Statically indeterminate examples - axial loaded members, rod in torsion, members in bending
|
|
- Daniel Simpson
- 5 years ago
- Views:
Transcription
1 Elsticity nd Plsticity Stticlly indeterminte exmples - xil loded memers, rod in torsion, memers in ending Deprtment of Structurl Mechnics Fculty of Civil Engineering, VSB - Technicl University Ostrv 1 / 8
2 Stticlly indeterminte structures Condition of solution: elstic (liner) ehviour of strin-stress digrm of mteril Stticlly indetermined prolems: numer of unknown vriles > numer of equilirium equtions Solution: numer of unknown vriles numer of equilirium + equtions numer of deformtion conditions Stticlly determined nd indetermined exmples / 8
3 Axilly loded memers 1. Fixed supported column on oth end. Rods 3. Nehomogenized r (steel pipe filled in y concret). 3 / 8
4 Exmple 1: Fixed supported column on oth ends R l Condition of solution: elstic (liner) ehviour of strin-stress digrm of mteril Unknown vriles in exmple: R ( N ) R ( ), N 1 F l 1 l Equilirium eqution: R 0 : R + R F 0 z N1 + N F 0 Deformtion eqution: R l 0 : l N1l1 Nl + E1. A1 E. A 1 + l 0 Stticlly determined nd indetermined exmples 4 / 8
5 Determine norml stress in oth prts, cross sections I140 nd I180, F650kN. N 1 R + N - -R Exmple 1 I 140 I 180 R F R l 1 1,5m l,5m We cn determine the unknows just from the one eqution deformtion condition. 1) 1x stticlly indetermined in the xil tsk ) Equilirium equtions (just xil tsk): F i,verticl 0 R + R F 0 3) Deformtion condition: l 0 From the digrm ohf norml forces : 1 R N R F N N l1 Nl R 1 ( ) 1 l R F l EA EA EA EA 1 l l + l 1 By sustituting into the deformtion condition: 1 0 R F l l A 1 A1 + l 1 A N 1 R N R - F ( -R) 5 / 8
6 Exmple 1 Determine norml stress in oth prts, cross sections I140 nd I180, F650kN. R R N1 R 338, 58kN N 1 + I 140 F l 1 1,5m N 311, 4kN Norml stress in the r: N - -R I 180 R l,5m N1 σ x1 186, 03MP A 1 N σ x 111, 6MP A 6 / 8
7 Exmple The r is loded y forces see the picture. A 1 3cm, A 10cm, E 1 E, F 1 0kN, F 45kN. Guess the direction of the rections nd digrm of norml forces Divide the r on prts, where there will e different vlue of stresses nd clculte them. x Results.: N 1 1,875kN N -18,15kN N 3 6,85kN R 6,85kN R 1,875kN F 1 F 1 0,6m 0,8m 0,4m σ 1 6,5MP σ -18,15MP σ 3 6,875MP 7 / 8
8 Exmple Determine norml stress in the r U100, which is under the temperture chnge T90 C. l6m, E, MP, α T 1, 10 5 [ ] o 1 C ΔT 1) 1x stticlly indetermined in the xil tsk ) Equilirium equtions (just xil tsk): F i,x 0 R R 0 R R N R R 3) Deformtion condition: 4) Norml stress in the r: N l 0 Nl l + αt T l EA N αt T EA 0 55,15 kn σ x N A 06,8MP We cn determine the unknows just from the one eqution deformtion condition. 8 / 8
9 Exmple 3 The r of the lenght l 1 m is etween two stiff wlls, the hole is 0, mm. Wht vlue of norml stress is in the rod, if the temperture chnge is +50 C? α T C -1, E 1, MP 0, mm l 1000 mm 1) Deformtion eqution: l 0, 10 Nl EA 3 m + αt T l 0, 10 ) Result: 3 σx 71,5MP 9 / 8
10 Exmple 4 Determine stress in the rods, if oth re from I 140. Conditions of solution: elstic ehviour of the rods, idelly stiff sl 1 g 10 knm -1 c l 1 m 3 m 4 m L 7 m 10 / 8
11 Exmple 4 Determine stress in the rods, if oth re from I 140. Conditions of solution: elstic ehviour of the rods, stiff ehviour of the em. 1) 1x stticlly indetermined ) Equilirium equtions : R R c F ix 0 R x 1 g l 1 m F iz 0 M i 0 3) Deformtion condition: 3 m 4 m R z L 7 m 11 / 8
12 Exmple 4 Determine stress in the rods, if oth re from I 140. (Equilirium equtions): F ix 0 F iz 0 M i 0 1 l 1 c l l 1 m l1 l + N l EA N 1 g N N1l 1 1 EA ( + ) ( unknowns forces N 1, N, choose n eqution from Equilirium equtions, which includes just N 1 N ) N 3) Deformtion condition: N 7 q 7 3,5 0 1 / 8
13 Exmple 5 Determine N in rods. I 450, 1m. Conditions of solution: elstic ehviour of the rods, idelly stiff sl c 1 3 l 1 m F 400 kn 13 / 8
14 Exmple 5 Determine norml forces in the rods. Cross sections re I ) 1x stticlly indetermined in the xil ts R R R c c N N 1 N N 3 N N 3 ) Equilirium conditions: l 1 m F ix 0 F iz 0 M i 0 R N 1, R N, R c N 3 F 400 kn 14 / 8
15 Exmple 5 Determine norml forces in the rods. Cross sections re I 450. Deformtion of construction: c 1 3 l 1 m l l 3 l 1 F 400 kn 15 / 8
16 Exmple 5 Determine norml forces in the rods. Cross sections re I ) Deformtion condition: l 1 c 1 3 l 1 m l l 3 (coordinte system) y x z l1 l3 l l3 4 (3 unknowns forces N 1, N, N 3, choose equtions from Equilirium equtions) Chosen equtions: F iz 0 M i 0 16 / 8
17 Exmple 5 Solution: 1 3 N 1 N N 3 F 400 kn results: N 1 450kN, N 1400kN, N 3 350kN y z c x l 1 m Deform. condition: l1 l3 l l3 4 l l1 + l3 N l/ean 1 l/ea+n 3 l/ea Equilirium equtions: F iz 0 -N 1 - N - N 3 + F d 0 M i M i 0..N +4..N 3.F d 0 17 / 8
