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Compatibility equation for two-hinged arch

Short answer

The compatibility equation for a two-hinged parabolic arch is H = (∫(M0 y)/EI ds + αtL – δ) / (∫ y²/EI ds + ∫ cos²θ/AE ds), where the numerator includes external load, temperature, and support yield effects, and the denominator includes bending and rib shortening contributions.

Write down the compatibility equation for a two hinged parabolic arch due to external loads, variation in temperature, rib shortening and yielding of supports.

A two-hinged arch is indeterminate to the first degree. Take the horizontal thrust HH as the redundant, release the hinge at B (roller), and write that the net horizontal movement of B is equal to the yield of the support.

          C
       .-----.
     /         \
   A o           o B  <-- H (redundant)
   |<----- L ----->|

Displacement of B in the released structure (outward positive)

  1. External loads: Δ10=∫M0 yEI ds\Delta_{10} = \displaystyle\int \frac{M_0\,y}{EI}\,ds (M0M_0 = BM of the equivalent simple beam, yy = ordinate of the arch axis). The axial-force term is small and is usually neglected.
  2. Temperature rise tt: Δ1t=α t L\Delta_{1t} = \alpha\,t\,L (a fall in temperature gives a negative value).
  3. Redundant HH (unit horizontal force at B gives m=−ym = -y and N=−cos⁡θN = -\cos\theta):
Δ1H=−H f11,f11=∫y2EI ds+∫cos⁡2θAE ds\Delta_{1H} = -H\,f_{11}, \qquad f_{11} = \int \frac{y^2}{EI}\,ds + \int \frac{\cos^2\theta}{AE}\,ds

The first term of f11f_{11} is bending, and the second is the rib shortening due to the axial thrust Hcos⁡θH\cos\theta.

  1. Yielding of support: B moves outward by δ\delta (positive outward).

Compatibility equation

The final horizontal movement of B must equal the support yield δ\delta:

Δ10+α t L−H f11=δ\Delta_{10} + \alpha\,t\,L - H\,f_{11} = \delta H=∫M0 yEI ds+α t L−δ∫y2EI ds+∫cos⁡2θAE ds\boxed{H = \frac{\displaystyle\int \frac{M_0\,y}{EI}\,ds + \alpha\,t\,L - \delta}{\displaystyle\int \frac{y^2}{EI}\,ds + \int \frac{\cos^2\theta}{AE}\,ds}}

Remarks

  • For I=Icsec⁡θI = I_c\sec\theta the bending integrals become 1EIc∫M0 y dx\dfrac{1}{EI_c}\int M_0\,y\,dx and 1EIc∫y2 dx\dfrac{1}{EI_c}\int y^2\,dx, and with A=Acsec⁡θA = A_c\sec\theta the rib shortening term is 1EAc∫cos⁡2θ dx\dfrac{1}{EA_c}\int\cos^2\theta\,dx.
  • A temperature rise or an inward movement of B increases HH. An outward yield and rib shortening reduce HH (rib shortening acts like an elastic spring in the denominator).
  • After HH is found, the moment at any section is M=M0−HyM = M_0 - Hy, the normal thrust is N=Hcos⁡θ+V0sin⁡θN = H\cos\theta + V_0\sin\theta and the radial shear is Vr=V0cos⁡θ−Hsin⁡θV_r = V_0\cos\theta - H\sin\theta.

✓ Answer checked by Claude Opus 5.5 (high effort)

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