FIXED BEAMS CONTINUOUS BEAMS

Size: px
Start display at page:

Download "FIXED BEAMS CONTINUOUS BEAMS"

Transcription

1 FIXED BEAMS CONTINUOUS BEAMS

2 INTRODUCTION A beam carried over more than two supports is known as a continuous beam. Railway bridges are common examples of continuous beams. But the beams in railway bridges are subjected to travelling loads in addition to static loads. We will only consider the effect of static, concentrated, and distributed loads for the analysis of reactions and support moments. Figure 1 shows a beam ABCD, carried over three spans of lengths L 1, L 2, and L 3, respectively. End A of the beam is fixed, while end D is simply supported. At the end D support moment will be zero, but at end A, supports B and C there will be support moments in the beam, to be determined. Figure 1 Continuous beam

3 Prof. Clapeyron has provided a theorem showing the relationship between three support moments of any two consecutive spans of a continuous beam and the loads applied on these two spans. This theorem is generally known as the Clapeyron s theorem of three moments. Engineers are generally responsible with the job of analyzing support moments, support reactions, and bending moments in a continuous beam for the optimum design of beam sections.

4 CLAPEYRON S THEOREM OF THREE MOMENTS This theorem provides a relationship between three moments of two consecutive spans of a continuous beam with the loading arrangement on these spans. Let us consider a continuous beam A ABCC supported over five supports, and there are four spans of the beam with lengths L 1 L 1, L 2, and L 2, respectively, as shown in Figure 2. In this beam let s consider consecutive spans AB and BC carrying a uniformly distributed loading (udl) of intensities w 1 and w 2, respectively, as shown in Figure 2. Figure 2 Continuous beam

5 CLAPEYRON S THEOREM OF THREE MOMENTS Let s say that support moments at A, B, and C are M A, M B, M C, respectively. If the bending moment on spans AB and BC is positive, then support moments will be negative. Now let s take two spans AB and BC independently and draw the bending moment (BM) diagram of each considering simple supports at ends. Maximum bending moment of AB will occur at its centre and be equal to: (Fixed beams, distributed loading, SS case, page 24) 2 w 1 L 1 8 Figure 2 Continuous beam

6 Similarly, maximum bending moment at the centre of span BC will be as shown in Figure 3. 2 w 2 L 2 8 Figure 3 BM diagrams over two supports

7 Span AB (Independently) Origin at B, x positive towards left, bending moment at any section X-X is Support moments M A, M B, M C are shown in the diagram. Bending moment at this section due to support moments (using the top triangle) w x x w L x x L w M x x M B M M A x L x 1 A A B B A x A B A x A B A x M L x M M L x M M M M M L x L M M L M M x L M M B A B x M M L x M M 1

8 Resultant bending moment at the section (when AB is a part of a continuous beam) or M x M x 2 d y EI 2 dx w1 L1 x M x 2 w1 L1 x 2 w1 x 2 2 w1 x 2 2 M B M x L 1 B x L M A 1 M M A B M B Integrating this equation, we get where C 1 is a constant of integration. At support B, where x = 0, slope (say) so, EIi B = C 1 or constant of integration, C 1 = +EIi B

9 Now Integrating this, we get where C 2 is another constant of integration. At support B, x = 0, deflection y = 0, so, 0 = C 2 Constant C 2 = 0

10 Finally At the support A, x = L 1, deflection y = 0, so, or

11 Similarly considering span BC, origin at B, x positive towards right and proceeding in the same manner as before, we can write the equation The slope i B = i B because in portion AB, x is taken positive towards left and in portion BC, x is taken positive towards right. Adding and we get

12 But i B = i B 2M B (L 1 + L 2 ) + M A L 1 + M C L 2 This is a well-known Clapeyron s theorem of three moments (for support moments having three consecutive supports for a continuous beam carrying uniformly distributed loads). If there are n supports for a continuous beam and if the two ends are simply supported, there will be (n 2) intermediate supports and (n 2) equations will be formed so as to determine the support moments at intermediate supports.

13 Example A continuous beam ABCD is carried over three equal spans of length L each. It carries a udl of intensity w through its length as shown in the figure. Determine the (i) support moments, (ii) support reactions, (iii) deflection at centre of span BC, if EI is the flexural rigidity of the beam. Draw the BM diagram of the continuous beam. The beam is simply supported at ends A and D, so bending moments M A = M D = 0

14 Moreover, the beam is symmetrically loaded about its centre; therefore, M B = M C and reactions R A = R D and R B = R C. Using Clapeyron s theorem of three moments for spans AB and BC M A L + 2M B (L + L) + M C L (from page 11) But M A = 0, M B = M C, so, Taking moments at support B of the beam, only on left side of B or

15 Reaction, Reaction, R A = 0.4wL = Reaction, R D Total load on beam = 3wL = R A + R B + R C + R D But R B = R C, due to symmetry, therefore, 2R A + 2 R B = 3wL or 2 0.4wL + 2R B = 3wL Reaction, R B = 1.1wL = Reaction, R C Bending moment at centre of each span

16 The figure above shows the BM diagram for the continuous beam with four points of contraflexure P 1, P 2, P 3, and P 4, respectively. Bending moment at centre of span AB and CD = 0.125wL wL 2 = wL 2

17 Deflection at the Centre of Span BC Considering span BC only, with known values of moments M B = M C = 0.1 wl 2 Reaction R B = R C = 1.1 wl If we take a section XX at a distance of x from B, the bending moment Integrating this equation, we get where C 1 is constant of integration.

18 At the centre of middle span, slope is zero due to symmetric loading, so Constant, Now, Integrating this equation we get where C 2 is another constant of integration. At x = 0, y = 0, therefore, EI 0 = C 2 Constant C 2 = 0

19 Finally, Deflection at centre, We should note that in this problem we have taken uniform section throughout. The section of the beam can change from span to span or within the span, depending upon the requirement.