18 Exmple 6 Nehomogenized r (steel pipe filled in y concret). Determine norml stress in steel nd concret. d 1 80 mm (externl dimeter), d 70 mm (internl dimeter). E 10GP, E cm 4GP. Conditions of solution: - elstic ehviour of mterils, - F ffects uniformly to the section F 11 kn 1) 1x internlly stticlly indetermined l 0,5 m 18 / 8
19 N N o + N B N N O - - Exmple 6 F ) Deformtion eqution: l S l C l 0,5 m N sl E s A s Ncl E A ( unknowns, we tke one eqution from equilirium equtions) 3) Equilirium equtions: c F i,verticl 0 N B F - R 0 R F -N - N S - N C (F R 0) c F + N S + N C 0 3) Stresses: R σ S N A S, σ S N A C C results: N S -81,65kN, N C -30,35kN, σ S -69,31MP, σ C -7,91MP 19 / 8
20 Exmple 7: Reinforced concrete column Condition of solution: Elstic (liner) ehviour of strin-stress digrm of mteril nd uniform ffect of lod to cross-section re F steel Unknown vriles in exmple: N s, N c Equilirium eqution: F N s + N c concrete Deformtion eqution: l s l c N s. l E. A s s Nc. l E. A c c Stticlly determined nd indetermined exmples 0 / 8
21 Stticlly indeterminte prolems in torsion Both fixed ended shft l1 l l Condition of solution: liner elstic ehviour of mteril M x, M x, c M x, M x, + T c M x, Unknowns: M x, ( M x,1 ), M x, ( M x, ) Equilirium equtions: M i 0 : x, M x, M x, + M x, c 0 Deformtion condition: ϕ i 0 : i 1 T.l G.I i i i t, i 0 Stticlly indeterminte prolems 1 / 8
22 Stticlly indeterminte prolems in ending Methods of computing of stticlly indeterminte endings ems: ) Fourth-order integrtion of the function of lod ) Force method c) Methods sed on energetic principles (Elsticity nd plsticity II.) Fourth-Order Integrtion of differentil eqution (from the function of lod) Schwedlers reltions w ϕ y w M y E. I y. w Vz E. I y. w q ( x)? z E. I. w y IV E. I. w E. I E. I IV y q x y y ( ). w q + C1 V ( x) z. w q + C1. x + C M ( x) y x E. J. w y q + C1. + C. x + C ( x) 3 3 x x E. I y. w q + C1. + C. + C. x + C 6 ( x) 3 4 Solution: 4 unknowns C 1 C, C3,, C 4 oundry conditions 4 Stticlly indeterminte prolems in ending Fourth-order Integrtion / 8
23 Stticl nd deformtion oundry conditions Type of the end (oundry) Deformtion Boundry Condition Stticl Boundry Condition Free end w 0 ϕ 0 M 0 w 0 V 0 w 0 Simply supported end Fixed end w 0 ϕ 0 w 0 ϕ 0 M 0 w 0 V 0 w 0 M 0 w 0 V 0 w 0 Stticlly indeterminte prolems in ending Fourth-order Integrtion 3 / 8
24 Fourth-Order Integrtion of differentil eqution Exmple 1 Determine the digrms of internl forces (V, M) t stticlly indeterminte em. Use differentil reltions. q l 4 / 8
25 Fourth-Order Integrtion of differentil eqution Boundry conditions: 5 / 8
26 Fourth-Order Integrtion of differentil eqution 6 / 8
27 Fourth-Order Integrtion of differentil eqution Exmple Determine the internl forces (V, M) t stticlly indeterminte em y the Fourth-order integrtion of differentil eqution. q l Equtions the sme s Exmple 1, oundry conditions different 7 / 8
28 Force method Principle of the Force method: q( x ) q z ϕ Deformtion conditions: 0 ϕ ϕ ϕ, q +, M Superposition 0 + q( x ) Superposition ϕ, q 0 ϕ, M 0 q z M y Designte one of the rections s redundnt nd eliminte it The redundnt rection is then treted s n unknown lod tht together with other lods must produce deformtions tht re comptile with the originl supports The deflection or ngulr rottion t the point where the support hs een eliminted is otined y computing seprtely - the deformtions cused y the given lods nd y the redundnt rection Results will e otined y superposition Stticlly indeterminte prolems in ending Force method 8 / 8
29 Exmple 1 Force method Determine the digrms of internl forces (V, M) t stticlly indeterminte em. Use the Force method (method of superposition). q l Deformtion condition: w,q + w,r 0 q l R 9 / 8
30 Exmple 1 Force method Deformtion condition: w,q + w,r 0 w,q w,r 4 q.l 8.EI R.l/ 3.EI 3 Determine other rections from equilirium conditions nd construct the digrms of internl forces. 30 / 8
31 Exmple Force method Determine the internl forces (V, M) t stticlly indeterminte em y the Force method. (redundnt rection is M ) q ϕ 0 Deformtion condition: ϕ,q + ϕ,m 0 q ϕ,m M ϕ,q 31 / 8
32 Exmple Force method q ϕ,q q.l 3 4.EI ϕ,q ϕ,m M ϕ,m M.l 3.EI Deformtion condition: Other rections from equilirium conditions 3 / 8
Theme 8 Stability and buckling of members
Elsticity nd plsticity Theme 8 Stility nd uckling o memers Euler s solution o stility o n xilly compressed stright elstic memer Deprtment o Structurl Mechnics culty o Civil Engineering, VSB - Technicl
More informationModule 1. Energy Methods in Structural Analysis
Module 1 Energy Methods in Structurl Anlysis Lesson 4 Theorem of Lest Work Instructionl Objectives After reding this lesson, the reder will be ble to: 1. Stte nd prove theorem of Lest Work.. Anlyse stticlly
