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Built-up beam, unsupported 4 m, 40 kN/m + 100 kN

Short answer

Use a built-up section: ISMB 300 with two 180 × 14 mm flange plates (total depth 328 mm). Lateral-torsional buckling capacity M_d = 202.9 kN·m > M_u = 182.5 kN·m; shear and deflection are safe.

Design a built up beam having laterally unsupported span of 4 m, support width 300 mm. Beam is subjected to design imposed load of 40 KN/m and 100 KN at mid span. Depth of beam is limited to 350 mm.

Data

  • Fe 410 (E250): fy=250f_y = 250 N/mm², fu=410f_u = 410 N/mm², E=2×105E = 2\times10^5 N/mm², γm0=1.10\gamma_{m0} = 1.10. Limit state design (IS 800:2007).
  • Effective span L=4.00L = 4.00 m, maximum overall depth 350 mm. A rolled I-section alone is not enough, so flange plates are added.

Loads and design forces

The imposed UDL of 40 kN/m and the 100 kN load at mid-span are the design (factored) loads. Span L=4L = 4 m, support width 300 mm (stiff bearing b1=300b_1 = 300 mm), depth limited to 350 mm. The beam is laterally unsupported over the full span, so LLT=4.0L_{LT} = 4.0 m (simple supports, torsion restrained, warping free).

Unfactored loads for deflection: 40/1.5=26.740/1.5 = 26.7 kN/m and 100/1.5=66.7100/1.5 = 66.7 kN.

Without self-weight M=180.0M = 180.0 kN·m, so even with full lateral support Zp≥Mγm0/fy=792Z_p \ge M\gamma_{m0}/f_y = 792 cm³. The deepest rolled section within the depth limit, ISMB 350 (Zp≈890Z_p \approx 890 cm³), would lose much of this capacity to lateral-torsional buckling over the unsupported 4 m span, so plates are added to both flanges to increase both ZpZ_p and the lateral stiffness IyI_y.

Trial section

Try ISMB 300 with two plates 180 × 14 mm (one on each flange). ISMB 300: D=300D = 300, bf=140b_f = 140, tw=7.7t_w = 7.7, tf=13.1t_f = 13.1, R1=14R_1 = 14 mm, Izz=8990I_{zz} = 8990 cm⁴, mass 46.0 kg/m. Overall depth =300+2×14=328= 300 + 2\times14 = 328 mm ≤350\le 350 mm.

yc=D/2+tp/2=157 mmIzz=8990×104+2[180×14312+180×14×1572]=21421 cm4Ze=Izz/(328/2)=1306 cm3Zp=Zp,ISMB+2(bptp)yc=670+791=1462 cm3\begin{aligned} y_c &= D/2 + t_p/2 = 157\ \text{mm} \\ I_{zz} &= 8990\times10^4 + 2\left[\frac{180\times14^3}{12} + 180\times14\times157^2\right] = 21421\ \text{cm}^4 \\ Z_e &= I_{zz}/(328/2) = 1306\ \text{cm}^3 \\ Z_p &= Z_{p,ISMB} + 2(b_pt_p)y_c = 670 + 791 = 1462\ \text{cm}^3 \end{aligned}

Mass of section =46.0+2×0.180×0.014×7850=85.6= 46.0 + 2\times0.180\times0.014\times7850 = 85.6 kg/m, self-weight =0.839= 0.839 kN/m (factored 1.259 kN/m). Total factored UDL w=40.00+1.26=41.26w = 40.00 + 1.26 = 41.26 kN/m.

Mu=wL28+WL4=41.26×4.0028+100.0×4.004=182.5 kN⋅mVu=132.5 kN\begin{aligned} M_u &= \frac{wL^2}{8} + \frac{WL}{4} = \frac{41.26\times4.00^2}{8} + \frac{100.0\times4.00}{4} = 182.5\ \text{kN·m} \\ V_u &= 132.5\ \text{kN} \end{aligned}

Section classification

ε=1\varepsilon = 1. Plate outstand (from the web face) b/t=(180−7.7)/2/14=6.15<9.4εb/t = (180 - 7.7)/2/14 = 6.15 < 9.4\varepsilon (plastic; plates continuously connected). ISMB flange b/tf=5.34b/t_f = 5.34, web d/tw=31.9<84d/t_w = 31.9 < 84. Plastic section, βb=1\beta_b = 1.