20 Exercise 5.1 A continuous beam ABC is carried over two spans AB and BC, in which AB = 6 m and BC = 4 m. Span AB carries a udl of 4 kn/m and span BC carries a udl of 6 kn/m, as shown in the figure. Calculate the support reactions and support moments.

21 THEOREM OF THREE MOMENTS ANY TYPE OF LOADING So far we have considered only uniformly distributed loading over the spans of a continuous beam. But a beam can be subjected to any type of loading and the Clapeyron s theorem can be modified for any type of loading on a continuous beam. Let us consider two spans AB and BC of spans lengths L 1 and L 2, respectively, of a continuous beam. Spans carry the combination of loads as shown in Figure 4. Figure 4 Loads on a continuous beam

22 THEOREM OF THREE MOMENTS ANY TYPE OF LOADING Considering the beam of spans AB and BC, independently as simply supported, the bending moment diagrams of two spans can be drawn. Then support moment diagrams will be as shown by AA B C C. Consider span AB, origin at A, x positive towards right, section X-X, bending moment at the section will be M = M x + M x M= BM considering span as simply supported + BM due to support moments or Figure 4 Loads on a continuous beam

23 Multiplying both the sides by x dx and integrating or where a 1 = Area of BM diagram of span AB, considering this as simply supported, a 1 = Area of BM diagram of span AB due to support moments, = Distance of centroid of a 1 from end A, and = Distance of centroid of area a 1 (due to support moments from A).

24 Moreover, from A (from the figure, lined area)) From, we can write a BM diagram support moments Similarly considering the span CB, taking origin at C and x positive towards left, another equation can be written: But slope at i B = i B because in portion AB we have taken x positive towards right and in portion CB we have taken x positive towards left. Adding these last two equations:

25 or Area a 1 and a 2 are positive as per convention and support moments M A, M B, M C are negative. Figure 4 Support moments diagram

26 Example A continuous beam ABCD, 12 m long supported over spans AB = BC = CD = 4 m each, carries a udl of 20 kn/m run over span AB, a concentrated load of 40 kn at a distance of 1 m from point B on span BC, and a load of 30 kn at the centre of the span CD. Determine support moments and draw the BM diagram for the continuous beam. The figure shows a continuous beam ABCD, with equal spans. AB carries a udl of 20 kn/m. Span BC carries a concentrated load of 40 kn at E, 1 m from B. Span CD carries a point load of 30 kn at F, at centre of CD. Let us construct a diagrams (BM diagrams considering each span independently as S.S.) Span AB Maximum BM

27 For parabola AG B, area Span BC Maximum BM Triangle BE C, area (about B) (about C)

28 Span CD, Maximum BM Using the equation of three moments for spans AB and CB 4M A + 16M B + 4M C = = 530 or M A + 4M B + MC = (i) But M A = 0 So, 4M B + M C = (ii)

29 Using the equation of three moments for spans BC and DC But M D = 0 4M B + 16M C = = 330 4M B + 16M C = 330 (iii) From Equations (ii) and (iii) 15M C = M C = knm M B = knm Taking BB = knm CC = knm

30 Drawing lines AB, B C, C D, the diagram AB C DA, is the BM diagram due to support moments. There are four points of contraflexure in the BM diagram for continuous beam when a diagrams are superimposed over a diagram, the BM diagram due to support moments. Positive and negative areas of the BM diagram are also marked.

31 SUPPORTS NOT AT SAME LEVEL There are two spans AB and BC of lengths L 1 and L 2 of a continuous beam. Supports A, B, and C are not at same one level. Support B is below support A by δ 1 and below support C by δ 2 as shown in Figure 5 (a). These level differences are very small in comparison to span length, say of the order of 0.1% of span length. For spans AB and BC, bending moment diagrams are plotted considering the spans independently as shown by the shaded diagrams. Say Figure 5 Continuous beam

32 M B M A M B L 1 M C L 2

33 Span AB: Consider a section X-X, at a distance of x from A or or

34 Similarly consider span CB, origin at C, x positive towards left It may be noted that i B = i B slope, because for span AB, we have taken x positive towards right but for span CB, we have taken x positive towards left. So, i B + i B = 0 Adding and or M A L 1 + 2M B (L 1 + L 2 ) + M C L 2 From this equation M A, M B, and M C can be determined, after determining and.

35 Example A continuous beam ABC, 10 m long, spans AB = 6 m, span BC = 4 m, carries a udl of 2 kn/m over AB and a concentrated load of 6 kn at centre of BC. Support B is below the level of A by 10 mm and below the level of C by 5 mm. Determine support moments and support reactions, if EI = 6,000 knm 2. Figure (a) shows the loads on the beam. Let us draw BM diagrams considering the spans as independently supported.

36 Span AB area Span CB area

37 Support moments M A = M C = 0 Using the equation derived in Fixed Beams, Support Moments: Total load on beam = = 18kN Moreover M B = R A = 6R A 36 Reaction, R A = kn also M B = 4R C = 4R C 12 Reaction, R C = kn Reaction, R B = = kn.

38 CONTINUOUS BEAM WITH FIXED END For a continuous beam with a fixed end, the equations for support moments can be derived considering the slope and deflection at fixed end to be zero. Figure 6 (a) shows two consecutive spans AB and BC of a continuous beam. End A of the beam is fixed. Bending moment diagrams a 1 and a 2 are plotted considering spans AB and BC supported independently as shown in Figure 6. At any section if: M x = BM due load on span, considering span independently M x = BM due to support moments, then Figure 6 Support moments

39 Considering origin as B and x positive towards left: But at fixed end: or where M A is the fixing couple at fixed end A. This relationship can also be obtained by considering an imaginary span A A of zero length and bending moment at A, M A = 0 using Clapeyron s theorem for two spans A A and AB.

40 or If the other end of the continuous beam is also fixed, a similar equation can be made by considering an imaginary span to the right of the other fixed end, and then applying the theorem of three moments.