More informationTheme 9 Stability and buckling of members
Elsticit n plsticit Theme 9 Stilit n uckling o memers Euler s solution o stilit o stright elstic memer uner pressure Deprtment o Structurl Mechnics cult o Civil Engineering, VSB - Technicl Universit Ostrv
More informationBME 207 Introduction to Biomechanics Spring 2018
April 6, 28 UNIVERSITY O RHODE ISAND Deprtment of Electricl, Computer nd Biomedicl Engineering BME 27 Introduction to Biomechnics Spring 28 Homework 8 Prolem 14.6 in the textook. In ddition to prts -e,
More informationChapter 5 Bending Moments and Shear Force Diagrams for Beams
Chpter 5 ending Moments nd Sher Force Digrms for ems n ddition to illy loded brs/rods (e.g. truss) nd torsionl shfts, the structurl members my eperience some lods perpendiculr to the is of the bem nd will
More information1 Bending of a beam with a rectangular section
1 Bending of bem with rectngulr section x3 Episseur b M x 2 x x 1 2h M Figure 1 : Geometry of the bem nd pplied lod The bem in figure 1 hs rectngur section (thickness 2h, width b. The pplied lod is pure
More informationModule 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method. Version 2 CE IIT, Kharagpur
Module Anlysis of Stticlly Indeterminte Structures by the Mtrix Force Method Version CE IIT, Khrgpur esson 8 The Force Method of Anlysis: Bems Version CE IIT, Khrgpur Instructionl Objectives After reding
More informationRigid Frames - Compression & Buckling
ARCH 614 Note Set 11.1 S014n Rigid Frmes - Compression & Buckling Nottion: A = nme or re d = nme or depth E = modulus o elsticity or Young s modulus = xil stress = ending stress z = stress in the x direction
More informationV. DEMENKO MECHANICS OF MATERIALS LECTURE 6 Plane Bending Deformation. Diagrams of Internal Forces (Continued)
V. DEMENKO MECHNCS OF MTERLS 015 1 LECTURE 6 Plne ending Deformtion. Digrms of nternl Forces (Continued) 1 Construction of ending Moment nd Shering Force Digrms for Two Supported ems n this mode of loding,
More informationAvailable online at ScienceDirect. Procedia Engineering 190 (2017 )
Aville online t www.sciencedirect.com ScienceDirect Procedi Engineering 19 (217 ) 237 242 Structurl nd Physicl Aspects of Construction Engineering Numericl Anlysis of Steel Portl Frme Exposed to Fire Lenk
More informationExplain shortly the meaning of the following eight words in relation to shells structures.
Delft University of Technology Fculty of Civil Engineering nd Geosciences Structurl Mechnics Section Write your nme nd study number t the top right-hnd of your work. Exm CIE4143 Shell Anlysis Tuesdy 15
More informationColumns and Stability
ARCH 331 Note Set 1. Su01n Columns nd Stilit Nottion: A = nme or re A36 = designtion o steel grde = nme or width C = smol or compression C c = column slenderness clssiiction constnt or steel column design
More informationPlates on elastic foundation
Pltes on elstic foundtion Circulr elstic plte, xil-symmetric lod, Winkler soil (fter Timoshenko & Woinowsky-Krieger (1959) - Chpter 8) Prepred by Enzo Mrtinelli Drft version ( April 016) Introduction Winkler
More informationReview of Gaussian Quadrature method
Review of Gussin Qudrture method Nsser M. Asi Spring 006 compiled on Sundy Decemer 1, 017 t 09:1 PM 1 The prolem To find numericl vlue for the integrl of rel vlued function of rel vrile over specific rnge
More informationShear and torsion interaction of hollow core slabs
Competitive nd Sustinble Growth Contrct Nº G6RD-CT--6 Sher nd torsion interction of hollow core slbs HOLCOTORS Technicl Report, Rev. Anlyses of hollow core floors December The content of the present publiction
More informationIntroduction to statically indeterminate structures
Sttics of Buiding Structures I., EASUS Introduction to stticy indeterminte structures Deprtment of Structur echnics Fcuty of Civi Engineering, VŠB-Technic University of Ostrv Outine of Lecture Stticy indeterminte
More informationThomas Whitham Sixth Form
Thoms Whithm Sith Form Pure Mthemtics Unit C Alger Trigonometry Geometry Clculus Vectors Trigonometry Compound ngle formule sin sin cos cos Pge A B sin Acos B cos Asin B A B sin Acos B cos Asin B A B cos
More informationMECHANICS OF MATERIALS
9 The cgrw-hill Compnies, Inc. All rights reserved. Fifth SI Edition CHAPTER 5 ECHANICS OF ATERIALS Ferdinnd P. Beer E. Russell Johnston, Jr. John T. DeWolf Dvid F. zurek Lecture Notes: J. Wlt Oler Texs
More informationdy ky, dt where proportionality constant k may be positive or negative
Section 1.2 Autonomous DEs of the form 0 The DE y is mthemticl model for wide vriety of pplictions. Some of the pplictions re descried y sying the rte of chnge of y(t) is proportionl to the mount present.
