Shear Force Diagram Calculator

Support reactions, internal shear V(x) and shear stress, solved step by step
A 6 m simply supported beam carries a 12 kN point load 2 m from the left support. Find the shear force diagram.
An 8 m simply supported beam carries a UDL of 4 kN/m. Where is the shear zero?
Find the average and maximum shear stress for V = 16 kN on a 50 mm x 150 mm rectangle
A 3 m cantilever carries 10 kN at its free end. Find the shear at the wall.

Reactions First, Then the Shear Force

The internal shear force VV at a section is the net transverse force carried across it. Cut the beam anywhere and sum everything to one side:

V(x)=тИСFleft┬аof┬аthe┬аcutV(x) = \sum F_{\text{left of the cut}}

Before you can do that you need the support reactions, from the two statics equations:

тИСFy=0,тИСM=0\sum F_y = 0, \qquad \sum M = 0

Symbols and units:

  • VV тАФ internal shear force, newtons (N), usually kN in structures
  • RA,RBR_A, R_B тАФ support reactions, N
  • ww тАФ uniformly distributed load, newtons per metre (N/m)
  • xx тАФ distance from the left end, metres (m)

Shape rules that let you sketch V(x)V(x) without integrating:

  • an unloaded span gives a horizontal shear line
  • a point load causes a vertical jump equal to that load
  • a uniform load ww gives a straight line of slope тИТw-w

When it applies: statically determinate beams, where two equations are enough. Continuous or fixed-fixed beams are indeterminate and need compatibility conditions as well.

The assumption people forget: replace a distributed load by its resultant, wLwL acting at its centroid, only when taking moments тАФ never when drawing V(x)V(x).

From Shear Force to Shear Stress

Once VV is known, the stress it produces on the cross-section follows. The quick estimate is the average shear stress:

╧Дavg=VA\tau_{\text{avg}} = \frac{V}{A}

with AA the cross-sectional area in m┬▓ and ╧Д\tau in pascals. But shear stress is not uniform through the depth тАФ it is zero at the top and bottom faces and peaks at the neutral axis. The exact distribution is

╧Д=VQIтАЙt\tau = \frac{VQ}{I\,t}

where QQ is the first moment of the area above the level of interest (m┬│), II is the second moment of area (mтБ┤) and tt is the width there (m). For a rectangular section this evaluates to a simple result:

╧ДmaxтБб=3V2A=1.5тАЙ╧Дavg\tau_{\max} = \frac{3V}{2A} = 1.5\,\tau_{\text{avg}}

and for a solid circular section ╧ДmaxтБб=4V/(3A)\tau_{\max} = 4V/(3A).

Design check: the largest тИгVтИг|V| almost always sits at a support, so that is where you check shear.

The assumption people forget: the 1.51.5 factor is specific to rectangles. Using ╧Дavg\tau_{\text{avg}} alone underestimates the peak by 50%50\%.

Common Mistakes to Avoid

  • Drawing the diagram before finding the reactions тАФ every value on it depends on them.
  • Missing the jump at a point load тАФ the shear steps discontinuously by exactly the load.
  • Getting the sign convention backwards тАФ pick one (upward force on the left segment is positive shear) and hold it for the whole beam.
  • Sloping the line the wrong way under a UDL тАФ the slope is тИТw-w, so shear falls left to right.
  • Using the resultant of a UDL when cutting тАФ only the portion left of the cut, wxwx, acts.
  • Assuming ╧ДmaxтБб=V/A\tau_{\max} = V/A тАФ for a rectangle the peak is 1.51.5 times that.
  • Mixing mm and m in ╧Д=V/A\tau = V/A тАФ a 50├Ч15050 \times 150 mm section is 7.5├Ч10тИТ37.5 \times 10^{-3} m┬▓.

