The shear force diagram for a simply supported beam carrying a uniformly distributed load of w per unit length, consists of:
Two right angled triangle
Let's analyze the shear force diagram for a simply supported beam carrying a uniformly distributed load (UDL) of intensity \(w\) per unit length over its entire span.
A simply supported beam is supported at both ends, typically with one pin support and one roller support, allowing it to carry vertical loads.
A uniformly distributed load is a load that is spread evenly over a section of the beam, meaning the load intensity \(w\) is constant along that section.
For a simply supported beam of length \(L\) subjected to a UDL \(w\) over its full length, the total load is \(wL\). Due to symmetry, the vertical reactions at both supports are equal.
Let \(R_A\) and \(R_B\) be the reactions at supports A and B respectively.
Total downward force = \(wL\)
Total upward force = \(R_A + R_B\)
For vertical equilibrium, \(R_A + R_B = wL\). Since the loading is symmetric, \(R_A = R_B\).
Therefore, \(R_A = R_B = \frac{wL}{2}\).
The shear force at any section of the beam is the algebraic sum of the vertical forces to the left or right of that section.
Let's consider a section at a distance \(x\) from the left support (A).
The forces to the left of this section are:
Considering upward forces as positive and downward forces as negative, the shear force \(V(x)\) at distance \(x\) from A is:
\(V(x) = R_A - wx = \frac{wL}{2} - wx\)
The equation \(V(x) = \frac{wL}{2} - wx\) shows that the shear force varies linearly with \(x\). This means the shear force diagram will be a straight line.
The shear force changes linearly from \(+\frac{wL}{2}\) at one end to \(-\frac{wL}{2}\) at the other end.
The point where the shear force is zero can be found by setting \(V(x) = 0\):
\(\frac{wL}{2} - wx = 0\)
\(wx = \frac{wL}{2}\)
\(x = \frac{L}{2}\)
This means the shear force is zero at the mid-span of the beam.
The shear force diagram is a graph of \(V(x)\) versus \(x\). Since \(V(x)\) is a linear function of \(x\), the graph is a straight line with a negative slope (\(-w\)).
The diagram starts at \(x=0\) with a value of \(+\frac{wL}{2}\) and ends at \(x=L\) with a value of \(-\frac{wL}{2}\), passing through zero at \(x=\frac{L}{2}\).
This linear variation results in the shear force diagram being composed of two parts:
When plotted against the horizontal beam axis (x-axis) and the vertical shear force axis (y-axis), these two parts form triangles. Since the axes are perpendicular, these triangles are right-angled triangles.
Both triangles have a base of length \(\frac{L}{2}\) and a height of \(\frac{wL}{2}\).
Therefore, the shear force diagram for a simply supported beam carrying a uniformly distributed load consists of two right-angled triangles.
| Property | Value/Description |
|---|---|
| Load Type | Uniformly Distributed Load (UDL) |
| Beam Type | Simply Supported |
| Reactions at Supports | \(\frac{wL}{2}\) at each end |
| Shear Force Equation | \(V(x) = \frac{wL}{2} - wx\) |
| Shear Force at Supports | \(+\frac{wL}{2}\) and \(-\frac{wL}{2}\) |
| Point of Zero Shear Force | Mid-span (\(x = \frac{L}{2}\)) |
| Shape of SFD | Two right-angled triangles |
Understanding shear force diagrams is crucial in structural analysis. The shape of the diagram depends heavily on the type of loading and supports. Here are some other common cases:
Comparing these cases helps illustrate how different loading conditions result in distinct shear force diagram shapes, from rectangles (constant shear) to triangles (linearly varying shear) to parabolas (for bending moment with UDL, but not shear force in this case).
The bending moment diagram of a simply supported beam carrying uniformly distributed load over the entire span is-
A simply supported beam is subjected to a linearly varying load from one end to other end. The nature of variation of shear force diagram is-
Which type of beam, freely supported at two points, has one or both ends extending beyond these supports?
Which of the following statements are correct?
Point of contraflexure in a beam occurs when the bending moment