More informationCOLLEGE OF ENGINEERING AND TECHNOLOGY
COLLEGE OF ENGNEERNG ND TECHNOLOGY DEPRTMENT : Construction nd uilding Engineering COURSE : Structurl nlysis 2 COURSE NO : C 343 LECTURER : Dr. Mohmed SFN T. SSSTNT : Eng. Mostf Yossef, Eng. l-hussein
More informationSolution Manual. for. Fracture Mechanics. C.T. Sun and Z.-H. Jin
Solution Mnul for Frcture Mechnics by C.T. Sun nd Z.-H. Jin Chpter rob.: ) 4 No lod is crried by rt nd rt 4. There is no strin energy stored in them. Constnt Force Boundry Condition The totl strin energy
More informationANALYSIS OF MECHANICAL PROPERTIES OF COMPOSITE SANDWICH PANELS WITH FILLERS
ANALYSIS OF MECHANICAL PROPERTIES OF COMPOSITE SANDWICH PANELS WITH FILLERS A. N. Anoshkin *, V. Yu. Zuiko, A.V.Glezmn Perm Ntionl Reserch Polytechnic University, 29, Komsomolski Ave., Perm, 614990, Russi
More informationConsequently, the temperature must be the same at each point in the cross section at x. Let:
HW 2 Comments: L1-3. Derive the het eqution for n inhomogeneous rod where the therml coefficients used in the derivtion of the het eqution for homogeneous rod now become functions of position x in the
More informationExam CT3109 STRUCTURAL MECHANICS april 2011, 09:00 12:00 hours
Subfculty of Civil Engineering rk ech ge with your: Structurl echnics STUDENT NUBER : NAE : Em CT309 STRUCTURAL ECHANICS 4 ril 0, 09:00 :00 hours This em consists of 4 roblems. Use for ech roblem serte
More informationEvaluating Definite Integrals. There are a few properties that you should remember in order to assist you in evaluating definite integrals.
Evluting Definite Integrls There re few properties tht you should rememer in order to ssist you in evluting definite integrls. f x dx= ; where k is ny rel constnt k f x dx= k f x dx ± = ± f x g x dx f
More informationCE 160 Lab 2 Notes: Shear and Moment Diagrams for Beams
E 160 Lb 2 Notes: Sher nd oment Digrms for ems Sher nd moment digrms re plots of how the internl bending moment nd sher vry long the length of the bem. Sign onvention for nd onsider the rbitrrily loded
More informationEquations of Motion. Figure 1.1.1: a differential element under the action of surface and body forces
Equtions of Motion In Prt I, lnce of forces nd moments cting on n component ws enforced in order to ensure tht the component ws in equilirium. Here, llownce is mde for stresses which vr continuousl throughout
More informationSUPPLEMENTARY INFORMATION
DOI:.38/NMAT343 Hybrid Elstic olids Yun Li, Ying Wu, Ping heng, Zho-Qing Zhng* Deprtment of Physics, Hong Kong University of cience nd Technology Cler Wter By, Kowloon, Hong Kong, Chin E-mil: phzzhng@ust.hk
More informationThin and Thick Cylinders and Spheres
CHAPTR 8 Thin nd Thick Cylinders nd Spheres Prolem. A shell.5 m long nd m dimeter, is sujected to n internl pressure of. N/mm. If the thickness of the shell is 0 mm find the circumferentil nd longitudinl
More informationThe Complete Part Design Handbook
The Complete Prt Design Hndbook For Injection Molding of Thermoplstics Berbeitet von E. Alfredo Cmpo 1. Auflge 006. Buch. XXI, 870 S. Hrdcover ISBN 978 3 6 0309 3 Formt (B x L): 1,5 x 7,7 cm Geicht: 3050
More informationTrigonometric Functions
Exercise. Degrees nd Rdins Chpter Trigonometric Functions EXERCISE. Degrees nd Rdins 4. Since 45 corresponds to rdin mesure of π/4 rd, we hve: 90 = 45 corresponds to π/4 or π/ rd. 5 = 7 45 corresponds
More informationeleven rigid frames: compression & buckling Rigid Frames Rigid Frames Rigid Frames ELEMENTS OF ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN
ELEMENTS O RCHITECTURL STRUCTURES: ORM, BEHVIOR, ND DESIGN DR. NNE NICHOLS SRING 018 lecture eleven rigid rmes: compression & uckling Rigid rmes 1 Lecture 11 S009n http:// nisee.erkeley.edu/godden Rigid
More informationAns. Ans. Ans. Ans. Ans. Ans.
