ther plane. These elements are sometmes referred to
More informationLecture 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 informationIndeterminate 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 informationDetermination 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 informationDUE: 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 informationNONLINEAR 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 informationWeek 9 Chapter 10 Section 1-5
Week 9 Chapter 10 Secton 1-5 Rotaton Rgd Object A rgd object s one that s nondeformable The relatve locatons of all partcles makng up the object reman constant All real objects are deformable to some extent,
More informationFinite 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 informationModeling and Simulation of a Hexapod Machine Tool for the Dynamic Stability Analysis of Milling Processes. C. Henninger, P.
Smpack User Meetng 27 Modelng and Smulaton of a Heapod Machne Tool for the Dynamc Stablty Analyss of Mllng Processes C. Hennnger, P. Eberhard Insttute of Engneerng project funded by the DFG wthn the framework
More informationChapter 4 The Wave Equation
Chapter 4 The Wave Equaton Another classcal example of a hyperbolc PDE s a wave equaton. The wave equaton s a second-order lnear hyperbolc PDE that descrbes the propagaton of a varety of waves, such as
More informationIn 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( ) = ( ) + ( 0) ) ( )
EETOMAGNETI OMPATIBIITY HANDBOOK 1 hapter 9: Transent Behavor n the Tme Doman 9.1 Desgn a crcut usng reasonable values for the components that s capable of provdng a tme delay of 100 ms to a dgtal sgnal.
More informationNote 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 informationFUZZY 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 informationCanonical transformations
Canoncal transformatons November 23, 2014 Recall that we have defned a symplectc transformaton to be any lnear transformaton M A B leavng the symplectc form nvarant, Ω AB M A CM B DΩ CD Coordnate transformatons,
More informationInner Product. Euclidean Space. Orthonormal Basis. Orthogonal
Inner Product Defnton 1 () A Eucldean space s a fnte-dmensonal vector space over the reals R, wth an nner product,. Defnton 2 (Inner Product) An nner product, on a real vector space X s a symmetrc, blnear,
More informationAdjoint Methods of Sensitivity Analysis for Lyapunov Equation. Boping Wang 1, Kun Yan 2. University of Technology, Dalian , P. R.
th World Congress on Structural and Multdscplnary Optmsaton 7 th - th, June 5, Sydney Australa Adjont Methods of Senstvty Analyss for Lyapunov Equaton Bopng Wang, Kun Yan Department of Mechancal and Aerospace
More informationGeorgia Tech PHYS 6124 Mathematical Methods of Physics I
Georga Tech PHYS 624 Mathematcal Methods of Physcs I Instructor: Predrag Cvtanovć Fall semester 202 Homework Set #7 due October 30 202 == show all your work for maxmum credt == put labels ttle legends
More informationPHYS 705: Classical Mechanics. Calculus of Variations II
1 PHYS 705: Classcal Mechancs Calculus of Varatons II 2 Calculus of Varatons: Generalzaton (no constrant yet) Suppose now that F depends on several dependent varables : We need to fnd such that has a statonary
More informationAppendix B. The Finite Difference Scheme
140 APPENDIXES Appendx B. The Fnte Dfference Scheme In ths appendx we present numercal technques whch are used to approxmate solutons of system 3.1 3.3. A comprehensve treatment of theoretcal and mplementaton
More informationInductance Calculation for Conductors of Arbitrary Shape
CRYO/02/028 Aprl 5, 2002 Inductance Calculaton for Conductors of Arbtrary Shape L. Bottura Dstrbuton: Internal Summary In ths note we descrbe a method for the numercal calculaton of nductances among conductors
More informationFrame element resists external loads or disturbances by developing internal axial forces, shear forces, and bending moments.
CE7 Structural Analyss II PAAR FRAE EEET y 5 x E, A, I, Each node can translate and rotate n plane. The fnal dsplaced shape has ndependent generalzed dsplacements (.e. translatons and rotatons) noled.