41 Example A continuous beam ABCD 14 m long rests on supports A, B, C, and D all at the same level. AB = 6 m, BC = 4 m, CD = 4 m. Support A is a fixed support. It carries two concentrated loads of 60 kn each, at a distance of 2 m from end A and end D as shown in the figure. There is a udl of 15 kn/m over span BC. Find the moments and reactions at the supports. The figure shows the continuous beam ABCD, with fixed end at A. Let us first draw BM diagrams considering each span to be simply supported.

42 Span AB Maximum BM, Origin at A, Origin at B,

43 Span BC Span CD

44 Considering imaginary span AA of zero length and using Clapeyron s theorem for two spans A A and AB, or

45 Spans AB and BC Spans BC and CD But 4M B + 16M C = 600 (iv)

46 Putting the value of M A in equation (iii) M B + 4M C = 150 From eq. (iv) (vi) Solving eqs. (v) and (vi), we get 16 M B = 330 Moment, M B = knm, Putting the value of M B in eq. (vi) 4 M C = Moments,

47 The figure shows shaded diagrams are a 1, a 2, and a 3 BM diagrams. Bending moment diagram due to support moments is superimposed on these diagrams to get resultant BM at any section.

48 Support Reactions M C = 4R D 60 2 = Reaction, R D = 21.9 kn M B = 8R D + 4R C = R D + 4R C = R C = Reaction, R C = 71.0 kn Moments about A 14R D + 10R C + 6R B = M A = knm

49 Putting the values in the solution: Reaction, R B = 41.1 kn Total load on beam = = 180 kn Reaction R A = = 46 kn

50 Example A continuous beam ABC, fixed at end A, supported over spans AB = BC = 6 m each. There is a udl of 10 kn/m over AB and a concentrated load of 40 kn at centre of BC as shown in the figure. While the supports A and C remain at the same level, the level of support B is 1 mm below due to sinking. Moment of inertia of beam from A to B is 18,000 cm 4 and from BC it is 12,000 cm 4. If E = 210 kn/mm 2, determine support moments and draw BM diagram. Let us first draw a diagram for both spans area,

51 a 2 is a triangle with Moment, M C = 0, because end C is a simple support.

52 Span AA B Imaginary span AA and AB equation of three moments. Taking I 1 common throughout (because level of A is higher than level of B by 1 mm) 12MA + 6MB = (i) Now using the theorem of three moments for spans AB and BC, and noting that I 1 is different than I 2, equation can be modified as

53 Multiplying throughout by I 1, But I 1 = 1.5I2, putting this value, we get 6M A + 30M B + 9M C = M A + 30M B + 9M C = knm But M C = 0

54 So, 6M A + 30M B = knm (ii) 6M A + 3M B = knm From eq (i) (iii) From these two equations Support moments, Superimposing diagram over this, we get resultant bending moment diagram. Shaded parts show positive BM. There are three points of contraflexure as shown.

FIXED BEAMS IN BENDING

FIXED BEAMS IN BENDING FIXED BEAMS IN BENDING INTRODUCTION Fixed or built-in beams are commonly used in building construction because they possess high rigidity in comparison to simply supported beams. When a simply supported

More information

techie-touch.blogspot.com DEPARTMENT OF CIVIL ENGINEERING ANNA UNIVERSITY QUESTION BANK CE 2302 STRUCTURAL ANALYSIS-I TWO MARK QUESTIONS UNIT I DEFLECTION OF DETERMINATE STRUCTURES 1. Write any two important

More information

UNIT III DEFLECTION OF BEAMS 1. What are the methods for finding out the slope and deflection at a section? The important methods used for finding out the slope and deflection at a section in a loaded

More information

UNIT II SLOPE DEFLECION AND MOMENT DISTRIBUTION METHOD

UNIT II SLOPE DEFLECION AND MOMENT DISTRIBUTION METHOD SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road 517583 QUESTION BANK (DESCRIPTIVE) Subject with Code : SA-II (13A01505) Year & Sem: III-B.Tech & I-Sem Course & Branch: B.Tech

More information

Shear force and bending moment of beams 2.1 Beams 2.2 Classification of beams 1. Cantilever Beam Built-in encastre' Cantilever

Shear force and bending moment of beams 2.1 Beams 2.2 Classification of beams 1. Cantilever Beam Built-in encastre' Cantilever CHAPTER TWO Shear force and bending moment of beams 2.1 Beams A beam is a structural member resting on supports to carry vertical loads. Beams are generally placed horizontally; the amount and extent of

More information

MAHALAKSHMI ENGINEERING COLLEGE

MAHALAKSHMI ENGINEERING COLLEGE AHAAKSHI ENGINEERING COEGE TIRUCHIRAPAI - 611. QUESTION WITH ANSWERS DEPARTENT : CIVI SEESTER: V SU.CODE/ NAE: CE 5 / Strength of aterials UNIT INDETERINATE EAS 1. Define statically indeterminate beams.

More information

Procedure for drawing shear force and bending moment diagram:

Procedure for drawing shear force and bending moment diagram: Procedure for drawing shear force and bending moment diagram: Preamble: The advantage of plotting a variation of shear force F and bending moment M in a beam as a function of x' measured from one end of

More information

UNIT-V MOMENT DISTRIBUTION METHOD

UNIT-V MOMENT DISTRIBUTION METHOD UNIT-V MOMENT DISTRIBUTION METHOD Distribution and carryover of moments Stiffness and carry over factors Analysis of continuous beams Plane rigid frames with and without sway Neylor s simplification. Hardy

More information

Problem 1: Calculating deflection by integration uniform load. Problem 2: Calculating deflection by integration - triangular load pattern

Problem 1: Calculating deflection by integration uniform load. Problem 2: Calculating deflection by integration - triangular load pattern Problem 1: Calculating deflection by integration uniform load Problem 2: Calculating deflection by integration - triangular load pattern Problem 3: Deflections - by differential equations, concentrated

More information

Continuous Beams - Flexibility Method

Continuous Beams - Flexibility Method ontinuous eams - Flexibility Method Qu. Sketch the M diagram for the beam shown in Fig.. Take E = 200kN/mm 2. 50kN 60kN-m = = 0kN/m D I = 60 50 40 x 0 6 mm 4 Fig. 60.0 23.5 D 25.7 6.9 M diagram in kn-m