08 Solutions 46060 5/28/10 8:34 M Pge 532 8 1. sphericl gs tnk hs n inner rdius of r = 1.5 m. If it is subjected to n internl pressure of p = 300 kp, determine its required thickness if the mximum norml
More informationx = a To determine the volume of the solid, we use a definite integral to sum the volumes of the slices as we let!x " 0 :
Clculus II MAT 146 Integrtion Applictions: Volumes of 3D Solids Our gol is to determine volumes of vrious shpes. Some of the shpes re the result of rotting curve out n xis nd other shpes re simply given
More informationA - INTRODUCTION AND OVERVIEW
MMJ5 COMPUTATIONAL METHOD IN SOLID MECHANICS A - INTRODUCTION AND OVERVIEW INTRODUCTION AND OVERVIEW M.N. Tmin, CSMLb, UTM MMJ5 COMPUTATIONAL METHOD IN SOLID MECHANICS Course Content: A INTRODUCTION AND
More informationWhy symmetry? Symmetry is often argued from the requirement that the strain energy must be positive. (e.g. Generalized 3-D Hooke s law)
Why symmetry? Symmetry is oten rgued rom the requirement tht the strin energy must be positie. (e.g. Generlized -D Hooke s lw) One o the derities o energy principles is the Betti- Mxwell reciprocity theorem.
More informationA Brief Note on Quasi Static Thermal Stresses In A Thin Rectangular Plate With Internal Heat Generation
Americn Journl of Engineering Reserch (AJER) 13 Americn Journl of Engineering Reserch (AJER) e-issn : 3-847 p-issn : 3-936 Volume-, Issue-1, pp-388-393 www.jer.org Reserch Pper Open Access A Brief Note
More informationDesigning Information Devices and Systems I Discussion 8B
Lst Updted: 2018-10-17 19:40 1 EECS 16A Fll 2018 Designing Informtion Devices nd Systems I Discussion 8B 1. Why Bother With Thévenin Anywy? () Find Thévenin eqiuvlent for the circuit shown elow. 2kΩ 5V
More informationSection 4: Integration ECO4112F 2011
Reding: Ching Chpter Section : Integrtion ECOF Note: These notes do not fully cover the mteril in Ching, ut re ment to supplement your reding in Ching. Thus fr the optimistion you hve covered hs een sttic
More informationMAC-solutions of the nonexistent solutions of mathematical physics
Proceedings of the 4th WSEAS Interntionl Conference on Finite Differences - Finite Elements - Finite Volumes - Boundry Elements MAC-solutions of the nonexistent solutions of mthemticl physics IGO NEYGEBAUE
More information99/105 Comparison of OrcaFlex with standard theoretical results
99/105 Comprison of OrcFlex ith stndrd theoreticl results 1. Introduction A number of stndrd theoreticl results from literture cn be modelled in OrcFlex. Such cses re, by virtue of being theoreticlly solvble,
More information2. VECTORS AND MATRICES IN 3 DIMENSIONS
2 VECTORS AND MATRICES IN 3 DIMENSIONS 21 Extending the Theory of 2-dimensionl Vectors x A point in 3-dimensionl spce cn e represented y column vector of the form y z z-xis y-xis z x y x-xis Most of the
More informationPROPERTIES OF AREAS In general, and for an irregular shape, the definition of the centroid at position ( x, y) is given by
PROPERTES OF RES Centroid The concept of the centroid is prol lred fmilir to ou For plne shpe with n ovious geometric centre, (rectngle, circle) the centroid is t the centre f n re hs n is of smmetr, the
More informationEFFECTIVE BUCKLING LENGTH OF COLUMNS IN SWAY FRAMEWORKS: COMPARISONS
IV EFFETIVE BUING ENGTH OF OUMN IN WAY FRAMEWOR: OMARION Ojectives In the present context, two different pproches re eployed to deterine the vlue the effective uckling length eff n c of colun n c out the
More information6.5 Plate Problems in Rectangular Coordinates
6.5 lte rolems in Rectngulr Coordintes In this section numer of importnt plte prolems ill e emined ug Crte coordintes. 6.5. Uniform ressure producing Bending in One irection Consider first the cse of plte
More informationM344 - ADVANCED ENGINEERING MATHEMATICS
M3 - ADVANCED ENGINEERING MATHEMATICS Lecture 18: Lplce s Eqution, Anltic nd Numericl Solution Our emple of n elliptic prtil differentil eqution is Lplce s eqution, lso clled the Diffusion Eqution. If
More informationThe Wave Equation I. MA 436 Kurt Bryan
1 Introduction The Wve Eqution I MA 436 Kurt Bryn Consider string stretching long the x xis, of indeterminte (or even infinite!) length. We wnt to derive n eqution which models the motion of the string
More information4.5 Material Anisotropy
. Mteril Anisoopy.. Mteril Symmey he isoopic mteril ws defined s one whose mteril response ws unffected y rigid ody rottions of the reference configurtion. Other mteril symmeies re possile; to generlise
More informationTHEORY OF VIBRATIONS OF TETRA-ATOMIC SYMMETRIC BENT MOLECULES
terils Physics nd echnics (0 9- Received: rch 0 THEORY OF VIRTIONS OF TETR-TOIC SYETRIC ENT OLECLES lexnder I eler * ri Krupin Vitly Kotov Deprtment of Physics of Strength nd Plsticity of terils Deprtment
More information10.2 The Ellipse and the Hyperbola
CHAPTER 0 Conic Sections Solve. 97. Two surveors need to find the distnce cross lke. The plce reference pole t point A in the digrm. Point B is meters est nd meter north of the reference point A. Point
