Skip to main content

Frame horizontal deflection at E

Short answer

Horizontal deflection at E is 921.7/EI to the right. Virtual work with a unit horizontal load at E gives ∫M m/EI = 921.7/EI kNm³.

Determine horizontal deflection at E of the frame shown in figure below. [Figure: frame; left column A-B-C with A (hinge) at the bottom, B 3 m above A, C 3 m above B; 10 kN horizontal load at B; top beam CD of 4 m (2EI) with 20 kN/m UDL; right column D-E of 4 m (EI) with E roller; left column EI; width 4 m.]

Given data

Frame: A(0,0) hinge, B(0,3), C(0,6), D(4,6), E(4,2) roller. Left column AC: EIEI (3 m + 3 m); beam CD: 2EI2EI, 4 m, UDL 20 kN/m; right column DE: EIEI, 4 m. 10 kN horizontal at B (to the right). Required: horizontal deflection of E.

Real loading: reactions

∑MA=0:  Ey×4=10×3+80×2⇒Ey=47.5 kN,Ay=80−47.5=32.5 kN,Ax=10 kN (left)\sum M_A = 0:\; E_y\times4 = 10\times3 + 80\times2 \Rightarrow E_y = 47.5\ \text{kN},\quad A_y = 80 - 47.5 = 32.5\ \text{kN},\quad A_x = 10\ \text{kN (left)}

(The 10 kN load gives 30 kNm clockwise about A, the UDL resultant 80 kN at x=2x = 2 m gives 160 kNm.)

Virtual load: unit horizontal load at E (to the right)

Ax=1A_x = 1 (left); moments about A: Ey×4=1×2E_y\times4 = 1\times2, so Ey=0.5E_y = 0.5 (up), Ay=0.5A_y = 0.5 (down).

Moments and integrals (ss from the start of each member, A-B-C-D-E)

Memberss (m)stiffnessMM (kNm)mm∫Mm ds\int Mm\,ds / stiffness
AB0-3EIEI10s10sss90.00
BC0-3EIEI30s+3s + 3405.00
CD0-42EI2EI30+32.5s−10s230 + 32.5s - 10s^26−s/26 - s/2426.67
DE0-4EIEI04−s4 - s0
ΔEh=90+405+426.67EI=921.67EI\Delta_{Eh} = \frac{90 + 405 + 426.67}{EI} = \frac{921.67}{EI}

Answer: horizontal deflection of E =921.7/EI= 921.7/EI (kNm3^3/EI), to the right.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures I chapter 3 questions →