More information12. The Hamilton-Jacobi Equation Michael Fowler
1. The Hamlton-Jacob Equaton Mchael Fowler Back to Confguraton Space We ve establshed that the acton, regarded as a functon of ts coordnate endponts and tme, satsfes ( ) ( ) S q, t / t+ H qpt,, = 0, and
More informationSUPPLEMENTARY INFORMATION
do: 0.08/nature09 I. Resonant absorpton of XUV pulses n Kr + usng the reduced densty matrx approach The quantum beats nvestgated n ths paper are the result of nterference between two exctaton paths of
More informationAERODYNAMICS I LECTURE 6 AERODYNAMICS OF A WING FUNDAMENTALS OF THE LIFTING-LINE THEORY
LECTURE 6 AERODYNAMICS OF A WING FUNDAMENTALS OF THE LIFTING-LINE THEORY The Bot-Savart Law The velocty nduced by the sngular vortex lne wth the crculaton can be determned by means of the Bot- Savart formula
More informationConstitutive 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 informationModeling of Dynamic Systems
Modelng of Dynamc Systems Ref: Control System Engneerng Norman Nse : Chapters & 3 Chapter objectves : Revew the Laplace transform Learn how to fnd a mathematcal model, called a transfer functon Learn how
More informationON 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 informationNovember 5, 2002 SE 180: Earthquake Engineering SE 180. Final Project
SE 8 Fnal Project Story Shear Frame u m Gven: u m L L m L L EI ω ω Solve for m Story Bendng Beam u u m L m L Gven: m L L EI ω ω Solve for m 3 3 Story Shear Frame u 3 m 3 Gven: L 3 m m L L L 3 EI ω ω ω
More informationPhysics 5153 Classical Mechanics. Principle of Virtual Work-1
P. Guterrez 1 Introducton Physcs 5153 Classcal Mechancs Prncple of Vrtual Work The frst varatonal prncple we encounter n mechancs s the prncple of vrtual work. It establshes the equlbrum condton of a mechancal
More informationChapter 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 informationIrregular 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 informationA NUMERICAL COMPARISON OF LANGRANGE AND KANE S METHODS OF AN ARM SEGMENT
Internatonal Conference Mathematcal and Computatonal ology 0 Internatonal Journal of Modern Physcs: Conference Seres Vol. 9 0 68 75 World Scentfc Publshng Company DOI: 0.4/S009450059 A NUMERICAL COMPARISON
More informationCHAPTER 14 GENERAL PERTURBATION THEORY
CHAPTER 4 GENERAL PERTURBATION THEORY 4 Introducton A partcle n orbt around a pont mass or a sphercally symmetrc mass dstrbuton s movng n a gravtatonal potental of the form GM / r In ths potental t moves
More information), it produces a response (output function g (x)
Lnear Systems Revew Notes adapted from notes by Mchael Braun Typcally n electrcal engneerng, one s concerned wth functons of tme, such as a voltage waveform System descrpton s therefore defned n the domans
More informationStatistical Energy Analysis for High Frequency Acoustic Analysis with LS-DYNA
14 th Internatonal Users Conference Sesson: ALE-FSI Statstcal Energy Analyss for Hgh Frequency Acoustc Analyss wth Zhe Cu 1, Yun Huang 1, Mhamed Soul 2, Tayeb Zeguar 3 1 Lvermore Software Technology Corporaton
More informationEVALUATION 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 informationSalmon: Lectures on partial differential equations. Consider the general linear, second-order PDE in the form. ,x 2
Salmon: Lectures on partal dfferental equatons 5. Classfcaton of second-order equatons There are general methods for classfyng hgher-order partal dfferental equatons. One s very general (applyng even to
More informationModule 1 : The equation of continuity. Lecture 1: Equation of Continuity
1 Module 1 : The equaton of contnuty Lecture 1: Equaton of Contnuty 2 Advanced Heat and Mass Transfer: Modules 1. THE EQUATION OF CONTINUITY : Lectures 1-6 () () () (v) (v) Overall Mass Balance Momentum
