Example board · Engineering

Beams: shear, bending and deflection

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Structural Mechanics Beams: shear, bending and deflectionStudy
BeamsBeams: shear, bending and deflection11 sections · 3 columns
The six standard cases
Beam and loadMax shearMax momentWhereMax deflectionWorked M: L = 6 m, P = 20 kN, w = 10 kN/m
Simply supported, point load P at midspanP/2PL/4MidspanPL³/48EI30 kNm
Simply supported, UDL wwL/2wL²/8Midspan5wL⁴/384EI45 kNm
Cantilever, point load P at the tipPPLAt the supportPL³/3EI, at the tip120 kNm
Cantilever, UDL wwLwL²/2At the supportwL⁴/8EI, at the tip180 kNm
Fixed both ends, point load P at midspanP/2PL/8Ends and midspanPL³/192EI15 kNm
Fixed both ends, UDL wwL/2wL²/12, hoggingEnds (wL²/24 at midspan)wL⁴/384EI30 kNm (15 at midspan)
Shear stress
  • τ = VQ/Ib: Q is the first moment of area beyond the cut
  • Largest at the neutral axis, zero at the top and bottom
  • Rectangle: τmax⁡\tau_{\max} = 1.5 V/A
  • In an I-beam the web carries almost all of it
Units and traps
  • kNm to Nmm is × 10⁶; kN/m is the same as N/mm
  • Cantilever: the peak moment is at the support, not the tip
  • Fixed ends hog: the moment over the supports is negative
  • Don't forget the beam's own weight: it is a UDL
  • Many Australian courses plot M on the tension side; the diagram here plots sagging above
The rules that draw the diagrams
  • Slope of the shear diagram = the load; slope of the moment diagram = the shear
  • So M peaks where V crosses zero
  • No load: V flat, M straight. UDL: V sloped, M a parabola
  • Point load: a step in V, a kink in M. Applied couple: a step in M
  • The change in M between two points = the area under V between them
Bending stress
  • σ = My/I; at the extreme fibre σ = M/Z, with Z=I/ymax⁡Z = I/y_{\max}
  • Zero on the neutral axis, largest at the top and bottom
  • Sagging: compression on top, tension underneath
  • Rectangle b × d: I = bd³/12, Z = bd²/6
Deflection
  • EI d²y/dx² = M: integrate twice, then fit the supports
  • Point load: δ ∝ L³. UDL: δ ∝ L⁴, so double the span, 16× the sag
  • Superposition: add the cases, since the beam stays linear elastic
  • Serviceability: span/250 is a common total-deflection limit (AS 3600)
Drawing them, in order
  1. Free-body diagram; the reactions from ΣFy = 0 and ΣM = 0
  2. Cut at each change of load; take equilibrium of one side
  3. Plot V left to right: steps at point loads, slopes under UDLs
  4. Plot M from the areas under V
  5. Check M returns to zero at a pinned or free end
Supports and reactions
  • Pin: two reactions, no moment. Roller: one reaction
  • Fixed: two reactions and a moment
  • Simply supported and cantilever: statically determinate
  • Fixed–fixed or propped: indeterminate, so add compatibility (deflection) to equilibrium
Why beams are deep
  • I grows with d³: double the depth for 8× the stiffness
  • Z grows with d²: double the depth for 4× the strength
  • Double the width: only 2× of each
  • An I-section puts its area in the flanges, where the stress is
Worked: 6 m span, 10 kN/m
  • Reactions wL/2 = 30 kN; Mmax⁡M_{\max} = wL²/8 = 45 kNm
  • 200 × 400 mm: Z = 5.33 × 10⁶ mm³, σ = M/Z = 8.4 MPa
  • E = 10,000 MPa, I = 1.07 × 10⁹ mm⁴: δ = 15.8 mm
  • Span/250 = 24 mm: it passes

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