More information

QUESTION BANK. SEMESTER: V SUBJECT CODE / Name: CE 6501 / STRUCTURAL ANALYSIS-I

QUESTION BANK. SEMESTER: V SUBJECT CODE / Name: CE 6501 / STRUCTURAL ANALYSIS-I QUESTION BANK DEPARTMENT: CIVIL SEMESTER: V SUBJECT CODE / Name: CE 6501 / STRUCTURAL ANALYSIS-I Unit 5 MOMENT DISTRIBUTION METHOD PART A (2 marks) 1. Differentiate between distribution factors and carry

More information

BUILT-IN BEAMS. The maximum bending moments and maximum deflections for built-in beams with standard loading cases are as follows: Summary CHAPTER 6

BUILT-IN BEAMS. The maximum bending moments and maximum deflections for built-in beams with standard loading cases are as follows: Summary CHAPTER 6 ~ or CHAPTER 6 BUILT-IN BEAMS Summary The maximum bending moments and maximum deflections for built-in beams with standard loading cases are as follows: MAXIMUM B.M. AND DEFLECTION FOR BUILT-IN BEAMS Loading

More information

Chapter Objectives. Copyright 2011 Pearson Education South Asia Pte Ltd

Chapter Objectives. Copyright 2011 Pearson Education South Asia Pte Ltd Chapter Objectives To generalize the procedure by formulating equations that can be plotted so that they describe the internal shear and moment throughout a member. To use the relations between distributed

More information

THE AREA-MOMENT / MOMENT-AREA METHODS:

THE AREA-MOMENT / MOMENT-AREA METHODS: THE AREA-MOMENT / MOMENT-AREA METHODS: The area moment method is a semi graphical method of dealing with problems of deflection of beams subjected to bending. The method is based on a geometrical interpretation

More information

MAHALAKSHMI ENGINEERING COLLEGE

MAHALAKSHMI ENGINEERING COLLEGE CE840-STRENGTH OF TERIS - II PGE 1 HKSHI ENGINEERING COEGE TIRUCHIRPI - 611. QUESTION WITH NSWERS DEPRTENT : CIVI SEESTER: IV SU.CODE/ NE: CE 840 / Strength of aterials -II UNIT INDETERINTE ES 1. Define

More information

2. Determine the deflection at C of the beam given in fig below. Use principal of virtual work. W L/2 B A L C

2. Determine the deflection at C of the beam given in fig below. Use principal of virtual work. W L/2 B A L C CE-1259, Strength of Materials UNIT I STRESS, STRAIN DEFORMATION OF SOLIDS Part -A 1. Define strain energy density. 2. State Maxwell s reciprocal theorem. 3. Define proof resilience. 4. State Castigliano

More information

2 marks Questions and Answers

2 marks Questions and Answers 1. Define the term strain energy. A: Strain Energy of the elastic body is defined as the internal work done by the external load in deforming or straining the body. 2. Define the terms: Resilience and

More information

UNIT I ENERGY PRINCIPLES

UNIT I ENERGY PRINCIPLES UNIT I ENERGY PRINCIPLES Strain energy and strain energy density- strain energy in traction, shear in flexure and torsion- Castigliano s theorem Principle of virtual work application of energy theorems

More information

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method Module 2 Analysis of Statically Indeterminate Structures by the Matrix Force Method Lesson 8 The Force Method of Analysis: Beams Instructional Objectives After reading this chapter the student will be

More information

BEAM A horizontal or inclined structural member that is designed to resist forces acting to its axis is called a beam

BEAM A horizontal or inclined structural member that is designed to resist forces acting to its axis is called a beam BEM horizontal or inclined structural member that is designed to resist forces acting to its axis is called a beam INTERNL FORCES IN BEM Whether or not a beam will break, depend on the internal resistances

More information

Unit II Shear and Bending in Beams

Unit II Shear and Bending in Beams Unit II Shear and Bending in Beams Syllabus: Beams and Bending- Types of loads, supports - Shear Force and Bending Moment Diagrams for statically determinate beam with concentrated load, UDL, uniformly

More information

UNIT IV FLEXIBILTY AND STIFFNESS METHOD

UNIT IV FLEXIBILTY AND STIFFNESS METHOD SIDDHARTH GROUP OF INSTITUTIONS :: PUTTUR Siddharth Nagar, Narayanavanam Road 517583 QUESTION BANK (DESCRIPTIVE) Subject with Code : SA-II (13A01505) Year & Sem: III-B.Tech & I-Sem Course & Branch: B.Tech

More information

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A DEPARTMENT: CIVIL SUBJECT CODE: CE2201 QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State

More information

MODULE 3 ANALYSIS OF STATICALLY INDETERMINATE STRUCTURES BY THE DISPLACEMENT METHOD

MODULE 3 ANALYSIS OF STATICALLY INDETERMINATE STRUCTURES BY THE DISPLACEMENT METHOD ODULE 3 ANALYI O TATICALLY INDETERINATE TRUCTURE BY THE DIPLACEENT ETHOD LEON 19 THE OENT- DITRIBUTION ETHOD: TATICALLY INDETERINATE BEA WITH UPPORT ETTLEENT Instructional Objectives After reading this

More information

Chapter 8 Supplement: Deflection in Beams Double Integration Method

Chapter 8 Supplement: Deflection in Beams Double Integration Method Chapter 8 Supplement: Deflection in Beams Double Integration Method 8.5 Beam Deflection Double Integration Method In this supplement, we describe the methods for determining the equation of the deflection

More information

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A (2 Marks) 1. Define longitudinal strain and lateral strain. 2. State Hooke s law. 3. Define modular ratio,

More information

Mechanics of Structure

Mechanics of Structure S.Y. Diploma : Sem. III [CE/CS/CR/CV] Mechanics of Structure Time: Hrs.] Prelim Question Paper Solution [Marks : 70 Q.1(a) Attempt any SIX of the following. [1] Q.1(a) Define moment of Inertia. State MI

More information

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC.

