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Parabolic arch 90 m: BM, shear, thrust at D

Short answer

At section D (30 m) of a 90 m span, 6 m rise three-hinged parabolic arch with 180 kN at 25 m left and UDL 6 kN/m right half: reactions RA=197.5 kN, H=881.25 kN. With y=5.333 m, θ=5.08°, Mb=5025 kN m, Vb=17.5 kN. Bending moment = 325 kN m, radial shear = −60.59 kN, normal thrust = 879.34 kN.

Determine bending moment, radial shear force and normal thrust at point D of the three hinged parabolic arch shown in figure below. [Figure: span 90 m, rise 6 m; 180 kN vertical load 25 m from the left support; section D 30 m from the left support A; 6 kN/m UDL over the right half.]

Data: parabolic three-hinged arch, L=90L = 90 m, f=6f = 6 m. 180 kN vertical load at 25 m from AA; UDL 6 kN/m on the right half (x=45x = 45 to 90 m). Section DD at x=30x = 30 m from AA.

Step 1: Equation of the arch

y=4f x (L−x)L2=4×6 x (90−x)902y = \frac{4f\,x\,(L-x)}{L^2} = \frac{4\times 6\,x\,(90-x)}{90^2} tan⁡θ=dydx=4f (L−2x)L2\tan\theta = \frac{dy}{dx} = \frac{4f\,(L-2x)}{L^2}

At the section x=30x = 30 m: y=5.333y = 5.333 m, tan⁡θ=0.0889\tan\theta = 0.0889, so θ=5.08∘\theta = 5.08^\circ, sin⁡θ=0.0885\sin\theta = 0.0885, cos⁡θ=0.9961\cos\theta = 0.9961.

Step 2: Vertical reactions

Taking moments about AA for the whole arch:

RB×90=180×25+(6×45)×67.5=22725⇒RB=252.5 kNR_B \times 90 = 180\times 25 + (6\times 45)\times 67.5 = 22725 \Rightarrow R_B = 252.5\ \text{kN} RA=450−252.5=197.5 kNR_A = 450 - 252.5 = 197.5\ \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=6f = 6 m):

H×6=197.5×45−180×20=5287.5⇒H=881.25 kNH \times 6 = 197.5\times 45 - 180\times 20 = 5287.5 \Rightarrow H = 881.25\ \text{kN}

Step 4: Forces at the section (x = 30 m)

Simple-beam values at the section: Mb=5025M_b = 5025 kN m, Vb=17.5V_b = 17.5 kN.

M=Mb−H y=5025−881.25×5.333=325 kN mV=Vbcos⁡θ−Hsin⁡θ=17.5×0.9961−881.25×0.0885=−60.59 kNN=Vbsin⁡θ+Hcos⁡θ=17.5×0.0885+881.25×0.9961=879.34 kN\begin{aligned} M &= M_b - H\,y = 5025 - 881.25\times 5.333 = 325\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = 17.5\times 0.9961 - 881.25\times 0.0885 = -60.59\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 17.5\times 0.0885 + 881.25\times 0.9961 = 879.34\ \text{kN} \end{aligned}

Answer: at DD: bending moment =325= 325 kN m, radial shear =−60.59= -60.59 kN, normal thrust =879.34= 879.34 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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