More informationChapter E - Problems
Chpter E - Prolems Blinn College - Physics 2426 - Terry Honn Prolem E.1 A wire with dimeter d feeds current to cpcitor. The chrge on the cpcitor vries with time s QHtL = Q 0 sin w t. Wht re the current
More informationMASKING OF FERROMAGNETIC ELLIPTICAL SHELL IN TRANSVERSE MAGNETIC FIELD
POZNAN UNVE RSTY OF TE HNOLOGY AADE M JOURNALS No 7 Electricl Engineering Kzimierz JAKUUK* Mirosł WOŁOSZYN* Peł ZMNY* MASKNG OF FERROMAGNET ELLPTAL SHELL N TRANSVERSE MAGNET FELD A ferromgnetic oject,
More informationLecture Solution of a System of Linear Equation
ChE Lecture Notes, Dept. of Chemicl Engineering, Univ. of TN, Knoville - D. Keffer, 5/9/98 (updted /) Lecture 8- - Solution of System of Liner Eqution 8. Why is it importnt to e le to solve system of liner
More informationLinear Inequalities. Work Sheet 1
Work Sheet 1 Liner Inequlities Rent--Hep, cr rentl compny,chrges $ 15 per week plus $ 0.0 per mile to rent one of their crs. Suppose you re limited y how much money you cn spend for the week : You cn spend
More informationELASTICITY AND PLASTICITY I
ELASTICITY AD PLASTICITY I Litertur in Czech Ing. Lenk Lusová LPH 407/1 te. 59 73 136 enk.usov@vs.cz http://fst10.vs.cz/usov Literture: Higgeer Sttics nd mechnics of mteri, USA 199 Beer, Johnston, DeWof,
More informationSection 6.1 INTRO to LAPLACE TRANSFORMS
Section 6. INTRO to LAPLACE TRANSFORMS Key terms: Improper Integrl; diverge, converge A A f(t)dt lim f(t)dt Piecewise Continuous Function; jump discontinuity Function of Exponentil Order Lplce Trnsform
More informationCalculus Module C21. Areas by Integration. Copyright This publication The Northern Alberta Institute of Technology All Rights Reserved.
Clculus Module C Ares Integrtion Copright This puliction The Northern Alert Institute of Technolog 7. All Rights Reserved. LAST REVISED Mrch, 9 Introduction to Ares Integrtion Sttement of Prerequisite
More informationThis chapter will show you. What you should already know. 1 Write down the value of each of the following. a 5 2
1 Direct vrition 2 Inverse vrition This chpter will show you how to solve prolems where two vriles re connected y reltionship tht vries in direct or inverse proportion Direct proportion Inverse proportion
More informationPLEASE SCROLL DOWN FOR ARTICLE
This rticle ws downloded y:[knt, Trun] On: 8 Jnury 2008 Access Detils: [suscription numer 789308335] Pulisher: Tylor & Frncis Inform Ltd Registered in Englnd nd Wles Registered Numer: 1072954 Registered
More informationDesigning Information Devices and Systems I Spring 2018 Homework 7
EECS 16A Designing Informtion Devices nd Systems I Spring 2018 omework 7 This homework is due Mrch 12, 2018, t 23:59. Self-grdes re due Mrch 15, 2018, t 23:59. Sumission Formt Your homework sumission should
More informationNote 12. Introduction to Digital Control Systems
Note Introduction to Digitl Control Systems Deprtment of Mechnicl Engineering, University Of Ssktchewn, 57 Cmpus Drive, Ssktoon, SK S7N 5A9, Cnd . Introduction A digitl control system is one in which the
More informationPolynomials and Division Theory
Higher Checklist (Unit ) Higher Checklist (Unit ) Polynomils nd Division Theory Skill Achieved? Know tht polynomil (expression) is of the form: n x + n x n + n x n + + n x + x + 0 where the i R re the
More information10 Deflections due to Bending
1 Deflections due to Bending 1.1 The Moment/Curvture Reltion Just s we took the pure bending construction to be ccurte enough to produce useful estimtes of the norml stress due to bending for lodings tht
More informationFirst compression (0-6.3 GPa) First decompression ( GPa) Second compression ( GPa) Second decompression (35.
0.9 First ompression (0-6.3 GP) First deompression (6.3-2.7 GP) Seond ompression (2.7-35.5 GP) Seond deompression (35.5-0 GP) V/V 0 0.7 0.5 0 5 10 15 20 25 30 35 P (GP) Supplementry Figure 1 Compression
More informationThe Dirichlet Problem in a Two Dimensional Rectangle. Section 13.5
The Dirichlet Prolem in Two Dimensionl Rectngle Section 13.5 1 Dirichlet Prolem in Rectngle In these notes we will pply the method of seprtion of vriles to otin solutions to elliptic prolems in rectngle
More informationCHAPTER 7 TRANSPOSITION OF FORMULAE
CHAPTER 7 TRANSPOSITION OF FORMULAE EXERCISE 30, Pge 60 1. Mke d the subject of the formul: + b = c - d - e Since + b = c - d e then d = c e - b. Mke the subject of the formul: = 7 Dividing both sides
More informationPlate Bending Analysis by using a Modified Plate Theory
Copyright c 2006 Tech Science Press CMES, vol.11, no.3, pp.103-110, 2006 Plte Bending Anlysis y using Modified Plte Theory Y. Suetke 1 Astrct: Since Reissner nd Mindlin proposed their clssicl thick plte
More informationAQA Chemistry Paper 2
AQA hemistry Pper 2 1.1 A student is plnning n investigtion into how the concentrtion of hydrochloric cid ffects the rte of the rection with mrle chips. Wht is the independent vrile? Tick one ox. (1 mrk)
More informationA curve which touches each member of a given family of curves is called envelope of that family.
