NapkinCalc

Beams & Columns — Bending & Buckling

Bending stress — the load fibre furthest out feels

continues from lesson 1 — values defined earlier in the course stay live here

ELI5: when a beam bends, the top squashes and the bottom stretches — and the outermost fibres feel the most. Bending stress σ = M·c / I, where M is the bending moment and c is the distance to that outer fibre. It's what actually breaks a beam.

Pload:=10kNP_{load} := 10 kN = 10 kN a central point load
Lspan:=3mL_{span} := 3 m = 3 m the span between supports
Mmax=PloadLspan4M_{max} = \frac{P_{load} \cdot L_{span}}{4} = 7.5 kN m peak moment for a central load = 7.5 kN·m
cdist=hsec2c_{dist} = \frac{h_{sec}}{2} = 50 mm distance from centre to outer fibre
σbend:=Mmaxcdist/IrectinMPa\sigma _{bend} := M_{max} * c_{dist} / I_{rect} in MPa = 90 MPa bending stress = 90 MPa
✓ pass abs(σbend90MPa)<0.5MPaabs(\sigma _{bend} - 90 MPa) < 0.5 MPa the stress the beam's edge must survive
A simply supported beam under a central load — supports react, the middle bends the most.
A simply supported beam under a central load — supports react, the middle bends the most.
x * (3 - x)
00.511.5200.511.522.53

bending moment along a 3 m beam under uniform load — zero at the supports, peak in the middle