Examples

Step 1: Moments about AA: RB(6.0┬аm)=(12┬аkN)(2.0┬аm)=24┬аkN\cdotpmR_B(6.0\ \text{m}) = (12\ \text{kN})(2.0\ \text{m}) = 24\ \text{kN┬╖m}, so RB=4.0┬аkNR_B = 4.0\ \text{kN}
Step 2: Vertical equilibrium: RA=12┬аkNтИТ4.0┬аkN=8.0┬аkNR_A = 12\ \text{kN} - 4.0\ \text{kN} = 8.0\ \text{kN}
Step 3: For 0<x<2.00 < x < 2.0 m: V=RA=+8.0┬аkNV = R_A = +8.0\ \text{kN} (constant, no load in between)
Step 4: For 2.0<x<6.02.0 < x < 6.0 m: V=8.0┬аkNтИТ12┬аkN=тИТ4.0┬аkNV = 8.0\ \text{kN} - 12\ \text{kN} = -4.0\ \text{kN} тАФ a 1212 kN jump at the load
Answer: RA=8.0R_A = 8.0 kN, RB=4.0R_B = 4.0 kN; V=+8.0V = +8.0 kN then тИТ4.0-4.0 kN, so тИгVтИгmaxтБб=8.0|V|_{\max} = 8.0 kN

Step 1: Total load =wL=(4.0┬аkN/m)(8.0┬аm)=32┬аkN= wL = (4.0\ \text{kN/m})(8.0\ \text{m}) = 32\ \text{kN}; by symmetry RA=RB=16┬аkNR_A = R_B = 16\ \text{kN}
Step 2: Cutting at xx: V(x)=RAтИТwx=16┬аkNтИТ(4.0┬аkN/m)xV(x) = R_A - wx = 16\ \text{kN} - (4.0\ \text{kN/m})x
Step 3: V=0V = 0 when x=(16┬аkN)├╖(4.0┬аkN/m)=4.0┬аmx = (16\ \text{kN}) \div (4.0\ \text{kN/m}) = 4.0\ \text{m} тАФ midspan, where the bending moment peaks
Step 4: Maximum shear is at the supports: тИгVтИгmaxтБб=16┬аkN|V|_{\max} = 16\ \text{kN}
Answer: V(x)=16тИТ4xV(x) = 16 - 4x kN, zero at x=4.0x = 4.0 m, with тИгVтИгmaxтБб=16|V|_{\max} = 16 kN

Step 1: A=(0.050┬аm)(0.150┬аm)=7.5├Ч10тИТ3┬аm2A = (0.050\ \text{m})(0.150\ \text{m}) = 7.5 \times 10^{-3}\ \text{m}^2
Step 2: ╧Дavg=V/A=(16├Ч103┬аN)├╖(7.5├Ч10тИТ3┬аm2)=2.13├Ч106┬аPa\tau_{\text{avg}} = V/A = (16 \times 10^3\ \text{N}) \div (7.5 \times 10^{-3}\ \text{m}^2) = 2.13 \times 10^6\ \text{Pa}
Step 3: For a rectangle, ╧ДmaxтБб=1.5тАЙ╧Дavg\tau_{\max} = 1.5\,\tau_{\text{avg}} at the neutral axis
Step 4: ╧ДmaxтБб=1.5(2.13┬аMPa)=3.20┬аMPa\tau_{\max} = 1.5(2.13\ \text{MPa}) = 3.20\ \text{MPa}
Answer: ╧ДavgтЙИ2.13\tau_{\text{avg}} \approx 2.13 MPa, ╧ДmaxтБбтЙИ3.20\tau_{\max} \approx 3.20 MPa

Frequently Asked Questions

Find the support reactions from ╬гF = 0 and ╬гM = 0, then cut the beam at the section of interest and sum every vertical force on one side of the cut. That sum is the internal shear force V there, in newtons or kilonewtons.

Start at the left reaction and move right. A point load makes the line jump by that load, an unloaded stretch keeps it horizontal, and a uniform load w makes it slope at тИТw. The diagram must return to zero at the far end.

Almost always at a support, because the reaction is the largest single force applied. For a symmetric uniformly loaded simply supported beam the shear peaks at wL/2 at each support and passes through zero at midspan.

The average value is ╧Д = V/A, with V in newtons and the cross-sectional area in m┬▓. The true peak is at the neutral axis: ╧Д = VQ/(It), which for a rectangular section works out to 1.5V/A and for a circle to 4V/(3A).

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