Moment capacity

The beam is laterally unsupported, so lateral-torsional buckling governs. LLT=4.0L_{LT} = 4.0 m. Properties of the built-up section: Iy=Iy,ISMB+2tpbp3/12=1847I_y = I_{y,ISMB} + 2t_pb_p^3/12 = 1847 cm⁴; It=58.1I_t = 58.1 cm⁴ (Σbt3/3\Sigma bt^3/3); distance between flange centroids hf=303h_f = 303 mm; Iw=Iyhf2/4=42×1010I_w = I_yh_f^2/4 = 42\times10^{10} mm⁶. Welded built-up section: αLT=0.49\alpha_{LT} = 0.49 (Table 13).

Mcr=π2EIyLLT2(GIt+π2EIwLLT2)=469.7 kN⋅mλLT=Zpfy/Mcr=0.882, ϕLT=1.056, χLT=0.611fbd=χLTfy/γm0=138.8 N/mm2Md=Zpfbd=202.9 kN⋅m\begin{aligned} M_{cr} &= \sqrt{\frac{\pi^2EI_y}{L_{LT}^2}\left(GI_t + \frac{\pi^2EI_w}{L_{LT}^2}\right)} = 469.7\ \text{kN·m} \\ \lambda_{LT} &= \sqrt{Z_pf_y/M_{cr}} = 0.882,\ \phi_{LT} = 1.056,\ \chi_{LT} = 0.611 \\ f_{bd} &= \chi_{LT}f_y/\gamma_{m0} = 138.8\ \text{N/mm}^2 \\ M_d &= Z_pf_{bd} = 202.9\ \text{kN·m} \end{aligned}

Shear capacity

Shear is taken by the web of the rolled section: Vd=Dtwfy/(3γm0)=300×7.7×250/(3×1.1×103)=303.1V_d = D t_wf_y/(\sqrt3\gamma_{m0}) = 300\times7.7\times250/(\sqrt3\times1.1\times10^3) = 303.1 kN; Vu=132.5V_u = 132.5 kN.

Vu<0.6Vd=181.9V_u < 0.6V_d = 181.9 kN, so the shear is low and the moment capacity is not reduced. Md=202.9M_d = 202.9 kN·m >Mu=182.5> M_u = 182.5 kN·m. Safe.

Deflection (limit span/300, Table 6)

δ=5wL4384EI+WL348EI=4.15 mm<L300=13.33 mm\delta = \frac{5wL^4}{384EI} + \frac{WL^3}{48EI} = 4.15\ \text{mm} < \frac{L}{300} = 13.33\ \text{mm}

(unfactored imposed loads w=26.7w = 26.7 kN/m, W=66.7W = 66.7 kN, Izz=21421I_{zz} = 21421 cm⁴). OK.

Web buckling and bearing at the support

b1=300b_1 = 300 mm, d=245.8d = 245.8 mm, n1=d/2=122.9n_1 = d/2 = 122.9 mm, λ=0.7d/(tw/12)=77.4\lambda = 0.7d/(t_w/\sqrt{12}) = 77.4, fcd=140.4f_{cd} = 140.4 N/mm² (curve c): Fcdw=(b1+n1)twfcd=457.1F_{cdw} = (b_1 + n_1)t_wf_{cd} = 457.1 kN. Bearing: n2=2.5(tf+R1)=67.8n_2 = 2.5(t_f + R_1) = 67.8 mm, Fw=(b1+n2)twfy/γm0=643.6F_w = (b_1 + n_2)t_wf_y/\gamma_{m0} = 643.6 kN. Both exceed R=132.5R = 132.5 kN. OK.

Connection of plates to the flanges (fillet welds)

Horizontal shear flow at the support:

q=VuApycIzz=132.5×103×2520×15721421×104=244.7 N/mmq = \frac{V_uA_py_c}{I_{zz}} = \frac{132.5\times10^3\times2520\times157}{21421\times10^4} = 244.7\ \text{N/mm}

Use a 6 mm fillet weld along each edge of each plate: fwd=fu/(3γmw)=410/(3×1.25)=189.4f_{wd} = f_u/(\sqrt3\gamma_{mw}) = 410/(\sqrt3\times1.25) = 189.4 N/mm², strength per weld =0.7×6×189.4=795= 0.7\times6\times189.4 = 795 N/mm, two welds =1591= 1591 N/mm >244.7> 244.7 N/mm. OK.

Final design

ISMB 300 with a 180 × 14 mm plate on each flange (overall depth 328 mm), plates connected by 6 mm fillet welds along both edges. Md=202.9M_d = 202.9 kN·m >182.5> 182.5 kN·m, δ=4.1\delta = 4.1 mm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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