ENVELOPE A curve which touches ech memer of given fmil of curves is clle enveloe of tht fmil. Proceure to fin enveloe for the given fmil of curves: Cse : Enveloe of one rmeter fmil of curves Let us consier
More information( ) Same as above but m = f x = f x - symmetric to y-axis. find where f ( x) Relative: Find where f ( x) x a + lim exists ( lim f exists.
AP Clculus Finl Review Sheet solutions When you see the words This is wht you think of doing Find the zeros Set function =, fctor or use qudrtic eqution if qudrtic, grph to find zeros on clcultor Find
More informationOpen Access Prediction on Deflection of Z-Core Sandwich Panels in Weak Direction
Send Orders for Reprints to reprints@enthmsciencenet 88 The Open Ocen Engineering Journl 20 6 (Suppl- M7) 88-95 Open Access Prediction on Deflection of Z-Core Sndwich Pnels in Wek Direction Chen Cheng
More informationState space systems analysis (continued) Stability. A. Definitions A system is said to be Asymptotically Stable (AS) when it satisfies
Stte spce systems nlysis (continued) Stbility A. Definitions A system is sid to be Asymptoticlly Stble (AS) when it stisfies ut () = 0, t > 0 lim xt () 0. t A system is AS if nd only if the impulse response
More informationShear Force V: Positive shear tends to rotate the segment clockwise.
INTERNL FORCES IN EM efore a structural element can be designed, it is necessary to determine the internal forces that act within the element. The internal forces for a beam section will consist of a shear
More informationLecture 24: Laplace s Equation
Introductory lecture notes on Prtil Differentil Equtions - c Anthony Peirce. Not to e copied, used, or revised without explicit written permission from the copyright owner. 1 Lecture 24: Lplce s Eqution
More informationCalculus AB. For a function f(x), the derivative would be f '(
lculus AB Derivtive Formuls Derivtive Nottion: For function f(), the derivtive would e f '( ) Leiniz's Nottion: For the derivtive of y in terms of, we write d For the second derivtive using Leiniz's Nottion:
More informationThe contact stress problem for a piecewisely defined punch indenting an elastic half space. Jacques Woirgard
The contct stress prolem for pieceisely defined punch indenting n elstic hlf spce Jcques Woirgrd 5 Rue du Châteu de l Arceu 8633 Notre Dme d Or FRANC Astrct A solution for the contct stress prolem of n
More informationCBE 291b - Computation And Optimization For Engineers
The University of Western Ontrio Fculty of Engineering Science Deprtment of Chemicl nd Biochemicl Engineering CBE 9b - Computtion And Optimiztion For Engineers Mtlb Project Introduction Prof. A. Jutn Jn
More informationAvailable online at ScienceDirect. Procedia Engineering 172 (2017 )
Aville online t www.sciencedirect.com ScienceDirect Procedi Engineering 172 (2017 ) 218 225 Modern Building Mterils, Structures nd Techniques, MBMST 2016 Experimentl nd Numericl Anlysis of Direct Sher
More informationProblem 1. Solution: a) The coordinate of a point on the disc is given by r r cos,sin,0. The potential at P is then given by. r z 2 rcos 2 rsin 2
Prolem Consider disc of chrge density r r nd rdius R tht lies within the xy-plne. The origin of the coordinte systems is locted t the center of the ring. ) Give the potentil t the point P,,z in terms of,r,
More informationCOSC 3361 Numerical Analysis I Numerical Integration and Differentiation (III) - Gauss Quadrature and Adaptive Quadrature
COSC 336 Numericl Anlysis I Numericl Integrtion nd Dierentition III - Guss Qudrture nd Adptive Qudrture Edgr Griel Fll 5 COSC 336 Numericl Anlysis I Edgr Griel Summry o the lst lecture I For pproximting
More informationChapter 4: Techniques of Circuit Analysis. Chapter 4: Techniques of Circuit Analysis
Chpter 4: Techniques of Circuit Anlysis Terminology Node-Voltge Method Introduction Dependent Sources Specil Cses Mesh-Current Method Introduction Dependent Sources Specil Cses Comprison of Methods Source
More informationThings to Memorize: A Partial List. January 27, 2017
Things to Memorize: A Prtil List Jnury 27, 2017 Chpter 2 Vectors - Bsic Fcts A vector hs mgnitude (lso clled size/length/norm) nd direction. It does not hve fixed position, so the sme vector cn e moved
More information(4.1) D r v(t) ω(t, v(t))
1.4. Differentil inequlities. Let D r denote the right hnd derivtive of function. If ω(t, u) is sclr function of the sclrs t, u in some open connected set Ω, we sy tht function v(t), t < b, is solution
More informationDifferential Equations 2 Homework 5 Solutions to the Assigned Exercises
Differentil Equtions Homework Solutions to the Assigned Exercises, # 3 Consider the dmped string prolem u tt + 3u t = u xx, < x , u, t = u, t =, t >, ux, = fx, u t x, = gx. In the exm you were supposed
More informationPatch Antennas. Chapter Resonant Cavity Analysis
Chpter 4 Ptch Antenns A ptch ntenn is low-profile ntenn consisting of metl lyer over dielectric sustrte nd ground plne. Typiclly, ptch ntenn is fed y microstrip trnsmission line, ut other feed lines such
More informationGreen function and Eigenfunctions
Green function nd Eigenfunctions Let L e regulr Sturm-Liouville opertor on n intervl (, ) together with regulr oundry conditions. We denote y, φ ( n, x ) the eigenvlues nd corresponding normlized eigenfunctions
More informationPrecalculus Due Tuesday/Wednesday, Sept. 12/13th Mr. Zawolo with questions.
