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Hibbeler — Statics and Mechanics of Materials

Transverse shear — notched beam ends and integral joinery

Chapter 1 sized the roof beam for bending at mid-span — this is the different way a beam fails right at the support, and why a notched joint needs a generous shoulder.

See the build: ogopogo →

Concepts pulled in

  • Transverse shear (τ = VQ/(Ib))
  • Neutral axis

Chapter 1 sized the roof beam for bending in the middle of its span, where moment is highest. But beams don't just fail in the middle — they can fail right at the support, in a completely different way: horizontal shear, where the beam tries to slide along its own grain.

The formula: τ = VQ/(Ib), where V is the shear force (highest right at the supports, not the middle), Q is the first moment of area of the part of the cross-section above the point being checked, I is the moment of inertia, and b is the width. For a solid rectangular beam, the maximum horizontal shear stress lands at the neutral axis (the center), not the top or bottom edge — which is the opposite of where bending stress is worst.

Why this is the Ogopogo joint chapter

A notch cut into the bottom of a beam end (common in traditional joinery, and relevant to how the Ogopogo modular joints seat) removes material right where shear is highest and reduces the beam's effective depth right at the point of maximum shear stress — a notched end can fail in horizontal shear at a load a full-depth end would shrug off. This is the mechanism behind a failure mode that looks like nothing (no visible bend) until the beam splits lengthwise along the grain near a notch or bolt hole. It's also the reason integral joints (mortise-and-tenon, French cleats) need their bearing shoulder sized generously rather than cut thin to save material — the shoulder is carrying shear, not just holding shape.

Open items for a later pass

Exact notch/joint geometry for a specific Ogopogo connection, once a real joint detail exists to check against. Breyer Chapter 3 works the notched end with the NDS rules (a notch on the bottom face may not exceed a quarter of the beam depth, and the shear capacity falls with the square of the depth ratio), and the calculator on this page uses that form.

Try your own numbers

Starts on the Chapter 1 roof beam, checked for shear at the support instead of bending at mid-span. Add a notch to the bottom of the beam end to see how fast the margin disappears. Shear only: bending, deflection, bearing and bolt holes are separate checks.

  • Line load: (7 + 20) psf × 5 ft = 135 lb/ft
  • Reaction at each end: V = wL ÷ 2 = 135 × 10 ÷ 2 = 675 lb
  • Shear at the neutral axis, full depth: τ = 3V ÷ (2bd) = 3 × 675 ÷ (2 × 1.5 × 9.25) = 73 psi
  • That is 42% of the 175 psi allowable. This end carries up to 1,619 lb at that stress.
Shear holds

The notched-end formula is NDS 2018 Equation 3.4-3 for a notch on the tension face: V′ = (2/3) Fv′ b dn (dn ÷ d)², with the ratio squared, so a notch costs much more than the depth it removes. The NDS limits an end notch to d/4 (4.4.3.1). For a notched end the NDS has you use the full reaction, with no allowance for load near the support (3.4.3.2). Without a notch this check is a little cautious, because the NDS lets you ignore load within one beam depth of the support. Splits and checks along the grain, bolt holes, and bearing at the support are not included (bearing is in Breyer Chapter 3). Worked example, not a stamped design.

Print this calculation

Prints just the calculator above, with your numbers and the working, on a clean white page headed with this chapter and today's date. Add a name if you want it on the sheet, for a build file or a plan set.

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