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Circular arch ILDs at 3 m, then internal forces

Short answer

Using influence line diagrams for the section 3 m from the left support, the UDL on the left half and the 40 kN point load at 9 m from left give internal forces: bending moment 14.02 kN m, radial shear 7.79 kN, and normal thrust 71.69 kN. Horizontal thrust is 60 kN.

A three-hinged symmetrical circular arch is of 12 m span and 4 m rise. Draw influence line diagram for bending moment, radial shear and normal thrust in the section at distance of 3 m from the left support. Use the diagrams to determine these internal forces in the section when the left half of the span is loaded with a uniformly distributed load of intensity 20 kN/m and a vertical concentrated load of magnitude 40 kN at a distance of 3 m from the right support.

Data: three-hinged symmetrical circular arch, L=12L = 12 m, f=4f = 4 m. Radius R=L2/4+f22f=36+168=6.5R = \dfrac{L^2/4+f^2}{2f} = \dfrac{36+16}{8} = 6.5 m (centre 2.5 m below the springing level). Section DD at x=3x = 3 m from AA:

y=6.52−(3−6)2−2.5=3.266 m,tan⁡θ=6−35.766=0.5203, θ=27.49∘y = \sqrt{6.5^2-(3-6)^2} - 2.5 = 3.266\ \text{m}, \qquad \tan\theta = \frac{6-3}{5.766} = 0.5203, \ \theta = 27.49^\circ

Influence lines (unit load at x′x')

  • Thrust: H=x′2f=x′8H = \dfrac{x'}{2f} = \dfrac{x'}{8} for x′≤6x'\le 6; 12−x′8\dfrac{12-x'}{8} for x′≥6x'\ge 6 (peak 0.750.75 at the crown).
  • Bending moment: M=Mb−H yM = M_b - H\,y, with Mb=x′(12−3)12M_b = \dfrac{x'(12-3)}{12} for x′≤3x'\le 3 and 3(12−x′)12\dfrac{3(12-x')}{12} for x′≥3x'\ge 3.
  • Radial shear: V=Vbcos⁡θ−Hsin⁡θV = V_b\cos\theta - H\sin\theta with Vb=−x′12V_b = -\dfrac{x'}{12} (load left of DD) or 12−x′12\dfrac{12-x'}{12} (load right of DD).
  • Normal thrust: N=Vbsin⁡θ+Hcos⁡θN = V_b\sin\theta + H\cos\theta.
Load at x' (m)HM (m)V (radial)N
00000
3-0.3751.0251-0.39490.2173
3+0.3751.02510.49230.6788
60.75-0.94970.09740.8961
90.375-0.47490.04870.4481
120000

The M-ILD is positive near DD and negative towards the crown; the V-ILD has a jump of cos⁡θ=0.8871\cos\theta = 0.8871 at DD; the N-ILD has a jump of sin⁡θ=0.4615\sin\theta = 0.4615 at DD (shown by the two rows at 3 m).

Loading

UDL 20 kN/m on the left half (x′=0x' = 0 to 6 m) and a 40 kN point load at 3 m from the right support (x′=9x' = 9 m).

Each quantity =20×(area of ILD from 0 to 6)+40×(ordinate at 9 m)= 20\times(\text{area of ILD from 0 to 6}) + 40\times(\text{ordinate at 9 m}). The areas are obtained by the trapezoidal rule on each straight segment (using the values immediately left and right of DD):

QuantityArea (0-6 m)Ordinate at 9 mTotal
M1.6509-0.474914.02
V0.29220.04877.79
N2.68830.448171.69
H2.250.37560
M=14.02 kN mV=7.79 kNN=71.69 kNH=60 kN\begin{aligned} M &= 14.02\ \text{kN m}\\ V &= 7.79\ \text{kN}\\ N &= 71.69\ \text{kN}\\ H &= 60\ \text{kN} \end{aligned}

Check (direct statics): RA=100R_A = 100 kN, RB=60R_B = 60 kN, H=60H = 60 kN; M=100×3−20×3×1.5−60×3.266=14.02M = 100\times 3 - 20\times 3\times 1.5 - 60\times 3.266 = 14.02 kN m.

Answer: bending moment 14.0214.02 kN m (sagging), radial shear 7.797.79 kN, normal thrust 71.6971.69 kN at the section 3 m from the left support.

✓ Answer checked by Claude Opus 5.5 (high effort)

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