Preclculus Due Tuesd/Wednesd, Sept. /th Emil Mr. Zwolo (isc.zwolo@psv.us) with questions. 6 Sketch the grph of f : 7! nd its inverse function f (). FUNCTIONS (Chpter ) 6 7 Show tht f : 7! hs n inverse
More informationElectrical Drive 4 th Class
University Of Technology Electricl nd Electronics Deprtment Dr Nofl ohmmed Ther Al Kyt A drive consist of three min prts : prime mover; energy trnsmitting device nd ctul pprtus (lod), hich perform the
More informationKINEMATICS OF RIGID BODIES
KINEMTICS OF RIGID ODIES Introduction In rigid body kinemtics, e use the reltionships governing the displcement, velocity nd ccelertion, but must lso ccount for the rottionl motion of the body. Description
More informationNORMALS. a y a y. Therefore, the slope of the normal is. a y1. b x1. b x. a b. x y a b. x y
LOCUS 50 Section - 4 NORMALS Consider n ellipse. We need to find the eqution of the norml to this ellipse t given point P on it. In generl, we lso need to find wht condition must e stisfied if m c is to
More informationCase (a): Ans Ans. Case (b): ; s 1 = 65(4) Ans. s 1 = pr t. = 1.04 ksi. Ans. s 2 = pr 2t ; s 2 = 65(4) = 520 psi
8 3. The thin-wlled cylinder cn be supported in one of two wys s shown. Determine the stte of stress in the wll of the cylinder for both cses if the piston P cuses the internl pressure to be 65 psi. The
More informationDesign of T and L Beams in Flexure
Lecture 04 Design of T nd L Bems in Flexure By: Prof. Dr. Qisr Ali Civil Engineering Deprtment UET Peshwr drqisrli@uetpeshwr.edu.pk Prof. Dr. Qisr Ali CE 320 Reinforced Concrete Design Topics Addressed
More informationExploring parametric representation with the TI-84 Plus CE graphing calculator
Exploring prmetric representtion with the TI-84 Plus CE grphing clcultor Richrd Prr Executive Director Rice University School Mthemtics Project rprr@rice.edu Alice Fisher Director of Director of Technology
More informationBend Forms of Circular Saws and Evaluation of their Mechanical Properties
ISSN 139 13 MATERIALS SCIENCE (MEDŽIAGOTYRA). Vol. 11, No. 1. 5 Bend Forms of Circulr s nd Evlution of their Mechnicl Properties Kristin UKVALBERGIENĖ, Jons VOBOLIS Deprtment of Mechnicl Wood Technology,
More informationDETERMINATION OF MECHANICAL PROPERTIES OF NANOSTRUCTURES WITH COMPLEX CRYSTAL LATTICE USING MOMENT INTERACTION AT MICROSCALE
Determintion RevAdvMterSci of mechnicl 0(009) -7 properties of nnostructures with complex crystl lttice using DETERMINATION OF MECHANICAL PROPERTIES OF NANOSTRUCTURES WITH COMPLEX CRYSTAL LATTICE USING
More informationStress distribution in elastic isotropic semi-space with concentrated vertical force
Bulgrin Chemicl Communictions Volume Specil Issue pp. 4 9 Stress distribution in elstic isotropic semi-spce with concentrted verticl force L. B. Petrov Deprtment of Mechnics Todor Kbleshkov Universit of
More informationSECTION A STUDENT MATERIAL. Part 1. What and Why.?
SECTION A STUDENT MATERIAL Prt Wht nd Wh.? Student Mteril Prt Prolem n > 0 n > 0 Is the onverse true? Prolem If n is even then n is even. If n is even then n is even. Wht nd Wh? Eploring Pure Mths Are
More informationCHAPTER 10 PARAMETRIC, VECTOR, AND POLAR FUNCTIONS. dy dx
CHAPTER 0 PARAMETRIC, VECTOR, AND POLAR FUNCTIONS 0.. PARAMETRIC FUNCTIONS A) Recll tht for prmetric equtions,. B) If the equtions x f(t), nd y g(t) define y s twice-differentile function of x, then t
More informationSTRAND J: TRANSFORMATIONS, VECTORS and MATRICES
Mthemtics SKE: STRN J STRN J: TRNSFORMTIONS, VETORS nd MTRIES J3 Vectors Text ontents Section J3.1 Vectors nd Sclrs * J3. Vectors nd Geometry Mthemtics SKE: STRN J J3 Vectors J3.1 Vectors nd Sclrs Vectors
More informationENERGY-BASED METHOD FOR GAS TURBINE ENGINE DISK BURST SPEED CALCULATION
28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES ENERGY-BASED METHOD FOR GAS TURBINE ENGINE DISK BURST SPEED CALCULATION Anton N. Servetnik Centrl Institute of Avition Motors, Moscow, Russi servetnik@cim.ru
More information