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Parabolic arch 100 m: UDL left half and 80 kN

Short answer

For a three-hinged parabolic arch (span 100 m, rise 10 m) with 50 kN/m UDL left half and 80 kN at 25 m from right, at section D (20 m from left): y=6.4 m, θ=13.5°. Reactions: RA=1895 kN, H=3225 kN. Bending moment = 7260 kN m, shear = 117.66 kN, thrust = 3344.82 kN.

In the three hinged parabolic arch shown in figure below determine bending moment, normal thrust and radial shear force at section D. [Figure: parabolic three hinged arch, span 100 m, rise 10 m at the crown C; section D at 20 m horizontally from the left support A; 50 kN/m UDL over the left half; 80 kN vertical load 25 m from the right support B.]

Data: parabolic three-hinged arch, L=100L = 100 m, rise f=10f = 10 m at the crown CC. UDL 50 kN/m on the left half (x=0x = 0 to 50 m); 80 kN vertical load 25 m from BB (x=75x = 75 m). Section DD at x=20x = 20 m from AA.

Step 1: Equation of the arch

y=4f x (L−x)L2=4×10 x (100−x)1002y = \frac{4f\,x\,(L-x)}{L^2} = \frac{4\times 10\,x\,(100-x)}{100^2} tan⁡θ=dydx=4f (L−2x)L2\tan\theta = \frac{dy}{dx} = \frac{4f\,(L-2x)}{L^2}

At the section x=20x = 20 m: y=6.4y = 6.4 m, tan⁡θ=0.24\tan\theta = 0.24, so θ=13.5∘\theta = 13.5^\circ, sin⁡θ=0.2334\sin\theta = 0.2334, cos⁡θ=0.9724\cos\theta = 0.9724.

Step 2: Vertical reactions

Taking moments about AA for the whole arch:

RB×100=(50×50)×25+80×75=68500⇒RB=685 kNR_B \times 100 = (50\times 50)\times 25 + 80\times 75 = 68500 \Rightarrow R_B = 685\ \text{kN} RA=2580−685=1895 kNR_A = 2580 - 685 = 1895\ \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=1895×50−(50×50)×25=32250⇒H=3225 kNH \times 10 = 1895\times 50 - (50\times 50)\times 25 = 32250 \Rightarrow H = 3225\ \text{kN}

Step 4: Forces at the section (x = 20 m)

Simple-beam values at the section: Mb=27900M_b = 27900 kN m, Vb=895V_b = 895 kN.

M=Mb−H y=27900−3225×6.4=7260 kN mV=Vbcos⁡θ−Hsin⁡θ=895×0.9724−3225×0.2334=117.66 kNN=Vbsin⁡θ+Hcos⁡θ=895×0.2334+3225×0.9724=3344.82 kN\begin{aligned} M &= M_b - H\,y = 27900 - 3225\times 6.4 = 7260\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = 895\times 0.9724 - 3225\times 0.2334 = 117.66\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 895\times 0.2334 + 3225\times 0.9724 = 3344.82\ \text{kN} \end{aligned}

Answer: at DD: bending moment =7260= 7260 kN m, normal thrust =3344.82= 3344.82 kN, radial shear =117.66= 117.66 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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