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Cantilever 5 m: maximum and 25 mm bending stress

Short answer

Max hogging moment 175 kNm. Neutral axis 56.875 mm from base. Maximum bending stress 544.2 N/mm² (tension, top). Stress 25 mm below top surface = 423.9 N/mm² (tension).

A cantilever beam 5m in length is subjected to the loads as shown in figure. Determine the maximum bending stresses in the beam. Also, determine the value of bending stress 25 mm below from the top surface of the beam. [Figure: cantilever fixed at A, length 5 m, carrying an 8 kN/m UDL over its length and a 15 kN point load at the free end B; cross-section: rectangular web 50 mm wide and 120 mm high standing on a flange 200 mm wide and 50 mm thick (T-section).]

Section (as drawn): web 50 mm wide × 120 mm high standing on a flange 200 mm × 50 mm. So the flange is at the bottom, the web top is the top surface, and overall depth is 170 mm.

 8 kN/m                   15 kN
 vvvvvvvvvvvvvvvvvvvvvvv   v
 |#########################
 A            5 m          B

Maximum bending moment (at fixed end A, hogging)

Mmax=8×522+15×5=100+75=175 kNmM_{max} = \frac{8\times5^2}{2} + 15\times5 = 100 + 75 = 175\ \text{kNm}

Top fibres are in tension, bottom fibres in compression.

Section properties (from base, mm)

yˉ=200×50×25+50×120×11010000+6000=56.875 mm\bar y = \frac{200\times50\times25 + 50\times120\times110}{10000+6000} = 56.875\ \text{mm} I=200×50312+10000(25−56.875)2+50×120312+6000(110−56.875)2=36.377×106 mm4I = \frac{200\times50^3}{12} + 10000(25-56.875)^2 + \frac{50\times120^3}{12} + 6000(110-56.875)^2 = 36.377\times10^6\ \text{mm}^4

Distance to top =170−56.875=113.125= 170 - 56.875 = 113.125 mm; to bottom =56.875= 56.875 mm.

Maximum stresses

σtop=175×106×113.12536.377×106=544.2 N/mm2 (T)\sigma_{top} = \frac{175\times10^6\times113.125}{36.377\times10^6} = 544.2\ \text{N/mm}^2\ \text{(T)} σbottom=175×106×56.87536.377×106=273.6 N/mm2 (C)\sigma_{bottom} = \frac{175\times10^6\times56.875}{36.377\times10^6} = 273.6\ \text{N/mm}^2\ \text{(C)}

Stress 25 mm below the top surface

y=113.125−25=88.125y = 113.125 - 25 = 88.125 mm above the NA (tension):

σ=175×106×88.12536.377×106=423.9 N/mm2 (T)\sigma = \frac{175\times10^6\times88.125}{36.377\times10^6} = 423.9\ \text{N/mm}^2\ \text{(T)}

Answer: maximum bending stress = 544.2 N/mm² (tension, top) at the fixed end; stress 25 mm below top = 423.9 N/mm² (tension). These stresses are far above the yield stress of mild steel (about 250 MPa), so the section as given is not adequate for these loads.

✓ Answer checked by Claude Opus 5.5 (high effort)

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