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC. BENDING STRESS The effect of a bending moment applied to a cross-section of a beam is to induce a state of stress across that section. These stresses are known as bending stresses and they act normally

More information

Structural Steel Design Project

Structural Steel Design Project Job No: Sheet 1 of 6 Rev Worked Example - 1 Made by Date 4-1-000 Checked by PU Date 30-4-000 Analyse the building frame shown in Fig. A using portal method. 15 kn C F I L 4 m 0 kn B E H K 6 m A D G J 4

More information

Chapter 11. Displacement Method of Analysis Slope Deflection Method

Chapter 11. Displacement Method of Analysis Slope Deflection Method Chapter 11 Displacement ethod of Analysis Slope Deflection ethod Displacement ethod of Analysis Two main methods of analyzing indeterminate structure Force method The method of consistent deformations

More information

STATICALLY INDETERMINATE STRUCTURES

STATICALLY INDETERMINATE STRUCTURES STATICALLY INDETERMINATE STRUCTURES INTRODUCTION Generally the trusses are supported on (i) a hinged support and (ii) a roller support. The reaction components of a hinged support are two (in horizontal

More information

FRAME ANALYSIS. Dr. Izni Syahrizal bin Ibrahim. Faculty of Civil Engineering Universiti Teknologi Malaysia

FRAME ANALYSIS. Dr. Izni Syahrizal bin Ibrahim. Faculty of Civil Engineering Universiti Teknologi Malaysia FRAME ANALYSIS Dr. Izni Syahrizal bin Ibrahim Faculty of Civil Engineering Universiti Teknologi Malaysia Email: iznisyahrizal@utm.my Introduction 3D Frame: Beam, Column & Slab 2D Frame Analysis Building

More information

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method odule 3 Analysis of Statically Indeterminate Structures by the Displacement ethod Lesson 21 The oment- Distribution ethod: rames with Sidesway Instructional Objectives After reading this chapter the student

More information

FLOW CHART FOR DESIGN OF BEAMS

FLOW CHART FOR DESIGN OF BEAMS FLOW CHART FOR DESIGN OF BEAMS Write Known Data Estimate self-weight of the member. a. The self-weight may be taken as 10 percent of the applied dead UDL or dead point load distributed over all the length.

More information

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method odule 3 Analysis of Statically Indeterminate Structures by the Displacement ethod Lesson 16 The Slope-Deflection ethod: rames Without Sidesway Instructional Objectives After reading this chapter the student

More information

Beams. Beams are structural members that offer resistance to bending due to applied load

Beams. Beams are structural members that offer resistance to bending due to applied load Beams Beams are structural members that offer resistance to bending due to applied load 1 Beams Long prismatic members Non-prismatic sections also possible Each cross-section dimension Length of member

More information

SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS

SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS Time Allowed:2 Hours Maximum Marks: 300 Attention: 1. Paper consists of Part A (Civil & Structural) Part B (Electrical) and Part C (Mechanical)

More information

ENR202 Mechanics of Materials Lecture 4A Notes and Slides

ENR202 Mechanics of Materials Lecture 4A Notes and Slides Slide 1 Copyright Notice Do not remove this notice. COMMMONWEALTH OF AUSTRALIA Copyright Regulations 1969 WARNING This material has been produced and communicated to you by or on behalf of the University

More information

DEPARTMENT OF CIVIL ENGINEERING

DEPARTMENT OF CIVIL ENGINEERING KINGS COLLEGE OF ENGINEERING DEPARTMENT OF CIVIL ENGINEERING SUBJECT: CE 2252 STRENGTH OF MATERIALS UNIT: I ENERGY METHODS 1. Define: Strain Energy When an elastic body is under the action of external

More information

BEAM DEFLECTION THE ELASTIC CURVE

BEAM DEFLECTION THE ELASTIC CURVE BEAM DEFLECTION Samantha Ramirez THE ELASTIC CURVE The deflection diagram of the longitudinal axis that passes through the centroid of each cross-sectional area of a beam. Supports that apply a moment

More information

By Dr. Mohammed Ramidh

By Dr. Mohammed Ramidh Engineering Materials Design Lecture.6 the design of beams By Dr. Mohammed Ramidh 6.1 INTRODUCTION Finding the shear forces and bending moments is an essential step in the design of any beam. we usually

More information

3.4 Analysis for lateral loads

3.4 Analysis for lateral loads 3.4 Analysis for lateral loads 3.4.1 Braced frames In this section, simple hand methods for the analysis of statically determinate or certain low-redundant braced structures is reviewed. Member Force Analysis

More information

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method Module 2 Analysis of Statically Indeterminate Structures by the Matrix Force Method Lesson 11 The Force Method of Analysis: Frames Instructional Objectives After reading this chapter the student will be

More information

Bending Stress. Sign convention. Centroid of an area

Bending Stress. Sign convention. Centroid of an area Bending Stress Sign convention The positive shear force and bending moments are as shown in the figure. Centroid of an area Figure 40: Sign convention followed. If the area can be divided into n parts

More information

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method odule 3 Analysis of Statically Indeterminate Structures by the Displacement ethod Lesson 14 The Slope-Deflection ethod: An Introduction Introduction As pointed out earlier, there are two distinct methods

More information

Chapter 2 Basis for Indeterminate Structures

Chapter 2 Basis for Indeterminate Structures Chapter - Basis for the Analysis of Indeterminate Structures.1 Introduction... 3.1.1 Background... 3.1. Basis of Structural Analysis... 4. Small Displacements... 6..1 Introduction... 6.. Derivation...

