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Intermediate beam for 18 m x 6 m office hall

Short answer

Use ISMB 400 (61.5 kg/m). Factored moment 202.3 kN·m, capacity 264.0 kN·m; shear 467 kN > 128 kN; deflection 8.3 mm < L/300 (21 mm). The groove-supported RC slab provides full lateral restraint to the compression flange.

A office hall of clear dimension 18 m × 6 m is provided with 12 cm thick RC slab over rolled steel beams 3 m c/c. A wearing coat of 2 cm thick lime concrete is provided over RC concrete slab. The compression flange would be supported throughout its length by providing grooves in slabs. Design an intermediate beam with the following data. Live load = 5.5 kN/m² Unit wt. of cement concrete = 25 kN/m³ Unit wt. of lime concrete = 18 kN/m³

Data

  • Steel 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 (IS 800:2007, Table 5). Limit state design.
  • Effective span L=6.30L = 6.30 m, bearing length of support =300= 300 mm.

Loads and design forces

The hall is 6 m wide (clear), so the beams span 6 m at 3 m c/c. The wall width is not given; assume 300 mm bearing, so effective span L=6+0.3=6.3L = 6 + 0.3 = 6.3 m.

ItemCalculationkN/m²kN/m (3 m width)
RC slab 120 mm0.12×250.12\times253.0009.00
Lime concrete 20 mm0.02×180.02\times180.3601.08
Live loadgiven5.50016.50

Dead load =10.08= 10.08 kN/m, live =16.50= 16.50 kN/m; wu=1.5(10.08+16.50)=39.87w_u = 1.5(10.08 + 16.50) = 39.87 kN/m plus self-weight. b1=300b_1 = 300 mm.

Moment without self-weight M=197.8M = 197.8 kN·m, so Zp,req≈Mγm0/fy=197.8×106×1.1/250=870Z_{p,req} \approx M\gamma_{m0}/f_y = 197.8\times10^6\times1.1/250 = 870 cm³ (self-weight adds a little).

Trial section

Try ISMB 400 (IS 808): D=400D = 400 mm, bf=140b_f = 140 mm, tw=8.9t_w = 8.9 mm, tf=16.0t_f = 16.0 mm, R1=14R_1 = 14 mm; Izz=20500I_{zz} = 20500 cm⁴; Ze=1020Z_e = 1020 cm³; Zp≈Btf(D−tf)+tw(D−2tf)2/4=1161Z_p \approx B t_f (D - t_f) + t_w (D - 2t_f)^2/4 = 1161 cm³; mass 61.561.5 kg/m.

Self-weight =61.5×9.81/1000=0.603= 61.5\times9.81/1000 = 0.603 kN/m, factored =1.5×0.603=0.905= 1.5\times0.603 = 0.905 kN/m. Total factored UDL w=39.87+0.90=40.77w = 39.87 + 0.90 = 40.77 kN/m.

Mu=wL28=40.77×6.3028=202.3 kN⋅mVu=wL2=128.4 kN\begin{aligned} M_u &= \frac{wL^2}{8} = \frac{40.77\times6.30^2}{8} = 202.3\ \text{kN·m} \\ V_u &= \frac{wL}{2} = 128.4\ \text{kN} \end{aligned}

Section classification (Table 2)

ε=250/fy=1.00\varepsilon = \sqrt{250/f_y} = 1.00. Flange: b/tf=(140/2)/16.0=4.38<9.4ε=9.4b/t_f = (140/2)/16.0 = 4.38 < 9.4\varepsilon = 9.4. Web: d/tw=38.2<84ε=84d/t_w = 38.2 < 84\varepsilon = 84 (with d=D−2(tf+R1)=340.0d = D - 2(t_f + R_1) = 340.0 mm). The section is plastic, so βb=1.0\beta_b = 1.0.

Moment capacity (cl. 8.2.1.2)

The compression flange is supported throughout its length by the grooves in the slab, so lateral buckling is prevented.

