- Practice · 8 marks
Derivation of the flexure formula
Short answer
Assumptions: straight beam, homogeneous, isotropic, Hooke's law, plane sections remain plane, symmetry, large curvature radius. Derivation: strain ε = y/R, stress σ = Ey/R. Zero net axial force gives ∫y dA = 0, so neutral axis through centroid. Moment M = EI/R, thus M/I = σ/y = E/R.
State the assumptions made in the theory of simple bending and derive the flexure formula M/I = sigma/y = E/R. Show that the neutral axis passes through the centroid of the cross-section.
Assumptions
- The beam is initially straight, with constant cross-section, and the material is homogeneous and isotropic.
- The material obeys Hooke's law and is the same in tension and compression.
- Plane sections remain plane after bending (Bernoulli's assumption).
- The beam bends in a plane of symmetry and the loads act in that plane.
- The radius of curvature is large compared with the depth of the beam.
- Each layer is free to expand or contract, with no stress between layers.
Derivation
___ M M ___
---/ \_____N_____A_____/ \---
top: compression O = centre of curvature
NA : unchanged length
bottom: tension
Consider a length of beam bent to a radius (measured to the neutral layer) that subtends an angle at the centre of curvature. A layer at distance from the neutral layer, measured away from the centre of curvature, has original length and new length .
By Hooke's law:
So the stress varies linearly with : tensile on the side away from the centre of curvature and compressive on the side towards it.
Pure bending means no net axial force, so over the section
This says the first moment of area about the neutral axis is zero, so the neutral axis passes through the centroid.
The moment of resistance equals the applied moment :
where is the second moment of area about the neutral axis. From (1) and (2):
Use
The maximum stress is at the extreme fibre :
is the section modulus. For a rectangle ; for a circle .
✓ Answer checked by Claude Opus 5.5 (high effort)
Related questions
- Pure bending, neutral layer, neutral axis · Strength of Materials, chapter 3
- Derivation of shear stress formula in beams · Strength of Materials, chapter 5
- Bending stresses in a T-section beam · Strength of Materials, chapter 3
- Checking whether root locus passes through point P · Control Systems, chapter 5
- Principal MI and axis of composite section · Strength of Materials, chapter 2
- Neutral axis ratio in WSM beam · Design of RCC Structure, chapter 2
- Bending stress in unsymmetrical bending · Mechanics of Solids, chapter 7