Skip to main content

Two-hinged arch: BM, thrust, radial shear, support yield

Short answer

For the two-hinged parabolic arch, H=(∫M0 y dx/EIc - δ)/(∫y^2 dx/EIc), giving H=410.94 kN. At D, M=-1664.06 kNm hogging, normal thrust N=437.28 kN compression, and radial shear Q=12.35 kN.

In the two hinged parabolic arch shown below, find the values of bending moment, normal thrust and radial shear at section D due to the given loading and due to yielding of support B by 10 mm. Take EIc=100×106 kNm2EI_c = 100\times10^{6}\ \text{kNm}^2, I=Icsec⁡θI = I_c \sec\theta. Also draw bending moment diagram. [Figure: two-hinged parabolic arch AB, span 120 m (60 m + 60 m), rise 20 m at crown C; section D at 30 m from A; 10 kN/m UDL on the right half CB.]

A two-hinged arch has one redundant, the horizontal thrust HH. With I=Icsec⁡θI = I_c\sec\theta the compatibility equation (support B yields outward by δ\delta) is

H=1EIc∫M0 y dx−δ1EIc∫y2 dx=Hload−δ EIc∫y2 dxH = \frac{\displaystyle\frac{1}{EI_c}\int M_0\,y\,dx - \delta}{\displaystyle\frac{1}{EI_c}\int y^2\,dx} = H_{load} - \frac{\delta\,EI_c}{\int y^2\,dx}

Data

Span L=120L = 120 m, rise h=20h = 20 m, EIc=100×106EI_c = 100\times10^6 kNm2^2, δ=10\delta = 10 mm =0.01= 0.01 m; UDL 1010 kN/m on CB (60 m to 120 m).

y=4h x(L−x)L2=x(120−x)180,tan⁡θ=dydx=120−2x180y = \frac{4h\,x(L-x)}{L^2} = \frac{x(120-x)}{180},\qquad \tan\theta = \frac{dy}{dx} = \frac{120 - 2x}{180}

Simple-beam reactions and M0M_0

UDL resultant =10×60=600= 10\times60 = 600 kN at 90 m: VB=600(90)120=450V_B = \dfrac{600(90)}{120} = 450 kN, VA=150V_A = 150 kN.

  • 0≤x≤600 \le x \le 60: M0=150 xM_0 = 150\,x
  • 60≤x≤12060 \le x \le 120: M0=150 x−5(x−60)2M_0 = 150\,x - 5(x-60)^2

Thrust

∫0120y2 dx=8h2L15=25600,∫0120M0 y dx=11520000\int_0^{120} y^2\,dx = \frac{8h^2L}{15} = 25600,\qquad \int_0^{120} M_0\,y\,dx = 11520000 Hload=1152000025600=450.00 kNH_{load} = \frac{11520000}{25600} = 450.00\ \text{kN} Hyield=−δ EIc∫y2dx=−0.01×100×10625600=−39.06 kNH_{yield} = -\frac{\delta\,EI_c}{\int y^2dx} = -\frac{0.01\times100\times10^6}{25600} = -39.06\ \text{kN} H=450.00+(−39.06)=410.94 kNH = 450.00 + (-39.06) = 410.94\ \text{kN}

Section D (x=30x = 30 m)

yD=30(90)180=15 m,tan⁡θD=120−60180=13,  θD=18.43∘M0=VA(30)=4500 kNm,V0=VA=150 kN\begin{aligned} y_D &= \frac{30(90)}{180} = 15\ \text{m},\qquad \tan\theta_D = \frac{120-60}{180} = \frac13,\ \ \theta_D = 18.43^\circ \\ M_0 &= V_A(30) = 4500\ \text{kNm},\qquad V_0 = V_A = 150\ \text{kN} \end{aligned}

Bending moment

MD=M0−HyD=4500−410.94(15)=−1664.06 kNmM_D = M_0 - Hy_D = 4500 - 410.94(15) = -1664.06\ \text{kNm}

(Due to the load alone: −2250.00-2250.00 kNm; the yield adds +585.94+585.94 kNm.)

Normal thrust

ND=Hcos⁡θ+V0sin⁡θ=410.94(0.9487)+150(0.3162)=437.28 kNN_D = H\cos\theta + V_0\sin\theta = 410.94(0.9487) + 150(0.3162) = 437.28\ \text{kN}

Radial shear

QD=V0cos⁡θ−Hsin⁡θ=150(0.9487)−410.94(0.3162)=12.35 kNQ_D = V_0\cos\theta - H\sin\theta = 150(0.9487) - 410.94(0.3162) = 12.35\ \text{kN}

Bending moment diagram M=M0−HyM = M_0 - Hy (kNm)

xx (m)yy (m)M0M_0MM
00.000.00.0
158.752250.0-1345.7
3015.004500.0-1664.1
4518.756750.0-955.1
6020.009000.0781.2
7518.7510125.02419.9
9015.009000.02835.9
1058.755625.02029.3
1200.000.00.0

The BMD is hogging for 0<x<54.30 < x < 54.3 m (largest hogging about −1683-1683 kNm near x=27x = 27 m) and sagging for the rest, with the largest sagging moment about 28522852 kNm near x=88x = 88 m, under the loaded half. It is zero at both hinges.

Answer: at D, M=−1664.06M = -1664.06 kNm (hogging), N=437.28N = 437.28 kN (compression), radial shear Q=12.35Q = 12.35 kN; H=410.94H = 410.94 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures II chapter 2 questions →