Mr. Akash Assistant Professor Department of Civil Engineering DCE Darbhanga Module- 3 Bending moment and Shear Force Diagrams Part-1 Introduction to Solid Mechanics Course Code- 101205
Syllabus Bending moment and Shear Force Diagrams BM and SF diagrams for cantilevers , simply supported and fixed beams with or without overhangs. Calculation of maximum BM and SF and the point of contra flexure under concentrated loads, uniformly distributed loads over the whole span or part of span, combination of concentrated loads (two or three) and uniformly distributed loads, uniformly varying loads, application of moments.
Beam A beam is a horizontal structural member in a building to resist the lateral loads or resists the forces laterally or transversely applied to the (beam) axis. Slab |> Beam |> Column |> Foundation
A structural element which has one dimension considerably larger than the other two dimensions , namely breadth and depth, and is supported at few points. Purpose of Beam Resist loads Counter bending moment and shear forces . Connect the structure together. Provide a uniform distribution of loads . The total effect of all the forces acting on the beam to produce shear forces and bending moment within the beam, that in turn induce internal stresses, strains and deflections of the beam .
Beam made of steel or reinforced concrete Cement (RCC) Main Bars – Provide to carry loads (Moments). Stirrups – To counter the shear stresses (Shear force). Support bars – These bars are located in the top portion of the beam and just function to hold the stirrups in place. B1 B2 T1 S1
The reactions depend upon the type of supports and type of loading Support: A thing that bears the weight of something or keeps it upright. A beam has to be supported at different points by supports to withstand loads transmitted to it . There are different kinds of supports used to support a beam . Simple Support Hinged/Pinned/Pivoted Support Roller or Knife Edge Support Fixed(Build-in) Support
Simple Support When Beam placed on simple surface. There is connection between beam and support. Only vertical reaction will be produced. Simple supports are idealized by some to be frictionless surface supports
Hinged support Hinged support or pinned support can resist forces in any direction but it does not resist moments. There will be two reaction at the support. Roller Support Roller support can resist forces only in one direction irrespective of the loads transmitted to the support. Nos. of reaction is one and the direction of the resisting force is always perpendicular to the base of the support.
Fixed support A beam with firmly fixed end preventing any kind of movements and rotation is considered as a fixed support. Fixed support resists movement of the beam in any direction and also it prevents the rotation of the beam. Hence it can resist forces in any direction and also it can resist moments (resists rotation ).
Types of Beam Based on equilibrium conditions: Statically determinate beam – Statically determinate structures are structures that can be analyzed using statics equations only, (i.e., equilibrium in all directions ). Statically indeterminate beam – Statically indeterminate structures can't be analyzed using statics equations only; they require other material properties, such as deformations, in order to analyze them. Based on the type of support : Simply supported beam Cantilever beam Overhanging beam Fixed beam Continuous beam
Simply Supported Beam A simply supported beam is a type of beam that has pinned support at one end and roller support at the other end. Depending on the load applied, it undergoes shearing and bending. It is the one of the simplest structural elements in existence. Cantilever Beam Cantilever beams a structure member of which one end is fixed and other is free. This is one of the famous type of beam used in trusses, bridges etc.
Overhanging Beam The overhanging beam is a combination of simply supported beam and a cantilever beam, so has heritage properties of the cantilever and simply supported beam. One or both of end overhang of this beam. The beam is supported by roller support between two ends. Fixed Beam The beam is fixed from both ends. It does not allow vertical movement. It is only under the shear no moment produces in these beams. It is used in trusses.
Continuous Beam The beam is similar to simply supported beam except more than two support is used on it. One end of it is supported by hinged support and the other one is roller support. It is used in long concrete bridges where the length of the bridge is too large. Propped Cantilever It is a beam with one end fixed and the other end simply supported.
Type of Loads Point load or Concentrated load When a load is acting on a relatively small area it is considered as point load or concentrated load. W = Point Load It is given in N or KN (2) Uniformly Distributed Load A Load which is spread over a beam in such a manner that each unit length of beam is loaded to the same intensity is known as uniformly distributed load. W = U.D.L It is given in N/m or KN/m .
(3) Uniformly varying Load A Load which is spread over a beam in such a manner that its intensity varies uniformly on each unit is called uniformly varying load. When load is zero at one end and increases uniformly to the other end it is known as triangular load . (4) External Moment A beam may be subjected to external moment at certain points. Example- the beam is subjected to clockwise moment of 30 kN -m at a distance of 2 m from the left support
Axial force thrust The axial force (AF) at any section of a beam is equal to the algebraic sum of the forces parallel to the axis of the beam either to the left or the right of the section. Shear force The shear force (SF) at any section of a beam is equal to the algebraic sum of the forces perpendicular to the axis of the beam either to the left or the right of the section. Shear Forces occurs when two parallel forces act out of alignment with each other. For example, in a large boiler made from sections of sheet metal plate riveted together, there is an equal and opposite force exerted on the rivets, owing to the expansion and contraction of the plates . Bending moment The bending moment (BM) at any section of a beam is equal to the algebraic sum of the moments of all the forces, either to the left or to the right of the section, about the section. At any point within a beam, the Bending Moment is the sum of each external force multiplied by the distance that is perpendicular to the direction of the force. Bending Moments are rotational forces within the beam that cause bending.
Sign Convention of Axial Force, Shear Force & Bending Moment
BM and SF diagrams for cantilevers Beam Case-1_ Cantilever with point load (a) Reactions (b) Shear Force Shear Force at any section x from A , S.F=P (Remain constant between A and C) There is no shear force between C and B. (c.)Bending Moment From the right. At any distance x from C, M=- Px ( negative sign because it is clockwise from the right) At x = a , M A = - Pa (Maximum B.M.) At x=0, M c =0 (Minimum B.M.) There is no bending moment between C and B.
