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T-beam with overhang: max bending stress

Short answer

Maximum bending stress is 15.12 N/mm² (compressive) occurring at the bottom fibre over support B; the maximum tensile stress is 8.76 N/mm² at the top fibre over B.

Determine the maximum bending stress in the beam shown in figure below. [Figure: beam with a hinge at the left end and roller 6 m away, an overhang of 2 m beyond the roller; UDL 4 kN/m over the 6 m span; 10 kN downward load at the free end of the overhang. Cross-section: T-section with flange 10 + 10 + 10 = 30 cm wide and 10 cm thick, web 10 cm wide, stem total height 25 cm; all dimensions in cm.]

Assumption: flange 30 cm × 10 cm on top, web 10 cm wide, overall depth 25 cm (web depth 15 cm). Self-weight ignored.

   4 kN/m over A to B              10 kN
 vvvvvvvvvvvvvvvvvvvvvvvvvv          |
 |========================|==========v
 A (hinge)           B (roller)      C
 |<-------- 6 m --------->|<- 2 m -->|

Reactions

Taking moments about A:

RB×6=4×6×3+10×8⇒RB=25.33 kNR_B \times 6 = 4\times 6\times 3 + 10\times 8 \Rightarrow R_B = 25.33\ \text{kN}

RA=24+10−25.33=8.67R_A = 24 + 10 - 25.33 = 8.67 kN (check: ΣFy=0\Sigma F_y = 0).

Bending moments

  • At B (hogging): MB=−10×2=−20M_B = -10\times 2 = -20 kNm.
  • Zero shear at x=RA/4=2.167x = R_A/4 = 2.167 m from A, so the sagging moment is maximum there:
Mmax+=8.67×2.167−4×2.16722=9.39 kNmM_{max}^{+} = 8.67\times 2.167 - 4\times\frac{2.167^2}{2} = 9.39\ \text{kNm}

Section properties

Measure from the base (cm):

yˉ=30×10×20+10×15×7.5300+150=15.83 cm\bar y = \frac{30\times10\times20 + 10\times15\times7.5}{300+150} = 15.83\ \text{cm} I=30×10312+300(20−15.83)2+10×15312+150(7.5−15.83)2=20937.5 cm4I = \frac{30\times10^3}{12} + 300(20-15.83)^2 + \frac{10\times15^3}{12} + 150(7.5-15.83)^2 = 20937.5\ \text{cm}^4

Distance to top fibre =25−15.83=9.17= 25 - 15.83 = 9.17 cm; to bottom fibre =15.83= 15.83 cm.

Stresses (σ=My/I\sigma = My/I)

SectionTop fibreBottom fibre
Max sagging, 9.39 kNm4.11 N/mm² (C)7.10 N/mm² (T)
Support B, hogging 20 kNm8.76 N/mm² (T)15.12 N/mm² (C)
σ=20×106×158.320937.5×104=15.12 N/mm2\sigma = \frac{20\times10^6\times 158.3}{20937.5\times10^4} = 15.12\ \text{N/mm}^2

Answer: maximum bending stress = 15.12 N/mm² (compressive) at the bottom fibre over support B; the maximum tensile stress is 8.76 N/mm² at the top fibre over B.

✓ Answer checked by Claude Opus 5.5 (high effort)

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