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Beam reactions and mid-span deflection (2EI)

Short answer

Use two beam elements with EI=1000 kN m^2, fixed and two roller supports, including equivalent nodal loads for the 25 kN point load and 15 kN/m UDL. Solving gives reactions R1=9.57 kN up, M1=11.44 kN m counter-clockwise, R2=56.83 kN up, R3=33.61 kN up. Mid-span deflections are 2.22 mm downward in span 1 and 91.65 mm downward in span 2.

Determine support reactions and deflections at mid span for the given structure. E=2×105E = 2\times10^5 MPa, I=5×106I = 5\times10^6 mm4^4.

[Figure: beam fixed at the left end; 25 kN point load 3 m from the fixed end; EIEI span of 7 m (from the fixed end) to an intermediate support carrying an applied moment of 25 kNm; EIEI span of 5 m with 15 kN/m UDL to a roller support at the right end]

Data: EI=2×105 MPa×5×106 mm4=1012EI=2\times10^5\ \text{MPa}\times5\times10^6\ \text{mm}^4=10^{12} N mm2=1000^2=1000 kN m2^2 (same for both spans). Nodes: 1 = fixed end (x = 0); 2 = intermediate support (x = 7 m) with an applied moment of 25 kN m (taken clockwise); 3 = right roller (x = 12 m). Span 1: L=7L=7 m with 25 kN at 3 m from the fixed end; span 2: L=5L=5 m with 15 kN/m UDL. Units: kN, m.

Element stiffness

[k]=EIL3[126L−126L6L4L2−6L2L2−12−6L12−6L6L2L2−6L4L2],{d}={vi,θi,vj,θj}T[k]=\frac{EI}{L^3}\begin{bmatrix}12&6L&-12&6L\\6L&4L^2&-6L&2L^2\\-12&-6L&12&-6L\\6L&2L^2&-6L&4L^2\end{bmatrix},\quad \{d\}=\{v_i,\theta_i,v_j,\theta_j\}^T

(Upward forces and displacements, and counter-clockwise moments and rotations, are positive.)

Equivalent nodal loads

Span 1 (a=3a=3, b=4b=4, L=7L=7): Pb2(3a+b)L3=25×16×13343=15.16\dfrac{Pb^2(3a+b)}{L^3}=\dfrac{25\times16\times13}{343}=15.16 kN, Pab2L2=24.49\dfrac{Pab^2}{L^2}=24.49 kN m, Pa2(a+3b)L3=9.84\dfrac{Pa^2(a+3b)}{L^3}=9.84 kN, Pa2bL2=18.37\dfrac{Pa^2b}{L^2}=18.37 kN m. Span 2: wL/2=37.5wL/2=37.5 kN, wL2/12=31.25wL^2/12=31.25 kN m. Equivalent loads are the negatives of the fixed-end forces. The applied clockwise moment gives −25-25 kN m at θ2\theta_2 (counter-clockwise positive).

Assembled equation

Boundary conditions: v1=θ1=0v_1=\theta_1=0, v2=0v_2=0, v3=0v_3=0. Free DOFs: θ2,θ3\theta_2,\theta_3.

[1371.429400.000400.000800.000]{θ2θ3}={−37.88331.250}\begin{bmatrix}1371.429 & 400.000 \\ 400.000 & 800.000\end{bmatrix}\begin{Bmatrix}\theta_2\\\theta_3\end{Bmatrix}=\begin{Bmatrix}-37.883 \\ 31.250\end{Bmatrix} θ2=−0.04568 rad,θ3=0.06190 rad\theta_2=-0.04568\ \text{rad},\qquad \theta_3=0.06190\ \text{rad}

Support reactions {f}=[k]{d}−{Feq}\{f\}=[k]\{d\}-\{F_{eq}\}

ElementViV_iMiM_iVjV_jMjM_j
1-29.56711.43915.433-44.469
2-341.39419.46933.606-0.000
  • Fixed end: R1=9.567R_1=9.567 kN (up), M1=11.439M_1=11.439 kN m (counter-clockwise)
  • Intermediate support: R2=56.827R_2=56.827 kN (up)
  • Right roller: R3=33.606R_3=33.606 kN (up)
  • Check: ΣR=100.000\Sigma R=100.000 kN =25+15×5=100=25+15\times5=100 kN.

Deflection at mid span

The displacement within a span is the Hermite interpolation of the nodal values plus the fixed-end beam deflection due to the load. Evaluating (checked by refining the mesh with nodes at the mid-points):

  • Mid of span 1 (x = 3.5 m): v=−2.22v=-2.22 mm (downward)
  • Mid of span 2 (x = 9.5 m): v=−91.65v=-91.65 mm (downward)

The value is large because EI=1000EI=1000 kN m2^2 is small for these spans.

Answer: R1=9.57R_1=9.57 kN, M1=11.44M_1=11.44 kN m, R2=56.83R_2=56.83 kN, R3=33.61R_3=33.61 kN; mid-span deflections 2.222.22 mm (span 1) and 91.6591.65 mm (span 2), both downward.

✓ Answer checked by Claude Opus 5.5 (high effort)

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