More information

= 50 ksi. The maximum beam deflection Δ max is not = R B. = 30 kips. Notes for Strength of Materials, ET 200

= 50 ksi. The maximum beam deflection Δ max is not = R B. = 30 kips. Notes for Strength of Materials, ET 200 Notes for Strength of Materials, ET 00 Steel Six Easy Steps Steel beam design is about selecting the lightest steel beam that will support the load without exceeding the bending strength or shear strength

More information

Mechanics of Solids notes

Mechanics of Solids notes Mechanics of Solids notes 1 UNIT II Pure Bending Loading restrictions: As we are aware of the fact internal reactions developed on any cross-section of a beam may consists of a resultant normal force,

More information

Level 7 Postgraduate Diploma in Engineering Computational mechanics using finite element method

Level 7 Postgraduate Diploma in Engineering Computational mechanics using finite element method 9210-203 Level 7 Postgraduate Diploma in Engineering Computational mechanics using finite element method You should have the following for this examination one answer book No additional data is attached

More information

Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering

Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering 008/9 Dr. Colin Caprani 1 Contents 1. Introduction... 3 1.1 General... 3 1. Background... 4 1.3 Discontinuity Functions...

More information

6. Bending CHAPTER OBJECTIVES

6. Bending CHAPTER OBJECTIVES CHAPTER OBJECTIVES Determine stress in members caused by bending Discuss how to establish shear and moment diagrams for a beam or shaft Determine largest shear and moment in a member, and specify where

More information

Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering

Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering Deflection of Flexural Members - Macaulay s Method 3rd Year Structural Engineering 009/10 Dr. Colin Caprani 1 Contents 1. Introduction... 4 1.1 General... 4 1. Background... 5 1.3 Discontinuity Functions...

More information

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM - 613 403 - THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Sub : Strength of Materials Year / Sem: II / III Sub Code : MEB 310

More information

Sub. Code:

Sub. Code: Important Instructions to examiners: ) The answers should be examined by key words and not as word-to-word as given in the model answer scheme. ) The model answer and the answer written by candidate may

More information

STRUCTURAL ANALYSIS CHAPTER 2. Introduction

STRUCTURAL ANALYSIS CHAPTER 2. Introduction CHAPTER 2 STRUCTURAL ANALYSIS Introduction The primary purpose of structural analysis is to establish the distribution of internal forces and moments over the whole part of a structure and to identify

More information

bending moment in the beam can be obtained by integration

bending moment in the beam can be obtained by integration q 0 L 4 B = - v(l) = CCC ( ) 30 EI Example 9-5 an overhanging beam ABC with a concentrated load P applied at the end determine the equation of deflection curve and the deflection C at the end flexural

More information

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV UNIT I STRESS, STRAIN DEFORMATION OF SOLIDS PART A (2 MARKS)

More information

Moment Distribution Method

Moment Distribution Method Moment Distribution Method Lesson Objectives: 1) Identify the formulation and sign conventions associated with the Moment Distribution Method. 2) Derive the Moment Distribution Method equations using mechanics

More information

structural analysis Excessive beam deflection can be seen as a mode of failure.

structural analysis Excessive beam deflection can be seen as a mode of failure. Structure Analysis I Chapter 8 Deflections Introduction Calculation of deflections is an important part of structural analysis Excessive beam deflection can be seen as a mode of failure. Extensive glass

More information

Theory of Structures

Theory of Structures SAMPLE STUDY MATERIAL Postal Correspondence Course GATE, IES & PSUs Civil Engineering Theory of Structures C O N T E N T 1. ARCES... 3-14. ROLLING LOADS AND INFLUENCE LINES. 15-9 3. DETERMINACY AND INDETERMINACY..

More information

UNIVERSITY OF BOLTON SCHOOL OF ENGINEERING. BEng (HONS) CIVIL ENGINEERING SEMESTER 1 EXAMINATION 2016/2017 MATHEMATICS & STRUCTURAL ANALYSIS

UNIVERSITY OF BOLTON SCHOOL OF ENGINEERING. BEng (HONS) CIVIL ENGINEERING SEMESTER 1 EXAMINATION 2016/2017 MATHEMATICS & STRUCTURAL ANALYSIS TW21 UNIVERSITY OF BOLTON SCHOOL OF ENGINEERING BEng (HONS) CIVIL ENGINEERING SEMESTER 1 EXAMINATION 2016/2017 MATHEMATICS & STRUCTURAL ANALYSIS MODULE NO: CIE4011 Date: Wednesday 11 th January 2017 Time:

More information

Sample Question Paper

Sample Question Paper Scheme I Sample Question Paper Program Name : Mechanical Engineering Program Group Program Code : AE/ME/PG/PT/FG Semester : Third Course Title : Strength of Materials Marks : 70 Time: 3 Hrs. Instructions:

More information

UNIT II 1. Sketch qualitatively the influence line for shear at D for the beam [M/J-15]

UNIT II 1. Sketch qualitatively the influence line for shear at D for the beam [M/J-15] UNIT II 1. Sketch qualitatively the influence line for shear at D for the beam [M/J-15] 2. Draw the influence line for shear to the left of B for the overhanging beam shown in Fig. Q. No. 4 [M/J-15] 3.

More information

8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method

8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method. 8-5 Conjugate-Beam method The basis for the method comes from the similarity of eqn.1 &. to eqn 8. & 8. To show this similarity, we can write these eqn as shown dv dx w d θ M dx d M w dx d v M dx Here the shear V compares with

More information

SRI VIDYA COLLEGE OF ENGINEERING AND TECHNOLOGY, VIRUDHUNAGAR CE 6602 STRUCTURAL ANALYSIS - II DEPARTMENT OF CIVIL ENGINEERING CE 6501 STRUCTURAL ANALYSIS - I 2 MARK QUESTION BANK UNIT II - INFLUENCE LINES

More information

dv dx Slope of the shear diagram = - Value of applied loading dm dx Slope of the moment curve = Shear Force

dv dx Slope of the shear diagram = - Value of applied loading dm dx Slope of the moment curve = Shear Force Beams SFD and BMD Shear and Moment Relationships w dv dx Slope of the shear diagram = - Value of applied loading V dm dx Slope of the moment curve = Shear Force Both equations not applicable at the point

More information

Structural Analysis III Compatibility of Displacements & Principle of Superposition