More informationTHE VIBRATIONS OF MOLECULES II THE CARBON DIOXIDE MOLECULE Student Instructions
THE VIBRATIONS OF MOLECULES II THE CARBON DIOXIDE MOLECULE Student Instructons by George Hardgrove Chemstry Department St. Olaf College Northfeld, MN 55057 hardgrov@lars.acc.stolaf.edu Copyrght George
More informationAPPENDIX 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 informationStudy on Non-Linear Dynamic Characteristic of Vehicle. Suspension Rubber Component
Study on Non-Lnear Dynamc Characterstc of Vehcle Suspenson Rubber Component Zhan Wenzhang Ln Y Sh GuobaoJln Unversty of TechnologyChangchun, Chna Wang Lgong (MDI, Chna [Abstract] The dynamc characterstc
More informationA Solution of the Harry-Dym Equation Using Lattice-Boltzmannn and a Solitary Wave Methods
Appled Mathematcal Scences, Vol. 11, 2017, no. 52, 2579-2586 HIKARI Ltd, www.m-hkar.com https://do.org/10.12988/ams.2017.79280 A Soluton of the Harry-Dym Equaton Usng Lattce-Boltzmannn and a Soltary Wave
More informationPhysics 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 informationIntegrals and Invariants of Euler-Lagrange Equations
Lecture 16 Integrals and Invarants of Euler-Lagrange Equatons ME 256 at the Indan Insttute of Scence, Bengaluru Varatonal Methods and Structural Optmzaton G. K. Ananthasuresh Professor, Mechancal Engneerng,
More informationPHYS 705: Classical Mechanics. Canonical Transformation II
1 PHYS 705: Classcal Mechancs Canoncal Transformaton II Example: Harmonc Oscllator f ( x) x m 0 x U( x) x mx x LT U m Defne or L p p mx x x m mx x H px L px p m p x m m H p 1 x m p m 1 m H x p m x m m
More informationA how to guide to second quantization method.
Phys. 67 (Graduate Quantum Mechancs Sprng 2009 Prof. Pu K. Lam. Verson 3 (4/3/2009 A how to gude to second quantzaton method. -> Second quantzaton s a mathematcal notaton desgned to handle dentcal partcle
More informationTransfer 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 informationArmy Ants Tunneling for Classical Simulations
Electronc Supplementary Materal (ESI) for Chemcal Scence. Ths journal s The Royal Socety of Chemstry 2014 electronc supplementary nformaton (ESI) for Chemcal Scence Army Ants Tunnelng for Classcal Smulatons
More informationELASTIC 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 informationLab 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 informationChapter Eight. Review and Summary. Two methods in solid mechanics ---- vectorial methods and energy methods or variational methods
Chapter Eght Energy Method 8. Introducton 8. Stran energy expressons 8.3 Prncpal of statonary potental energy; several degrees of freedom ------ Castglano s frst theorem ---- Examples 8.4 Prncpal of statonary
More informationSpin-rotation coupling of the angularly accelerated rigid body
Spn-rotaton couplng of the angularly accelerated rgd body Loua Hassan Elzen Basher Khartoum, Sudan. Postal code:11123 E-mal: louaelzen@gmal.com November 1, 2017 All Rghts Reserved. Abstract Ths paper s
More informationUniqueness of Weak Solutions to the 3D Ginzburg- Landau Model for Superconductivity
Int. Journal of Math. Analyss, Vol. 6, 212, no. 22, 195-114 Unqueness of Weak Solutons to the 3D Gnzburg- Landau Model for Superconductvty Jshan Fan Department of Appled Mathematcs Nanjng Forestry Unversty
More informationA Hybrid Variational Iteration Method for Blasius Equation
Avalable at http://pvamu.edu/aam Appl. Appl. Math. ISSN: 1932-9466 Vol. 10, Issue 1 (June 2015), pp. 223-229 Applcatons and Appled Mathematcs: An Internatonal Journal (AAM) A Hybrd Varatonal Iteraton Method
More informationOne-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 informationMMA and GCMMA two methods for nonlinear optimization