Cantilever with point load at free end A B - (a) Reactions (b) Shear Force Shear Force at any section x from A , S.F=P (Remain constant between A and B) (c.)Bending Moment From the right. At any distance x from B, M=- Px ( negative sign because it is clockwise from the right) At point A (x=l ) M A = - Pl(Maximum B.M.) At point B ( x=0), M B =0 (Minimum B.M.)
Case- 2_ Cantilever with uniformly distributed load(UDL) This is hogging moment Shear Force At x , Fx = wl-wx when x=0, At point “A” F X = wl when x=l, At point “B” F X = 0 (b) Bending Moment Bending Moment at x when x=0, At point “A” when x=l, At point “B ” Mx =0 The variation is parabolic due to second degree equation.
Case-3 _ Cantilever with uniformly Varying load(UVL ) A cantilever beam of span L carries a uniformly varying load varying from zero at the free end to w/m at the fixed end. Total load on the beam = Area of the triangle = wL /2 Reactions R A = wL /2 Taking moments about A, Shear Force Calculating from the right, SF at x from B Fx = (wx/L)x/2 ( This + ve as it is download from the right.) This is a parabolic equation. At x=0 At point “B” , Fx = 0 At x=L , At point “A”, Fx = wL /2 Bending Moment Calculating from the right, BM at x from B Mx = At x=0 At point “B” , Mx = 0 At x=L , At point “A”, Mx = -
Case- 4_ Cantilever with Couple load A cantilever beam of span L carries a clockwise moment M at the free end. As there is no vertical load on the beam, with only one support , R AV =o, The reaction at A is restraining couple M A =M (a)Shear Force Fx = 0 throughout the beam ( n o vertical force on beam) (b) Bending Moment Bending Moment at x from B Mx =-M (remains constant throughout)
BM and SF diagrams for simply supported Beam Case-1_ Simply supported beam with point load A simply supported beam of span L carries a point load at a distance a from the left support . To find reactions, take moments about B; ( a)Shear Force SF between A and C SF = Pa/L ( + ve being upward from left) Remains constant between A and C Just to the right of C, SF = Pb /L –P =P(b/L-1) =-Pa/L Remains constant between C and B SF between C and B SF= - Pa/L (- ve being upward from right)
b) Bending Moment . At x=0 , At point”A ” M = 0 At x=a At point “C” M= Pab /L . At x=a , At point”A ” M = Pab /L ( This is equation of straight line) At x=L At point “C” M= 0
Case-2_ Simply supported beam with uniformly distributed load A simply-supported beam carries a UD load w/m throughout its length. By symmetry, the two reactions will be equal Otherwise, taking moments at B Shear Force Shear Force at A = + wL /2 , (positive as it is upwards from the left) At any x from A, SF= wL /2- wx At x =0 , At point “A” SF= wL /2, At x=L, At point “B” SF=- wL /2 At mid point SF= wL /2 –wx =0 , x=L/2
b) Bending Moment Bending moment at any distance x from A Mx = ( wL /2) -wx(x/2) Or, Mx = ……………….(1) This is equation of parabola . At x=0 , At point”A ” M = 0 At x=L At point “B” M= For maximum BM This is equation of shear force, By solving this , x = L/2. It means Maximum BM will be at the centre . So, Maximum BM =
Case-3_ Simply supported beam with uniformly varying load Shear Force SF at x , ………(a) Load intensity at x = wx/l A t x=0, At point “A” SF At x= l , At point”B” SF =
Putting SF =0 in equation (a) (b) Bending Moment BM at x, …………………………(b) At x=0, At point “A” At x=l, At point “B” To find the maximum value of the BM, This is similar to shear force , so Maximum BM at , Putting it equation (b)
Case-4_ Simply supported beam with triangular load Due to symmetry of loading, the reactions at A and B are equal.
A general equation of loading Shear Force For the left half from x=0 to x=l/2 SF at x , SF At x=0 , At Point”A ” SF = wl /4 At x= l/2 (At mid point) SF = 0 For the other half of the span, equation For x=l/2 to x=l SF at x, SF At x= l/2 (At mid point) SF = At x=0 , At Point”B” SF = wl /4
(b) Bending Moment For the left half from x=0 to x=l/2 BM At x=0 , At point “A” BM = 0 At x= l/2 (At mid point ), SF =0 BM is maximum For the other half of the span, equation For x=l/2 to x=l BM At x= l/2 (At mid point) SF = 0, BM is maximum At x=0 , At Point”B” BM =0
Case-5_ Simply supported beam with couple load Shear Force SF at x, In segment SF = -M/l (constant throughout beam) SF at x In segment CB , SF = -M/l ( acting upwards from the right) and is constant throughout
(b) Bending Moment In segment At x=a , the BM will have two values just to the left and right of the point at which the couple is acting In segment CB At x = a , At point “C” BM = M(l-a)/l At x= l , At point “B” BM=0
BM and SF diagrams for Overhanging beam Case-1_ Overhanging beam with UDL An overhanging beam of span L between supports and overhang length a is subjected to a UD load of w/m over the whole length. At Point “ A” SF = Point At SF=0 ,
SF=0 P oint of contraflexure- Where BM = 0
Point of contraflexure In a beam that is flexing (or bending), the point where there is zero bending moment is called the point of contraflexure. At that point, the direction of bending changes its sign from positive to negative or from negative to positive. (It may also be thought of as a change from compression to tension or vice versa ).