Structural Analysis III Compatibility of Displacements & Principle of Superposition Structural Analysis III Compatibility of Displacements & Principle of Superposition 2007/8 Dr. Colin Caprani, Chartered Engineer 1 1. Introduction 1.1 Background In the case of 2-dimensional structures

More information

Lecture 6: The Flexibility Method - Beams. Flexibility Method

Lecture 6: The Flexibility Method - Beams. Flexibility Method lexibility Method In 1864 James Clerk Maxwell published the first consistent treatment of the flexibility method for indeterminate structures. His method was based on considering deflections, but the presentation

More information

Semester: BE 3 rd Subject :Mechanics of Solids ( ) Year: Faculty: Mr. Rohan S. Kariya. Tutorial 1

Semester: BE 3 rd Subject :Mechanics of Solids ( ) Year: Faculty: Mr. Rohan S. Kariya. Tutorial 1 Semester: BE 3 rd Subject :Mechanics of Solids (2130003) Year: 2018-19 Faculty: Mr. Rohan S. Kariya Class: MA Tutorial 1 1 Define force and explain different type of force system with figures. 2 Explain

More information

29. Define Stiffness matrix method. 30. What is the compatibility condition used in the flexibility method?

29. Define Stiffness matrix method. 30. What is the compatibility condition used in the flexibility method? CLASS: III YEAR / VI SEMESTER CIVIL SUBJECTCODE AND NAME: CE 2351 - STRUCTURAL ANALYSIS-II UNIT1 FLEXIBILITY MATRIX METHOD. PART A 1. What is meant by indeterminate structures? 2. What are the conditions

More information

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR:

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR: MECHANICS OF STRUCTURES- ASSIGNMENT NO 1 SEMESTER: V 1) Find the least moment of Inertia about the centroidal axes X-X and Y-Y of an unequal angle section 125 mm 75 mm 10 mm as shown in figure 2) Determine

More information

Shear Force V: Positive shear tends to rotate the segment clockwise.

Shear 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 information

UNIT-II MOVING LOADS AND INFLUENCE LINES

UNIT-II MOVING LOADS AND INFLUENCE LINES UNIT-II MOVING LOADS AND INFLUENCE LINES Influence lines for reactions in statically determinate structures influence lines for member forces in pin-jointed frames Influence lines for shear force and bending

More information

Hong Kong Institute of Vocational Education (Tsing Yi) Higher Diploma in Civil Engineering Structural Mechanics. Chapter 2 SECTION PROPERTIES

Hong Kong Institute of Vocational Education (Tsing Yi) Higher Diploma in Civil Engineering Structural Mechanics. Chapter 2 SECTION PROPERTIES Section Properties Centroid The centroid of an area is the point about which the area could be balanced if it was supported from that point. The word is derived from the word center, and it can be though

More information

CH. 4 BEAMS & COLUMNS

CH. 4 BEAMS & COLUMNS CH. 4 BEAMS & COLUMNS BEAMS Beams Basic theory of bending: internal resisting moment at any point in a beam must equal the bending moments produced by the external loads on the beam Rx = Cc + Tt - If the

More information

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS Name :. Roll No. :..... Invigilator s Signature :.. 2011 SOLID MECHANICS Time Allotted : 3 Hours Full Marks : 70 The figures in the margin indicate full marks. Candidates are required to give their answers

More information

CITY AND GUILDS 9210 UNIT 135 MECHANICS OF SOLIDS Level 6 TUTORIAL 5A - MOMENT DISTRIBUTION METHOD

CITY AND GUILDS 9210 UNIT 135 MECHANICS OF SOLIDS Level 6 TUTORIAL 5A - MOMENT DISTRIBUTION METHOD Outcome 1 The learner can: CITY AND GUIDS 910 UNIT 15 ECHANICS OF SOIDS evel 6 TUTORIA 5A - OENT DISTRIBUTION ETHOD Calculate stresses, strain and deflections in a range of components under various load

More information

[8] Bending and Shear Loading of Beams

[8] Bending and Shear Loading of Beams [8] Bending and Shear Loading of Beams Page 1 of 28 [8] Bending and Shear Loading of Beams [8.1] Bending of Beams (will not be covered in class) [8.2] Bending Strain and Stress [8.3] Shear in Straight

More information

UNIT I ENERGY PRINCIPLES

UNIT I ENERGY PRINCIPLES UNIT I ENERGY PRINCIPLES Strain energy and strain energy density- strain energy in traction, shear in flexure and torsion- Castigliano s theorem Principle of virtual work application of energy theorems

More information

8 Deflectionmax. = 5WL 3 384EI

8 Deflectionmax. = 5WL 3 384EI 8 max. = 5WL 3 384EI 1 salesinfo@mechanicalsupport.co.nz PO Box 204336 Highbrook Auckland www.mechanicalsupport.co.nz 2 Engineering Data - s and Columns Structural Data 1. Properties properties have been

More information

P.E. Civil Exam Review:

P.E. Civil Exam Review: P.E. Civil Exam Review: Structural Analysis J.P. Mohsen Email: jpm@louisville.edu Structures Determinate Indeterminate STATICALLY DETERMINATE STATICALLY INDETERMINATE Stability and Determinacy of Trusses

More information

Assumptions: beam is initially straight, is elastically deformed by the loads, such that the slope and deflection of the elastic curve are

Assumptions: beam is initially straight, is elastically deformed by the loads, such that the slope and deflection of the elastic curve are *12.4 SLOPE & DISPLACEMENT BY THE MOMENT-AREA METHOD Assumptions: beam is initially straight, is elastically deformed by the loads, such that the slope and deflection of the elastic curve are very small,

More information

Internal Internal Forces Forces

Internal Internal Forces Forces Internal Forces ENGR 221 March 19, 2003 Lecture Goals Internal Force in Structures Shear Forces Bending Moment Shear and Bending moment Diagrams Internal Forces and Bending The bending moment, M. Moment

More information

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation.

