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Cantilever 3 m: bending stress 25 mm below top

Short answer

Maximum hogging moment 82.5 kNm. NA is 11.31 cm from base. At 25 mm below top (31.9 mm above NA) bending stress = 72.3 N/mm² tensile.

A cantilever beam 3m in length is subjected to load as shown below. Determine maximum bending stress at 25mm below from the top surface of the beam. [Figure: cantilever AB fixed at A, length 3 m, with 5 kN/m UDL over the span and a 20 kN point load at B; T-section, flange 20 cm wide, web 5 cm, stem 12 cm and flange depth 5 cm as marked.]

Section: flange 20 cm × 5 cm on top, stem 5 cm × 12 cm below; overall depth 17 cm.

Maximum bending moment (at fixed end A, hogging)

M=5×322+20×3=22.5+60=82.5 kNmM = \frac{5\times3^2}{2} + 20\times3 = 22.5 + 60 = 82.5\ \text{kNm}

Top fibres are in tension.

Neutral axis (from base, cm)

yˉ=20×5×14.5+5×12×6100+60=1450+360160=11.31 cm\bar y = \frac{20\times5\times14.5 + 5\times12\times6}{100+60} = \frac{1450+360}{160} = 11.31\ \text{cm}

Moment of inertia

I=20×5312+100(14.5−11.31)2+5×12312+60(6−11.31)2=3637.7 cm4=3.638×107 mm4I = \frac{20\times5^3}{12} + 100(14.5-11.31)^2 + \frac{5\times12^3}{12} + 60(6-11.31)^2 = 3637.7\ \text{cm}^4 = 3.638\times10^7\ \text{mm}^4

Stress 25 mm below the top

Top fibre is 17−11.31=5.6917 - 11.31 = 5.69 cm =56.9= 56.9 mm above the NA. The point 25 mm below the top is y=56.9−25=31.9y = 56.9 - 25 = 31.9 mm above the NA (tension).

σ=MyI=82.5×106×31.93.638×107=72.3 N/mm2 (T)\sigma = \frac{My}{I} = \frac{82.5\times10^6\times 31.9}{3.638\times10^7} = 72.3\ \text{N/mm}^2\ \text{(T)}

For reference, the extreme fibres are 129.0 N/mm² (top, tension) and 256.6 N/mm² (bottom, compression).

Answer: bending stress at 25 mm below the top = 72.3 N/mm² (tensile).

✓ Answer checked by Claude Opus 5.5 (high effort)

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