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Arch equation given: BM, thrust, shear at 5 m

Short answer

Parabolic arch with rise 10 m, section at x = 35 m. Bending moment = 562.5 kN m, normal thrust = 420 kN, radial shear = -60 kN.

The equation of a three-hinged arch, with origin at its left support, is y=x−x240y = x - \frac{x^2}{40}. The span of the arch is 40 m. Determine bending moment, normal thrust and radial shear at section 5 m from right support, when the arch is carrying a uniformly distributed load of 30 kN/m for the right half.

Data: y=x−x240y = x - \dfrac{x^2}{40} with the origin at AA, span L=40L = 40 m. Comparing with y=4f x (L−x)L2=4fLx−4fL2x2y = \dfrac{4f\,x\,(L-x)}{L^2} = \dfrac{4f}{L}x - \dfrac{4f}{L^2}x^2: 4fL=1⇒f=10\dfrac{4f}{L} = 1 \Rightarrow f = 10 m (the arch is parabolic with a rise of 10 m). UDL 30 kN/m on the right half (x=20x = 20 to 40 m); the section is 5 m from BB, i.e. at x=35x = 35 m.

Step 1: Equation and slope

y=x−x240y = x - \frac{x^2}{40} tan⁡θ=dydx=1−x20\tan\theta = \frac{dy}{dx} = 1 - \frac{x}{20}

At the section x=35x = 35 m: y=4.375y = 4.375 m, tan⁡θ=−0.75\tan\theta = -0.75, so θ=−36.87∘\theta = -36.87^\circ, sin⁡θ=−0.6\sin\theta = -0.6, cos⁡θ=0.8\cos\theta = 0.8.

Step 2: Vertical reactions

Taking moments about AA for the whole arch:

RB×40=(30×20)×30=18000⇒RB=450 kNR_B \times 40 = (30\times 20)\times 30 = 18000 \Rightarrow R_B = 450\ \text{kN} RA=600−450=150 kNR_A = 600 - 450 = 150\ \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=10f = 10 m):

H×10=150×20=3000⇒H=300 kNH \times 10 = 150\times 20 = 3000 \Rightarrow H = 300\ \text{kN}

Step 4: Forces at the section (x = 35 m)

Simple-beam values at the section: Mb=1875M_b = 1875 kN m, Vb=−300V_b = -300 kN.

M=Mb−H y=1875−300×4.375=562.5 kN mV=Vbcos⁡θ−Hsin⁡θ=(−300)×0.8−300×(−0.6)=−60 kNN=Vbsin⁡θ+Hcos⁡θ=(−300)×(−0.6)+300×0.8=420 kN\begin{aligned} M &= M_b - H\,y = 1875 - 300\times 4.375 = 562.5\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = (-300)\times 0.8 - 300\times (-0.6) = -60\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = (-300)\times (-0.6) + 300\times 0.8 = 420\ \text{kN} \end{aligned}

Answer: at 5 m from the right support: M=562.5M = 562.5 kN m, normal thrust N=420N = 420 kN, radial shear V=−60V = -60 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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