MMA and GCMMA two methods for nonlnear optmzaton Krster Svanberg Optmzaton and Systems Theory, KTH, Stockholm, Sweden. krlle@math.kth.se Ths note descrbes the algorthms used n the author s 2007 mplementatons
More informationOne 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 informationNumerical 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 informationRobert Eisberg Second edition CH 09 Multielectron atoms ground states and x-ray excitations
Quantum Physcs 量 理 Robert Esberg Second edton CH 09 Multelectron atoms ground states and x-ray exctatons 9-01 By gong through the procedure ndcated n the text, develop the tme-ndependent Schroednger equaton
More informationNON 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 informationThe equation of motion of a dynamical system is given by a set of differential equations. That is (1)
Dynamcal Systems Many engneerng and natural systems are dynamcal systems. For example a pendulum s a dynamcal system. State l The state of the dynamcal system specfes t condtons. For a pendulum n the absence
More informationHEAT TRANSFER THROUGH ANNULAR COMPOSITE FINS
Journal of Mechancal Engneerng and Technology (JMET) Volume 4, Issue 1, Jan-June 2016, pp. 01-10, Artcle ID: JMET_04_01_001 Avalable onlne at http://www.aeme.com/jmet/ssues.asp?jtype=jmet&vtype=4&itype=1
More informationNUMERICAL 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 informationUNIVERSITY OF BOLTON RAK ACADEMIC CENTRE BENG(HONS) MECHANICAL ENGINEERING SEMESTER TWO EXAMINATION 2017/2018 FINITE ELEMENT AND DIFFERENCE SOLUTIONS
OCD0 UNIVERSITY OF BOLTON RAK ACADEMIC CENTRE BENG(HONS) MECHANICAL ENGINEERING SEMESTER TWO EXAMINATION 07/08 FINITE ELEMENT AND DIFFERENCE SOLUTIONS MODULE NO. AME6006 Date: Wednesda 0 Ma 08 Tme: 0:00
More informationWeek3, 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 informationLecture 12: Discrete Laplacian
Lecture 12: Dscrete Laplacan Scrbe: Tanye Lu Our goal s to come up wth a dscrete verson of Laplacan operator for trangulated surfaces, so that we can use t n practce to solve related problems We are mostly
More informationLecture 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 informationPlease initial the statement below to show that you have read it
EN0: Structural nalyss Exam I Wednesday, March 2, 2005 Dvson of Engneerng rown Unversty NME: General Instructons No collaboraton of any nd s permtted on ths examnaton. You may consult your own wrtten lecture
More informationORIGIN 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 informationPhysics 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 informationSupporting Information Part 1. DFTB3: Extension of the self-consistent-charge. density-functional tight-binding method (SCC-DFTB)
Supportng Informaton Part 1 DFTB3: Extenson of the self-consstent-charge densty-functonal tght-ndng method SCC-DFTB Mchael Gaus, Qang Cu, and Marcus Elstner, Insttute of Physcal Chemstry, Karlsruhe Insttute
More informationPulse Coded Modulation
Pulse Coded Modulaton PCM (Pulse Coded Modulaton) s a voce codng technque defned by the ITU-T G.711 standard and t s used n dgtal telephony to encode the voce sgnal. The frst step n the analog to dgtal
More informationSOME ASPECTS OF THE EXISTENCE OF COULOMB VIBRATIONS IN A COMPOSITE BAR
SISOM 006, Bucharest 7-9 May SOME ASPECTS OF THE EXISTECE OF COULOMB VIBRATIOS I A COMPOSITE BAR Ştefana DOESCU Techncal Unversty of Cvl Engneerng, Dept. of Mathematcs, emal: stefa05@rdsln.ro. In ths paper,
More informationMAE140 - Linear Circuits - Winter 16 Final, March 16, 2016
ME140 - Lnear rcuts - Wnter 16 Fnal, March 16, 2016 Instructons () The exam s open book. You may use your class notes and textbook. You may use a hand calculator wth no communcaton capabltes. () You have
