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)=∑Fleft of the cutV(x) = \sum F_{\text{left of the cut}}

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

∑Fy=0,∑M=0\sum F_y = 0, \qquad \sum M = 0

Symbols and units:

  • VV — internal shear force, newtons (N), usually kN in structures
  • RA,RBR_A, R_B — support reactions, N
  • ww — uniformly distributed load, newtons per metre (N/m)
  • xx — 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 −w-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 — 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:

τavg=VA\tau_{\text{avg}} = \frac{V}{A}

with AA the cross-sectional area in mÂē and τ\tau in pascals. But shear stress is not uniform through the depth — it is zero at the top and bottom faces and peaks at the neutral axis. The exact distribution is

τ=VQI t\tau = \frac{VQ}{I\,t}

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

τmax⁥=3V2A=1.5 τavg\tau_{\max} = \frac{3V}{2A} = 1.5\,\tau_{\text{avg}}

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

Design check: the largest âˆĢVâˆĢ|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 τavg\tau_{\text{avg}} alone underestimates the peak by 50%50\%.

Common Mistakes to Avoid

  • Drawing the diagram before finding the reactions — every value on it depends on them.
  • Missing the jump at a point load — the shear steps discontinuously by exactly the load.
  • Getting the sign convention backwards — 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 — the slope is −w-w, so shear falls left to right.
  • Using the resultant of a UDL when cutting — only the portion left of the cut, wxwx, acts.
  • Assuming τmax⁥=V/A\tau_{\max} = V/A — for a rectangle the peak is 1.51.5 times that.
  • Mixing mm and m in τ=V/A\tau = V/A — a 50×15050 \times 150 mm section is 7.5×10−37.5 \times 10^{-3} mÂē.

Examples

Step 1: Moments about AA: RB(6.0 m)=(12 kN)(2.0 m)=24 kN\cdotpmR_B(6.0\ \text{m}) = (12\ \text{kN})(2.0\ \text{m}) = 24\ \text{kN·m}, so RB=4.0 kNR_B = 4.0\ \text{kN}
Step 2: Vertical equilibrium: RA=12 kN−4.0 kN=8.0 kNR_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 kNV = 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 kN−12 kN=−4.0 kNV = 8.0\ \text{kN} - 12\ \text{kN} = -4.0\ \text{kN} — 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 −4.0-4.0 kN, so âˆĢVâˆĢmax⁥=8.0|V|_{\max} = 8.0 kN

Step 1: Total load =wL=(4.0 kN/m)(8.0 m)=32 kN= wL = (4.0\ \text{kN/m})(8.0\ \text{m}) = 32\ \text{kN}; by symmetry RA=RB=16 kNR_A = R_B = 16\ \text{kN}
Step 2: Cutting at xx: V(x)=RA−wx=16 kN−(4.0 kN/m)xV(x) = R_A - wx = 16\ \text{kN} - (4.0\ \text{kN/m})x
Step 3: V=0V = 0 when x=(16 kN)÷(4.0 kN/m)=4.0 mx = (16\ \text{kN}) \div (4.0\ \text{kN/m}) = 4.0\ \text{m} — midspan, where the bending moment peaks
Step 4: Maximum shear is at the supports: âˆĢVâˆĢmax⁥=16 kN|V|_{\max} = 16\ \text{kN}
Answer: V(x)=16−4xV(x) = 16 - 4x kN, zero at x=4.0x = 4.0 m, with âˆĢVâˆĢmax⁥=16|V|_{\max} = 16 kN

Step 1: A=(0.050 m)(0.150 m)=7.5×10−3 m2A = (0.050\ \text{m})(0.150\ \text{m}) = 7.5 \times 10^{-3}\ \text{m}^2
Step 2: τavg=V/A=(16×103 N)÷(7.5×10−3 m2)=2.13×106 Pa\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, τmax⁥=1.5 τavg\tau_{\max} = 1.5\,\tau_{\text{avg}} at the neutral axis
Step 4: τmax⁥=1.5(2.13 MPa)=3.20 MPa\tau_{\max} = 1.5(2.13\ \text{MPa}) = 3.20\ \text{MPa}
Answer: τavg≈2.13\tau_{\text{avg}} \approx 2.13 MPa, τmax⁡≈3.20\tau_{\max} \approx 3.20 MPa

Frequently Asked Questions

Find the support reactions from ÎĢF = 0 and ÎĢM = 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 −w. 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 τ = V/A, with V in newtons and the cross-sectional area in mÂē. The true peak is at the neutral axis: τ = VQ/(It), which for a rectangular section works out to 1.5V/A and for a circle to 4V/(3A).

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