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Beam deflection used for column buckling load

Short answer

EI from simply supported beam central deflection: EI = 800 × 5000³ / (48 × 30) = 6.944×10¹⁰ N·mm². As a column fixed at one end and hinged at the other, P_cr = 2π²EI/L² ≈ 54.8 kN.

A 5m long simply supported beam has 30mm maximum deflection due to 800N transverse load applied at the center of the beam. Determine the buckling load if the same beam of 5m length is used as a column with one end fixed and other end hinged.

Given: simply supported beam, L=5L = 5 m = 5000 mm, central load W=800W = 800 N, maximum (central) deflection δ=30\delta = 30 mm.

Step 1: find EIEI

For a simply supported beam with a central point load:

δ=WL348EI  ⇒  EI=WL348δ=800×5000348×30=6.944×1010 N mm2\delta = \frac{WL^3}{48EI} \;\Rightarrow\; EI = \frac{WL^3}{48\delta} = \frac{800\times5000^3}{48\times30} = 6.944\times10^{10}\ \text{N mm}^2

Step 2: buckling load as a column

For one end fixed and the other hinged, the effective length is Le=0.7LL_e = 0.7L, which corresponds to the standard textbook form Pcr=2π2EI/L2P_{cr} = 2\pi^2EI/L^2:

Pcr=2π2EIL2=2π2×6.944×101050002=54,831 NP_{cr} = \frac{2\pi^2EI}{L^2} = \frac{2\pi^2\times6.944\times10^{10}}{5000^2} = 54{,}831\ \text{N}

(Using the exact root of tan⁡kL=kL\tan kL = kL, that is Pcr=20.19EI/L2P_{cr} = 20.19EI/L^2, gives about 56 kN.)

Answer: buckling load ≈54.8\approx 54.8 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

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