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Parabolic arch 20 m: two loads and UDL, 5 m section

Short answer

At 5 m from the left support, bending moment = -115 kN m, normal thrust = 171.28 kN, and radial shear = 2.68 kN, using horizontal thrust H = 152 kN.

A parabolic 3-hinged arch has a span of 20 m with a central rise of 5 m. The arch is loaded with two point loads of 20 kN and 30 kN at a distance of 3 m and 7 m respectively, from the left support. It also carries a UDL of 25 kN/m over right half of the span. Determine the bending moment, normal thrust and radial shear at 5 m from left support.

Data: parabolic three-hinged arch, L=20L = 20 m, rise f=5f = 5 m. Loads: 20 kN at 3 m and 30 kN at 7 m from AA; UDL 25 kN/m on the right half (x=10x = 10 to 20 m). Section at x=5x = 5 m from AA.

Step 1: Equation of the arch

y=4f x (L−x)L2=4×5 x (20−x)202y = \frac{4f\,x\,(L-x)}{L^2} = \frac{4\times 5\,x\,(20-x)}{20^2} tan⁡θ=dydx=4f (L−2x)L2\tan\theta = \frac{dy}{dx} = \frac{4f\,(L-2x)}{L^2}

At the section x=5x = 5 m: y=3.75y = 3.75 m, tan⁡θ=0.5\tan\theta = 0.5, so θ=26.57∘\theta = 26.57^\circ, sin⁡θ=0.4472\sin\theta = 0.4472, cos⁡θ=0.8944\cos\theta = 0.8944.

Step 2: Vertical reactions

Taking moments about AA for the whole arch:

RB×20=20×3+30×7+(25×10)×15=4020⇒RB=201 kNR_B \times 20 = 20\times 3 + 30\times 7 + (25\times 10)\times 15 = 4020 \Rightarrow R_B = 201\ \text{kN} RA=300−201=99 kNR_A = 300 - 201 = 99\ \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=99×10−20×7−30×3=760⇒H=152 kNH \times 5 = 99\times 10 - 20\times 7 - 30\times 3 = 760 \Rightarrow H = 152\ \text{kN}

Step 4: Forces at the section (x = 5 m)

Simple-beam values at the section: Mb=455M_b = 455 kN m, Vb=79V_b = 79 kN.

M=Mb−H y=455−152×3.75=−115 kN mV=Vbcos⁡θ−Hsin⁡θ=79×0.8944−152×0.4472=2.68 kNN=Vbsin⁡θ+Hcos⁡θ=79×0.4472+152×0.8944=171.28 kN\begin{aligned} M &= M_b - H\,y = 455 - 152\times 3.75 = -115\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = 79\times 0.8944 - 152\times 0.4472 = 2.68\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 79\times 0.4472 + 152\times 0.8944 = 171.28\ \text{kN} \end{aligned}

Answer: at 5 m from the left support: M=−115M = -115 kN m, normal thrust N=171.28N = 171.28 kN, radial shear V=2.68V = 2.68 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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