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Arch 20 m: reactions, BM, thrust, shear, BMD

Short answer

Reactions: R_A = 15.09 kN at 57.99° to horizontal, R_B = 8.62 kN at 21.8° (thrust H = 8 kN). At 4 m from left: M = 14.72 kN m, N = 9.29 kN, V = 0.87 kN. Maximum positive moment +15.06 kN m, maximum negative -8 kN m.

A three hinged parabolic arch as shown in fig-9 is loaded with udl 2 kN/m on the left 8 m length. Calculate (a) direction and magnitude of reaction at supports, (b) the bending moment, normal thrust and radial shear at 4m from left end, (c) draw bending moment diagram showing maximum positive and negative values. [Figure: three hinged parabolic arch, span 20 m, rise 4 m; 2 kN/m UDL on the left 8 m.]

Data: three-hinged parabolic arch, span L=20L = 20 m, rise f=4f = 4 m (y=0.04 x(20−x)y = 0.04\,x(20-x)), supports at the same level; UDL 2 kN/m on the left 8 m (x=0x = 0 to 8 m), total 16 kN acting at 4 m from AA.

(a) Reactions

VB×20=16×4⇒VB=3.2 kN,VA=16−3.2=12.8 kNV_B\times 20 = 16\times 4 \Rightarrow V_B = 3.2\ \text{kN}, \qquad V_A = 16 - 3.2 = 12.8\ \text{kN}

Crown hinge (MC=0M_C = 0), left part:

H×4=12.8×10−16×6=32⇒H=8 kNH\times 4 = 12.8\times 10 - 16\times 6 = 32 \Rightarrow H = 8\ \text{kN}

The reaction at each support is the resultant of its vertical component and the thrust:

  • At AA: RA=12.82+82=15.09R_A = \sqrt{12.8^2 + 8^2} = 15.09 kN, inclined at tan⁡−112.88=57.99∘\tan^{-1}\dfrac{12.8}{8} = 57.99^\circ above the horizontal, directed up and to the right (towards the span).
  • At BB: RB=3.22+82=8.62R_B = \sqrt{3.2^2 + 8^2} = 8.62 kN, inclined at tan⁡−13.28=21.8∘\tan^{-1}\dfrac{3.2}{8} = 21.8^\circ above the horizontal, directed up and to the left.

(b) Forces at 4 m from the left end

At x=4x = 4 m: y=0.04×4×16=2.56y = 0.04\times 4\times 16 = 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. Simple-beam shear Vb=VA−2×4=4.8V_b = V_A - 2\times 4 = 4.8 kN.

M=VA×4−2×4×2−H y=12.8×4−16−8×2.56=14.72 kN mV=Vbcos⁡θ−Hsin⁡θ=4.8(0.9015)−8(0.4327)=0.87 kNN=Vbsin⁡θ+Hcos⁡θ=4.8(0.4327)+8(0.9015)=9.29 kN\begin{aligned} M &= V_A\times 4 - 2\times 4\times 2 - H\,y = 12.8\times 4 - 16 - 8\times 2.56 = 14.72\ \text{kN m}\\ V &= V_b\cos\theta - H\sin\theta = 4.8(0.9015) - 8(0.4327) = 0.87\ \text{kN}\\ N &= V_b\sin\theta + H\cos\theta = 4.8(0.4327) + 8(0.9015) = 9.29\ \text{kN} \end{aligned}

(c) Bending moment diagram

M=Mb−H yM = M_b - H\,y along the span:

x (m)M (kN m)
00
210.08
414.72
613.92
87.68
100
12-5.12
14-7.68
16-7.68
18-5.12
200

The bending moment is zero at AA, at the crown hinge CC (x=10x = 10 m) and at BB. The maximum positive (sagging) value is about +15.06 kN m at x≈4.7x \approx 4.7 m (under the UDL) and the maximum negative (hogging) value is about -8 kN m at x≈15x \approx 15 m (in the right half).

 M (kN m)
 +15.06      ___
        _.-'   '-._
 0 ---A'---------C'-._----------B---
                       '-._ 
                           '--- -8

Answer: (a) RA=15.09R_A = 15.09 kN at 57.99° to the horizontal, RB=8.62R_B = 8.62 kN at 21.8° (thrust H=8H = 8 kN); (b) M=14.72M = 14.72 kN m, N=9.29N = 9.29 kN, V=0.87V = 0.87 kN at 4 m from the left; (c) maximum M=+15.06M = +15.06 kN m and minimum M=−8M = -8 kN m.

✓ Answer checked by Claude Opus 5.5 (high effort)

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