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Arch 100 m rise 15 m: rolling UDL 10 m, section 60 m

Short answer

For a three-hinged parabolic arch (span 100 m, rise 15 m) with a 10 m UDL of 50 kN/m, influence lines give at 60 m: max positive BM = +2136 kN m (shear 192 kN, thrust 584.6 kN) with load at 58.8–68.8 m; max negative BM = −1817 kN m (shear −136.6 kN, thrust 784.6 kN) with load at 40.83–50.83 m.

A three hinged parabolic arch of span 100 m and rise 15 m is to be designed to carry a rolling load of 50 kN/m of span 10 m. Determine the maximum bending moment, radial shear, and normal thrust at 60 m from the left support with the help of influence line diagrams.

Data: parabolic three-hinged arch, L=100L = 100 m, f=15f = 15 m, y=0.006 x(100−x)y = 0.006\,x(100-x). Rolling UDL 50 kN/m of length 10 m. Section DD at x=60x = 60 m (in the right half): y=14.4y = 14.4 m, tan⁡θ=0.006 (100−120)=−0.12\tan\theta = 0.006\,(100-120) = -0.12, so the tangent falls to the right (θ=−6.84∘\theta = -6.84^\circ).

For a section in the right half, the neutral point lies between the crown and the section.

ILDs for the section at x = 60 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=1.6667\dfrac{L}{4f} = 1.6667 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
50crown C1.667-4
54.55neutral point1.5150
60section D1.3334.8
100B00

The ILD of MM crosses zero at the neutral point, 54.55 m from AA (the vertical through the intersection of line AA–CC extended and line BB–DD extended). The ordinates are positive on one side of it and negative on the other.

Maximum positive bending moment

The UDL covers the region from x = 58.8 m to 68.8 m (the whole load is on the span); this lies in the positive region of the ILD, with equal ordinates at the two ends of the load.

M=w×(area of ILD)=50×(42.72)=2136 kN mH=w×(area of ILD of H)=50×(12.0667)=603.33 kN\begin{aligned} M &= w\times(\text{area of ILD}) = 50\times(42.72) = 2136\ \text{kN m}\\ H &= w\times(\text{area of ILD of }H) = 50\times(12.0667) = 603.33\ \text{kN} \end{aligned}

At the section: y=14.4y = 14.4 m, θ=−6.84∘\theta = -6.84^\circ, simple-beam shear Vb=121V_b = 121 kN.

V=Vbcos⁡θ−Hsin⁡θ=121×0.9929−603.33×(−0.1191)=192.02 kNN=Vbsin⁡θ+Hcos⁡θ=121×(−0.1191)+603.33×0.9929=584.62 kN\begin{aligned} V &= V_b\cos\theta - H\sin\theta = 121\times0.9929 - 603.33\times(-0.1191) = 192.02\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 121\times(-0.1191) + 603.33\times0.9929 = 584.62\ \text{kN} \end{aligned}

Maximum negative bending moment

The UDL covers the region from x = 40.83 m to 50.83 m (the whole load is on the span); this lies in the negative region of the ILD, with equal ordinates at the two ends of the load.

M=w×(area of ILD)=50×(−36.333)=−1816.7 kN mH=w×(area of ILD of H)=50×(15.2537)=762.69 kN\begin{aligned} M &= w\times(\text{area of ILD}) = 50\times(-36.333) = -1816.7\ \text{kN m}\\ H &= w\times(\text{area of ILD of }H) = 50\times(15.2537) = 762.69\ \text{kN} \end{aligned}

At the section: y=14.4y = 14.4 m, θ=−6.84∘\theta = -6.84^\circ, simple-beam shear Vb=−229.15V_b = -229.15 kN.

V=Vbcos⁡θ−Hsin⁡θ=(−229.15)×0.9929−762.69×(−0.1191)=−136.65 kNN=Vbsin⁡θ+Hcos⁡θ=(−229.15)×(−0.1191)+762.69×0.9929=784.55 kN\begin{aligned} V &= V_b\cos\theta - H\sin\theta = (-229.15)\times0.9929 - 762.69\times(-0.1191) = -136.65\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = (-229.15)\times(-0.1191) + 762.69\times0.9929 = 784.55\ \text{kN} \end{aligned}

Answer: at 60 m from the left support the maximum bending moments are +2136+2136 kN m (radial shear 192192 kN, normal thrust 584.6584.6 kN) and −1817-1817 kN m (radial shear −136.6-136.6 kN, normal thrust 784.6784.6 kN), with the 10 m UDL in the positions stated above.

✓ Answer checked by Claude Opus 5.5 (high effort)

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