Bending moment
The bending moment at a section is the sum of the moments of every force on one side of it. For a simply supported beam with a central point load, it peaks under the load:
Mmax =P·L4
- M
- bending moment
- N·m
- P
- point load
- N
- w
- uniform load
- N/m
- L
- span
- m
- x
- distance from left support
- m
- a
- load distance from left support
- m
- b
- load distance from right support
- m
- R
- support reaction
- N
| MP = PL/4 | 15 kN·m |
| Mw = wL²/8 | 9 kN·m |
| Mmax = MP + Mw | 24 kN·m |
Worked example
Uses the values in Fig. 2.2-1. Change them and the working updates.
Given
- Ppoint load at mid-span10 kN
- wuniform load2 kN/m
- Lspan6 m
Find
The bending moment at mid-span.
Solution
MP = PL/4 = 10 kN × 6 m / 4 = 15 kN·m
Mw = wL²/8 = 2 kN/m × (6 m)² / 8 = 9 kN·m
M = MP + Mw = 15 + 9 = 24 kN·m
Answer
M = 24 kN·m
Each support reaction is P/2 + wL/2 = 11 kN.
Related cases
Maximum bending moment for other common beams.
-
Simply supported, point load at a
M = PabL
-
Simply supported, uniform load
M = wL²8
-
Cantilever, end load
M = PL
-
Cantilever, uniform load
M = wL²2
Assumptions
- Loads add by superposition: the moment from each load is found alone and the results summed. This holds for linear-elastic beams with small deflections.
- A sagging moment, which bends the beam concave upwards, is positive.
- The supports are simple, so the moment is zero at each end.
- The beam's own weight is ignored unless it is included in w.
Derivation
Each support carries R = P/2 + wL/2. Cut the beam at distance x from the left support, with x ≤ L/2, and take moments of the forces to the left of the cut.
M(x) = Rx − wx²/2, since the uniform load on the left part,wx, acts atx/2.- Substitute R:
M(x) = Px/2 + wx(L − x)/2. - At mid-span,
x = L/2:M = PL/4 + wL²/8.
The point-load term grows linearly to mid-span and the uniform-load term is a parabola. Both peak at the centre, so their maxima add.