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The magnitude

More information

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains STRENGTH OF MATERIALS-I Unit-1 Simple stresses and strains 1. What is the Principle of surveying 2. Define Magnetic, True & Arbitrary Meridians. 3. Mention different types of chains 4. Differentiate between

More information

Module 4. Analysis of Statically Indeterminate Structures by the Direct Stiffness Method. Version 2 CE IIT, Kharagpur

Module 4. Analysis of Statically Indeterminate Structures by the Direct Stiffness Method. Version 2 CE IIT, Kharagpur Module Analysis of Statically Indeterminate Structures by the Direct Stiffness Method Version CE IIT, Kharagur Lesson 9 The Direct Stiffness Method: Beams (Continued) Version CE IIT, Kharagur Instructional

More information

OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS. You should judge your progress by completing the self assessment exercises. CONTENTS

OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS. You should judge your progress by completing the self assessment exercises. CONTENTS Unit 2: Unit code: QCF Level: 4 Credit value: 15 Engineering Science L/601/1404 OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS 1. Be able to determine the behavioural characteristics of elements of static engineering

More information

The bending moment diagrams for each span due to applied uniformly distributed and concentrated load are shown in Fig.12.4b.

The bending moment diagrams for each span due to applied uniformly distributed and concentrated load are shown in Fig.12.4b. From inspection, it is assumed that the support moments at is zero and support moment at, 15 kn.m (negative because it causes compression at bottom at ) needs to be evaluated. pplying three- Hence, only

More information

INFLUENCE LINE. Structural Analysis. Reference: Third Edition (2005) By Aslam Kassimali

INFLUENCE LINE. Structural Analysis. Reference: Third Edition (2005) By Aslam Kassimali INFLUENCE LINE Reference: Structural Analsis Third Edition (2005) B Aslam Kassimali DEFINITION An influence line is a graph of a response function of a structure as a function of the position of a downward

More information

CHENDU COLLEGE OF ENGINEERING &TECHNOLOGY DEPARTMENT OF CIVIL ENGINEERING SUB CODE & SUB NAME : CE2351-STRUCTURAL ANALYSIS-II UNIT-1 FLEXIBILITY

CHENDU COLLEGE OF ENGINEERING &TECHNOLOGY DEPARTMENT OF CIVIL ENGINEERING SUB CODE & SUB NAME : CE2351-STRUCTURAL ANALYSIS-II UNIT-1 FLEXIBILITY CHENDU COLLEGE OF ENGINEERING &TECHNOLOGY DEPARTMENT OF CIVIL ENGINEERING SUB CODE & SUB NAME : CE2351-STRUCTURAL ANALYSIS-II UNIT-1 FLEXIBILITY METHOD FOR INDETERMINATE FRAMES PART-A(2MARKS) 1. What is

More information

ENG202 Statics Lecture 16, Section 7.1

ENG202 Statics Lecture 16, Section 7.1 ENG202 Statics Lecture 16, Section 7.1 Internal Forces Developed in Structural Members - Design of any structural member requires an investigation of the loading acting within the member in order to be

More information

CHAPTER 7 DEFLECTIONS OF BEAMS

CHAPTER 7 DEFLECTIONS OF BEAMS CHPTER 7 DEFLECTIONS OF EMS OJECTIVES Determine the deflection and slope at specific points on beams and shafts, using various analytical methods including: o o o The integration method The use of discontinuity

More information

SN QUESTION YEAR MARK 1. State and prove the relationship between shearing stress and rate of change of bending moment at a section in a loaded beam.

SN QUESTION YEAR MARK 1. State and prove the relationship between shearing stress and rate of change of bending moment at a section in a loaded beam. ALPHA COLLEGE OF ENGINEERING AND TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING MECHANICS OF SOLIDS (21000) ASSIGNMENT 1 SIMPLE STRESSES AND STRAINS SN QUESTION YEAR MARK 1 State and prove the relationship

More information

Unit Workbook 1 Level 4 ENG U8 Mechanical Principles 2018 UniCourse Ltd. All Rights Reserved. Sample

Unit Workbook 1 Level 4 ENG U8 Mechanical Principles 2018 UniCourse Ltd. All Rights Reserved. Sample Pearson BTEC Levels 4 Higher Nationals in Engineering (RQF) Unit 8: Mechanical Principles Unit Workbook 1 in a series of 4 for this unit Learning Outcome 1 Static Mechanical Systems Page 1 of 23 1.1 Shafts

More information

BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS)

BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS) BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS) All questions carry equal marks(10 marks) Q.1 (a) Write the SI units of following quantities and also mention whether it is scalar or vector: (i)

More information

STRUCTURAL ANALYSIS BFC Statically Indeterminate Beam & Frame

STRUCTURAL ANALYSIS BFC Statically Indeterminate Beam & Frame STRUCTURA ANAYSIS BFC 21403 Statically Indeterminate Beam & Frame Introduction Analysis for indeterminate structure of beam and frame: 1. Slope-deflection method 2. Moment distribution method Displacement

More information

UNIT-I STRESS, STRAIN. 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2

UNIT-I STRESS, STRAIN. 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2 UNIT-I STRESS, STRAIN 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2 Young s modulus E= 2 x10 5 N/mm 2 Area1=900mm 2 Area2=400mm 2 Area3=625mm

More information

ME 201 Engineering Mechanics: Statics

ME 201 Engineering Mechanics: Statics ME 0 Engineering Mechanics: Statics Unit 9. Moments of nertia Definition of Moments of nertia for Areas Parallel-Axis Theorem for an Area Radius of Gyration of an Area Moments of nertia for Composite Areas

More information

276 Calculus and Structures

276 Calculus and Structures 76 Calculus and Structures CHAPTER THE CONJUGATE BEA ETHOD Calculus and Structures 77 Copyright Chapter THE CONJUGATE BEA ETHOD.1 INTRODUCTION To find the deflection of a beam you must solve the equation,

More information

1. Attempt any ten of the following : 20

1. Attempt any ten of the following : 20 *17204* 17204 21314 3 Hours/100 Marks Seat No. Instructions : (1) All questions are compulsory. (2) Answer each next main question on a new page. (3) Illustrate your answers with neat sketches wherever

More information