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Parabolic arch 80 m: inclined load, forces at D

Short answer

Using equilibrium and hinge condition for a three-hinged parabolic arch under inclined and vertical loads, at section D (15 m from left support): bending moment = 109.77 kN m, normal thrust = 225.32 kN, radial shear = 22.61 kN.

A three hinged parabolic arch having span 80 m and central rise 8 m is loaded as shown in figure below. Determine bending moment, normal thrust and radial shear force at section D. [Figure: three hinged parabolic arch ACB; section D at 15 m horizontally from the left support A; 250 kN load inclined at 30° to the horizontal acting 10 m from the crown hinge C on the left half; 100 kN vertical load 15 m from the right support B.]

Data and assumptions: parabolic three-hinged arch, span L=80L = 80 m, rise f=8f = 8 m, y=4×8 x (80−x)802=0.005 x (80−x)y = \dfrac{4\times 8\,x\,(80-x)}{80^2} = 0.005\,x\,(80-x). The 250 kN inclined load acts at x=30x = 30 m (10 m left of the crown), pointing downward and to the right at 30° to the horizontal (assumed). Its components: horizontal 250cos⁡30∘=216.51250\cos30^\circ = 216.51 kN (to the right), vertical 250sin⁡30∘=125250\sin30^\circ = 125 kN (downward). 100 kN vertical load at 15 m from BB (x=65x = 65 m). Section DD at x=15x = 15 m.

Heights of the loads: y(30)=7.5y(30) = 7.5 m, y(65)=4.875y(65) = 4.875 m; at DD: y=4.875y = 4.875 m, tan⁡θ=0.005 (80−30)=0.25\tan\theta = 0.005\,(80-30) = 0.25, θ=14.04∘\theta = 14.04^\circ.

Let the thrusts be HAH_A (to the right at AA) and HBH_B (to the left at BB), and the vertical reactions VAV_A, VBV_B.

Reactions

Horizontal equilibrium:

HA−HB+216.51=0⇒HB=HA+216.51H_A - H_B + 216.51 = 0 \Rightarrow H_B = H_A + 216.51

Moments about AA:

VB×80=100×65+125×30+216.51×7.5⇒VB=11873.880=148.42 kNV_B\times 80 = 100\times 65 + 125\times 30 + 216.51\times 7.5 \Rightarrow V_B = \frac{11873.8}{80} = 148.42\ \text{kN} VA=225−148.42=76.58 kNV_A = 225 - 148.42 = 76.58\ \text{kN}

Hinge condition (moment about CC of the forces on the left part, CC at (40,8)(40, 8)):

VA×40−HA×8−125×10−216.51×(8−7.5)=0V_A\times 40 - H_A\times 8 - 125\times 10 - 216.51\times(8-7.5) = 0 HA=76.58×40−1250−216.51×0.58=213.11 kN,HB=429.61 kNH_A = \frac{76.58\times 40 - 1250 - 216.51\times 0.5}{8} = 213.11\ \text{kN}, \qquad H_B = 429.61\ \text{kN}

Forces at D (left part, 15 m from A, no load on it)

M=VA×15−HA×yD=76.58×15−213.11×4.875=109.77 kN mV=VAcos⁡θ−HAsin⁡θ=76.58(0.9701)−213.11(0.2425)=22.61 kNN=VAsin⁡θ+HAcos⁡θ=76.58(0.2425)+213.11(0.9701)=225.32 kN\begin{aligned} M &= V_A\times 15 - H_A\times y_D = 76.58\times 15 - 213.11\times 4.875 = 109.77\ \text{kN m}\\ V &= V_A\cos\theta - H_A\sin\theta = 76.58(0.9701) - 213.11(0.2425) = 22.61\ \text{kN}\\ N &= V_A\sin\theta + H_A\cos\theta = 76.58(0.2425) + 213.11(0.9701) = 225.32\ \text{kN} \end{aligned}

Answer: at DD: bending moment =109.77= 109.77 kN m (sagging), normal thrust =225.32= 225.32 kN, radial shear =22.61= 22.61 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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