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Arch 20 m: ILDs and check by equilibrium

Short answer

Using influence line ordinates for the section at the load (4 m from left support), with a 4 kN point load: M = 7.68 kN m, radial shear = 2.019 kN, normal thrust = 3.188 kN. Equilibrium check confirms these values.

A three hinged symmetrical parabolic arch of span 20 m and rise 4 m is with a point load of magnitude 4 kN at 4 m distance from the left hinge. First, draw influence line diagram (ILD) for bending moment (BM), radial shear (RS), and normal thrust (NT) for the section where the point load is and then calculate the values of BM, RS and NT at the section using the ILDs. Also check these values of internal forces at the section by first principle using equilibrium equations.

Data: symmetrical parabolic three-hinged arch, L=20L = 20 m, f=4f = 4 m: y=4×4 x(20−x)400=0.04 x (20−x)y = \dfrac{4\times 4\,x(20-x)}{400} = 0.04\,x\,(20-x). A 4 kN point load acts at x=4x = 4 m from the left hinge (support) AA, and the internal forces are required at the section where the load acts. The section is taken just to the left of the load, so the load itself is not part of the free body. At x=4x = 4: y=2.56y = 2.56 m, tan⁡θ=0.04 (20−8)=0.48\tan\theta = 0.04\,(20-8) = 0.48, θ=25.64∘\theta = 25.64^\circ, sin⁡θ=0.4327\sin\theta = 0.4327, cos⁡θ=0.9015\cos\theta = 0.9015.

Influence lines (unit load at x')

  • RA=20−x′20R_A = \dfrac{20-x'}{20}, H=x′2f=x′8H = \dfrac{x'}{2f} = \dfrac{x'}{8} for x′≤10x'\le 10 and 20−x′8\dfrac{20-x'}{8} for x′≥10x'\ge 10 (peak L4f=1.25\dfrac{L}{4f} = 1.25 at the crown).
  • M=Mb−H yM = M_b - H\,y, with Mb=x′(20−4)20=0.8x′M_b = \dfrac{x'(20-4)}{20} = 0.8x' (x′≤4x'\le 4) or 4(20−x′)20\dfrac{4(20-x')}{20} (x′≥4x'\ge 4).
  • V=Vbcos⁡θ−Hsin⁡θV = V_b\cos\theta - H\sin\theta and N=Vbsin⁡θ+Hcos⁡θN = V_b\sin\theta + H\cos\theta, with Vb=−x′20V_b = -\dfrac{x'}{20} (load left of the section) or 20−x′20\dfrac{20-x'}{20} (load right of the section).
Unit load at x' (m)HM (m)V (radial)N
00000
40.51.920.50490.7969
101.25-1.2-0.09021.3433
150.625-0.6-0.04510.6716
200000

(The row at 4 m is for the load just to the right of the section.)

Values from the ILDs for P = 4 kN at the section

M=4×1.92=7.68 kN mV=4×0.5049=2.019 kNN=4×0.7969=3.188 kN\begin{aligned} M &= 4\times 1.92 = 7.68\ \text{kN m}\\ V &= 4\times 0.5049 = 2.019\ \text{kN}\\ N &= 4\times 0.7969 = 3.188\ \text{kN} \end{aligned}

Check by first principles (equilibrium)

RB=4×420=0.8 kN,RA=3.2 kNR_B = \frac{4\times 4}{20} = 0.8\ \text{kN}, \qquad R_A = 3.2\ \text{kN}

Moment at the crown hinge (right part): Hf=RB×10=8⇒H=84=2 kNH f = R_B\times 10 = 8 \Rightarrow H = \dfrac{8}{4} = 2\ \text{kN}.

M=RA×4−H×y=12.8−2×2.56=7.68 kN mV=RAcos⁡θ−Hsin⁡θ=3.2(0.9015)−2(0.4327)=2.019 kNN=RAsin⁡θ+Hcos⁡θ=3.2(0.4327)+2(0.9015)=3.188 kN\begin{aligned} M &= R_A\times 4 - H\times y = 12.8 - 2\times 2.56 = 7.68\ \text{kN m}\\ V &= R_A\cos\theta - H\sin\theta = 3.2(0.9015) - 2(0.4327) = 2.019\ \text{kN}\\ N &= R_A\sin\theta + H\cos\theta = 3.2(0.4327) + 2(0.9015) = 3.188\ \text{kN} \end{aligned}

The ILD values and the equilibrium values agree.

Answer: M=7.68M = 7.68 kN m, radial shear V=2.019V = 2.019 kN, normal thrust N=3.188N = 3.188 kN at the section.

✓ Answer checked by Claude Opus 5.5 (high effort)

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