More informationAPPROXIMATE 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 informationDESIGN OPTIMIZATION OF CFRP RECTANGULAR BOX SUBJECTED TO ARBITRARY LOADINGS
Munch, Germany, 26-30 th June 2016 1 DESIGN OPTIMIZATION OF CFRP RECTANGULAR BOX SUBJECTED TO ARBITRARY LOADINGS Q.T. Guo 1*, Z.Y. L 1, T. Ohor 1 and J. Takahash 1 1 Department of Systems Innovaton, School
More informationNumerical Solution of Ordinary Differential Equations
Numercal Methods (CENG 00) CHAPTER-VI Numercal Soluton of Ordnar Dfferental Equatons 6 Introducton Dfferental equatons are equatons composed of an unknown functon and ts dervatves The followng are examples
More informationThe Two-scale Finite Element Errors Analysis for One Class of Thermoelastic Problem in Periodic Composites
7 Asa-Pacfc Engneerng Technology Conference (APETC 7) ISBN: 978--6595-443- The Two-scale Fnte Element Errors Analyss for One Class of Thermoelastc Problem n Perodc Compostes Xaoun Deng Mngxang Deng ABSTRACT
More informationSecond 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 informationRELIABILITY ASSESSMENT
CHAPTER Rsk Analyss n Engneerng and Economcs RELIABILITY ASSESSMENT A. J. Clark School of Engneerng Department of Cvl and Envronmental Engneerng 4a CHAPMAN HALL/CRC Rsk Analyss for Engneerng Department
More informationApplied Mathematics Letters
Appled Matheatcs Letters 2 (2) 46 5 Contents lsts avalable at ScenceDrect Appled Matheatcs Letters journal hoepage: wwwelseverco/locate/al Calculaton of coeffcents of a cardnal B-splne Gradr V Mlovanovć
More informationThe Tangential Force Distribution on Inner Cylinder of Power Law Fluid Flowing in Eccentric Annuli with the Inner Cylinder Reciprocating Axially
Open Journal of Flud Dynamcs, 2015, 5, 183-187 Publshed Onlne June 2015 n ScRes. http://www.scrp.org/journal/ojfd http://dx.do.org/10.4236/ojfd.2015.52020 The Tangental Force Dstrbuton on Inner Cylnder
More informationComputing Nonequilibrium Conformational Dynamics of Structured Nucleic Acid Assemblies
Supportng Informaton for Computng Nonequlbrum Conformatonal Dynamcs of Structured Nuclec Acd Assembles Reza Sharf Sedeh,, Keyao Pan,, Matthew Ralph Adendorff, Oskar Hallatschek, Klaus-Jürgen Bathe,*, and
More informationGlobal Sensitivity. Tuesday 20 th February, 2018
Global Senstvty Tuesday 2 th February, 28 ) Local Senstvty Most senstvty analyses [] are based on local estmates of senstvty, typcally by expandng the response n a Taylor seres about some specfc values
More informationTHREE-DIMENSION DYNAMIC SOIL-STRUCTURE INTERACTION ANALYSIS USING THE SUBSTRUCTURE METHOD IN THE TIME DOMAIN
The 4 th October 2-7 2008 Bejng Chna THREE-DIENSION DYNAIC SOIL-STRUCTURE INTERACTION ANALYSIS USING THE SUBSTRUCTURE ETHOD IN THE TIE DOAIN X..Yang Y.Chen and B.P.Yang 2 Assocate Professor aculty of Constructon
More information11. Dynamics in Rotating Frames of Reference
Unversty of Rhode Island DgtalCommons@URI Classcal Dynamcs Physcs Course Materals 2015 11. Dynamcs n Rotatng Frames of Reference Gerhard Müller Unversty of Rhode Island, gmuller@ur.edu Creatve Commons
More informationSolutions for Homework #9
Solutons for Hoewor #9 PROBEM. (P. 3 on page 379 n the note) Consder a sprng ounted rgd bar of total ass and length, to whch an addtonal ass s luped at the rghtost end. he syste has no dapng. Fnd the natural
More informationOFF-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 information5.04, Principles of Inorganic Chemistry II MIT Department of Chemistry Lecture 32: Vibrational Spectroscopy and the IR
5.0, Prncples of Inorganc Chemstry II MIT Department of Chemstry Lecture 3: Vbratonal Spectroscopy and the IR Vbratonal spectroscopy s confned to the 00-5000 cm - spectral regon. The absorpton of a photon
More information