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Arch 100 m: rolling UDL 60 m, section at 30 m

Short answer

Using ILDs, maximum positive moment is +4375 kN m with normal thrust 1083.2 kN; maximum negative moment is -4375 kN m with normal thrust 2081.5 kN at the 30 m section.

In a three hinged symmetrical parabolic arch of span 100 m and central rise 10 m, a UDL load 25 kN/m and length 60 m moves from left to right. Determine maximum moment and normal thrusts at a section 30 m from left support.

Data: three-hinged symmetrical parabolic arch, L=100L = 100 m, f=10f = 10 m, y=4f x(L−x)L2=0.004 x (100−x)y = \dfrac{4f\,x(L-x)}{L^2} = 0.004\,x\,(100-x). A UDL of 25 kN/m and 60 m length moves from left to right. Section DD at x=30x = 30 m: yD=8.4y_D = 8.4 m, tan⁡θ=0.004 (100−60)=0.16\tan\theta = 0.004\,(100-60) = 0.16, θ=9.09∘\theta = 9.09^\circ. (When the load covers only the first or the last part of the span, part of the 60 m load is off the span.)

ILDs for the section at x = 30 m

The ILD of the horizontal thrust is H=x′2fH = \dfrac{x'}{2f} for a unit load at x′x' left of the crown and L−x′2f\dfrac{L-x'}{2f} right of it (peak L4f=2.5\dfrac{L}{4f} = 2.5 at the crown). The ILD of the bending moment at the section is M=Mb−H yM = M_b - H\,y.

x (m)PointILD of HILD of M at section
0A00
30section D1.58.4
41.67neutral point2.0830
50crown C2.5-6
100B00

The ILD of MM crosses zero at the neutral point, 41.67 m from AA (vertically below the intersection of line ADAD produced and line BCBC). The ordinates are positive on one side of it and negative on the other.

Maximum positive bending moment

The UDL covers the span from x=0x = 0 to 41.67 m (the rest of the load is still off the span), which is exactly the region where the ILD is positive.

M=w×(area of ILD)=25×175=4375 kN mH=w×(area of ILD of H)=25×43.403=1085.07 kN\begin{aligned} M &= w\times(\text{area of ILD}) = 25\times 175 = 4375\ \text{kN m}\\ H &= w\times(\text{area of ILD of }H) = 25\times 43.403 = 1085.07\ \text{kN} \end{aligned}

At the section: y=8.4y = 8.4 m, θ=9.09∘\theta = 9.09^\circ, simple-beam shear Vb=74.65V_b = 74.65 kN.

V=Vbcos⁡θ−Hsin⁡θ=74.65×0.9874−1085.07×0.158=−97.72 kNN=Vbsin⁡θ+Hcos⁡θ=74.65×0.158+1085.07×0.9874=1083.24 kN\begin{aligned} V &= V_b\cos\theta - H\sin\theta = 74.65\times0.9874 - 1085.07\times0.158 = -97.72\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 74.65\times0.158 + 1085.07\times0.9874 = 1083.24\ \text{kN} \end{aligned}

Maximum negative bending moment

The UDL covers the span from x=41.67x = 41.67 m to 100 m (the rest of the load is off the span beyond BB), which is exactly the region where the ILD is negative.

M=w×(area of ILD)=25×(−175)=−4375 kN mH=w×(area of ILD of H)=25×81.597=2039.93 kN\begin{aligned} M &= w\times(\text{area of ILD}) = 25\times(-175) = -4375\ \text{kN m}\\ H &= w\times(\text{area of ILD of }H) = 25\times 81.597 = 2039.93\ \text{kN} \end{aligned}

At the section: y=8.4y = 8.4 m, θ=9.09∘\theta = 9.09^\circ, simple-beam shear Vb=425.35V_b = 425.35 kN.

V=Vbcos⁡θ−Hsin⁡θ=425.35×0.9874−2039.93×0.158=97.72 kNN=Vbsin⁡θ+Hcos⁡θ=425.35×0.158+2039.93×0.9874=2081.51 kN\begin{aligned} V &= V_b\cos\theta - H\sin\theta = 425.35\times0.9874 - 2039.93\times0.158 = 97.72\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 425.35\times0.158 + 2039.93\times0.9874 = 2081.51\ \text{kN} \end{aligned}

Maximum horizontal thrust (for information)

The ILD of HH is positive everywhere; the thrust is greatest when the 60 m load is symmetrical about the crown (20 m to 80 m): Hmax=25×105=2625H_{max} = 25\times 105 = 2625 kN.

Answer: maximum bending moment at 30 m from the left support is +4375+4375 kN m (UDL from the left support up to the neutral point at 41.67 m), with normal thrust 1083.21083.2 kN, and −4375-4375 kN m (UDL from the neutral point to the right support), with normal thrust 2081.52081.5 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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