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Circular arch: BM, shear, thrust at D

Short answer

Vertical reactions: 687.5 kN and 562.5 kN; horizontal thrust 1875 kN from moment equilibrium about the crown. At section D (15 m from left support), bending moment = 420.6 kN m, radial shear = 4.31 kN, and normal thrust = 1900.86 kN.

In three hinged circular arch shown in figure below determine bending moment, radial shear and normal thrust at section D. [Figure: three hinged circular arch ACB; span 60 m; crown hinge C with a rise of 5 m as drawn; section D on the left half, 15 m horizontally from A; UDL 25 kN/m over the left half; 500 kN vertical load on the right half, 15 m from B.]

Data: three-hinged circular arch, span L=60L = 60 m, rise f=5f = 5 m (crown hinge CC at mid-span). UDL 25 kN/m on the left half (x=0x = 0 to 30 m); 500 kN vertical load on the right half, 15 m from BB (x=45x = 45 m). Section DD is 15 m horizontally from AA.

Step 1: Equation of the arch

y=R2−(x−30)2−(R−f),R=L2/4+f22f=602/4+522×5=92.5 my = \sqrt{R^2-(x-30)^2} - (R-f),\quad R = \frac{L^2/4+f^2}{2f} = \frac{60^2/4+5^2}{2\times 5} = 92.5\ \text{m} tan⁡θ=dydx=30−xR2−(x−30)2\tan\theta = \frac{dy}{dx} = \frac{30-x}{\sqrt{R^2-(x-30)^2}}

At the section x=15x = 15 m: y=3.776y = 3.776 m, tan⁡θ=0.1643\tan\theta = 0.1643, so θ=9.33∘\theta = 9.33^\circ, sin⁡θ=0.1622\sin\theta = 0.1622, cos⁡θ=0.9868\cos\theta = 0.9868.

Step 2: Vertical reactions

Taking moments about AA for the whole arch:

RB×60=(25×30)×15+500×45=33750⇒RB=562.5 kNR_B \times 60 = (25\times 30)\times 15 + 500\times 45 = 33750 \Rightarrow R_B = 562.5\ \text{kN} RA=1250−562.5=687.5 kNR_A = 1250 - 562.5 = 687.5\ \text{kN}

Step 3: Horizontal thrust

The bending moment at the crown hinge CC is zero. Taking moments of the forces on the left of CC about CC (rise f=5f = 5 m):

H×5=687.5×30−(25×30)×15=9375⇒H=1875 kNH \times 5 = 687.5\times 30 - (25\times 30)\times 15 = 9375 \Rightarrow H = 1875\ \text{kN}

Step 4: Forces at the section (x = 15 m)

Simple-beam values at the section: Mb=7500M_b = 7500 kN m, Vb=312.5V_b = 312.5 kN.

M=Mb−H y=7500−1875×3.776=420.6 kN mV=Vbcos⁡θ−Hsin⁡θ=312.5×0.9868−1875×0.1622=4.31 kNN=Vbsin⁡θ+Hcos⁡θ=312.5×0.1622+1875×0.9868=1900.86 kN\begin{aligned} M &= M_b - H\,y = 7500 - 1875\times 3.776 = 420.6\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = 312.5\times 0.9868 - 1875\times 0.1622 = 4.31\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 312.5\times 0.1622 + 1875\times 0.9868 = 1900.86\ \text{kN} \end{aligned}

Answer: at DD: bending moment =420.6= 420.6 kN m (sagging), radial shear =4.31= 4.31 kN, normal thrust =1900.86= 1900.86 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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