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BMD of portal frame with support settlement

Short answer

Settlement of a support in a statically indeterminate frame induces bending moments. The primary structure has zero M0; flexibility equations equate redundant displacements to settlement. The resulting M is linear between joints, proportional to EIδ/L^2, with moments on the tension side.

Explain with example how the bending moment diagram is drawn for a statically indeterminate portal frame which undergoes settlement of one support.

Settlement of a support in an indeterminate frame produces bending moments even without any external load, because the frame is forced to fit the new support position. The BMD is drawn from the redundant reactions caused by the settlement.

Procedure

  1. Find DsD_s and choose the redundants (for example the reactions of the settling support). Remove them to get the primary structure.
  2. The primary structure moves as a rigid body when the support settles, so M0=0M_0 = 0 and Δi0=0\Delta_{i0} = 0.
  3. Find the flexibility coefficients fijf_{ij} from unit-load moment diagrams mim_i.
  4. Write compatibility: the displacement at each redundant must equal the prescribed settlement δi\delta_i (measured positive in the direction of XiX_i): ∑jfijXj=δi\sum_j f_{ij}X_j = \delta_i.
  5. Solve for XjX_j and compute M=∑XjmjM = \sum X_j m_j. Since there are no member loads, the BM varies linearly between the joints, so the BMD is a set of straight lines joining the joint moments. Draw each ordinate on the tension side.

Note that the moments are proportional to EI δ/L2EI\,\delta/L^2, so a stiffer frame develops larger moments for the same settlement.

Example

Portal frame ABCD, h=L=4h = L = 4 m, EI=20000EI = 20000 kNm2^2 constant, A fixed, D hinged. D settles vertically by δ=10\delta = 10 mm.

Redundants: X1X_1 = HDH_D (→\rightarrow), X2X_2 = VDV_D (↑\uparrow). The unit moment diagrams are: m1m_1 = 0 at A rising to 4 at B, 4 along BC, falling to 0 at D; m2m_2 = 4 along AB, falling from 4 at B to 0 at C.

f11=106.67EI,f12=64EI,f22=85.33EIf_{11} = \frac{106.67}{EI},\quad f_{12} = \frac{64}{EI},\quad f_{22} = \frac{85.33}{EI} 106.67X1+64X2=064X1+85.33X2=−0.01×20000=−200\begin{aligned} 106.67X_1 + 64X_2 &= 0 \\ 64X_1 + 85.33X_2 &= -0.01\times20000 = -200 \end{aligned} X1=HD=2.56 kN (→),X2=VD=4.26 kN (downward, since D is pulled down)X_1 = H_D = 2.56\ \text{kN}\ (\rightarrow),\qquad X_2 = V_D = 4.26\ \text{kN}\ (\text{downward, since D is pulled down})

Bending moments (kNm; + tension on the inner face)

PointBM
A-17.05
B-6.82
C10.23
D0

BM is linear in every member; it is hogging (outer tension) in the left column and at B, and sagging at C (inner tension).

✓ Answer checked by Claude Opus 5.5 (high effort)

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