Md=βbZpfyγm0=1161×103×2501.1×106=264.0 kN⋅m1.2Zefy/γm0=1.2×1020×103×250/(1.1×106)=278.2 kN⋅m\begin{aligned} M_d &= \frac{\beta_b Z_p f_y}{\gamma_{m0}} = \frac{1161\times10^3\times250}{1.1\times10^6} = 264.0\ \text{kN·m} \\ 1.2 Z_e f_y/\gamma_{m0} &= 1.2\times1020\times10^3\times250/(1.1\times10^6) = 278.2\ \text{kN·m} \end{aligned}

The smaller value governs: Md=264.0M_d = 264.0 kN·m.

Md=264.0 kN⋅m>Mu=202.3 kN⋅mSafeM_d = 264.0\ \text{kN·m} > M_u = 202.3\ \text{kN·m}\quad \text{Safe}

Shear capacity (cl. 8.4)

Av=Dtw=400×8.9=3560 mm2Vd=Avfy3 γm0=3560×2503×1.1×103=467.1 kN\begin{aligned} A_v &= D t_w = 400\times8.9 = 3560\ \text{mm}^2 \\ V_d &= \frac{A_v f_y}{\sqrt3\,\gamma_{m0}} = \frac{3560\times250}{\sqrt3\times1.1\times10^3} = 467.1\ \text{kN} \end{aligned}

Vu=128.4V_u = 128.4 kN <Vd< V_d; also Vu<0.6Vd=280.3V_u < 0.6V_d = 280.3 kN, so the shear is low and the moment capacity is not reduced (cl. 9.2.1). Web shear buckling does not govern since d/tw=38.2<67ε=67d/t_w = 38.2 < 67\varepsilon = 67 (cl. 8.4.2.1).

Deflection (Table 6)

Deflection under unfactored service (imposed) loads, limit span/300 (floor and roof members, Table 6):

δ=5wL4384EI=5×16.50×(6300)4384×2×105×20500×104=8.25 mm\delta = \frac{5 w L^4}{384 E I} = \frac{5\times16.50\times(6300)^4}{384\times2\times10^5\times20500\times10^4} = 8.25\ \text{mm}

δ=8.25\delta = 8.25 mm <L/300=21.00< L/300 = 21.00 mm. OK.

Web buckling and bearing at support (cl. 8.7.3 and 8.7.4)

Stiff bearing length b1=300b_1 = 300 mm. Clear web depth d=340.0d = 340.0 mm; dispersion of load at 45° to mid-depth at an end support n1=d/2=170.0n_1 = d/2 = 170.0 mm. Effective length 0.7d0.7d (cl. 8.7.1.5), λ=0.7d/(tw/12)=92.6\lambda = 0.7d/(t_w/\sqrt{12}) = 92.6; curve c gives fcd=117.2f_{cd} = 117.2 N/mm².

Fcdw=(b1+n1)twfcd=(300+170.0)×8.9×117.2/103=490.2 kNn2=2.5(tf+R1)=75.0 mmFw=(b1+n2)twfyγm0=(300+75.0)×8.9×2501.1×103=758.5 kN\begin{aligned} F_{cdw} &= (b_1 + n_1) t_w f_{cd} = (300 + 170.0)\times8.9\times117.2/10^3 = 490.2\ \text{kN} \\ n_2 &= 2.5(t_f + R_1) = 75.0\ \text{mm} \\ F_w &= \frac{(b_1 + n_2) t_w f_y}{\gamma_{m0}} = \frac{(300 + 75.0)\times8.9\times250}{1.1\times10^3} = 758.5\ \text{kN} \end{aligned}

Support reaction R=128.4R = 128.4 kN <Fcdw< F_{cdw} and <Fw< F_w. No web stiffener is needed.

Final design

Provide ISMB 400 (61.5 kg/m): Md=264.0M_d = 264.0 kN·m >Mu=202.3> M_u = 202.3 kN·m, Vd=467V_d = 467 kN >Vu=128.4> V_u = 128.4 kN, δ=8.3\delta = 8.3 mm <21.0< 21.0 mm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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