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Beam supporting RCC slab, DL 10 kN/m, IL 30 kN

Short answer

ISMB 450. Factored moment 274.8 kN·m < capacity 348.7 kN·m; shear 183.2 kN < 555 kN; deflection 8.33 mm < 20 mm. Lateral buckling is prevented by the continuous slab restraint.

A simply supported beam of span 6 m supports a reinforcement concrete slab. The compression flange of the beam is restrained due to its connection with the slab. The beam is subjected to a dead load of 10 kN/m and imposed load of 30 kN. Design the beam. Assume the beam is sufficiently stiff against bearing.

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=6.00L = 6.00 m.

Loads and design forces

Span L=6L = 6 m. The "30 kN" imposed load is read as 30 kN/m (a UDL, like the dead load of 10 kN/m); dead load is taken to exclude the beam's own weight. Factored load wu=1.5(10+30)=60w_u = 1.5(10 + 30) = 60 kN/m, plus factored self-weight. The beam is "sufficiently stiff against bearing", so the web buckling and bearing checks are not required.

Moment without self-weight M=270.0M = 270.0 kN·m, so Zp,req≈Mγm0/fy=270.0×106×1.1/250=1188Z_{p,req} \approx M\gamma_{m0}/f_y = 270.0\times10^6\times1.1/250 = 1188 cm³ (self-weight adds a little).

Trial section

Try ISMB 450 (IS 808): D=450D = 450 mm, bf=150b_f = 150 mm, tw=9.4t_w = 9.4 mm, tf=17.4t_f = 17.4 mm, R1=15R_1 = 15 mm; Izz=30400I_{zz} = 30400 cm⁴; Ze=1350Z_e = 1350 cm³; Zp≈Btf(D−tf)+tw(D−2tf)2/4=1534Z_p \approx B t_f (D - t_f) + t_w (D - 2t_f)^2/4 = 1534 cm³; mass 72.472.4 kg/m.

Self-weight =72.4×9.81/1000=0.710= 72.4\times9.81/1000 = 0.710 kN/m, factored =1.5×0.710=1.065= 1.5\times0.710 = 1.065 kN/m. Total factored UDL w=60.00+1.07=61.07w = 60.00 + 1.07 = 61.07 kN/m.

Mu=wL28=61.07×6.0028=274.8 kN⋅mVu=wL2=183.2 kN\begin{aligned} M_u &= \frac{wL^2}{8} = \frac{61.07\times6.00^2}{8} = 274.8\ \text{kN·m} \\ V_u &= \frac{wL}{2} = 183.2\ \text{kN} \end{aligned}

Section classification (Table 2)

ε=250/fy=1.00\varepsilon = \sqrt{250/f_y} = 1.00. Flange: b/tf=(150/2)/17.4=4.31<9.4ε=9.4b/t_f = (150/2)/17.4 = 4.31 < 9.4\varepsilon = 9.4. Web: d/tw=41.0<84ε=84d/t_w = 41.0 < 84\varepsilon = 84 (with d=D−2(tf+R1)=385.2d = D - 2(t_f + R_1) = 385.2 mm). The section is plastic, so βb=1.0\beta_b = 1.0.

Moment capacity (cl. 8.2.1.2)

The compression flange is restrained by the RCC slab along its full length, so lateral-torsional buckling is prevented.

Md=βbZpfyγm0=1534×103×2501.1×106=348.7 kN⋅m1.2Zefy/γm0=1.2×1350×103×250/(1.1×106)=368.2 kN⋅m\begin{aligned} M_d &= \frac{\beta_b Z_p f_y}{\gamma_{m0}} = \frac{1534\times10^3\times250}{1.1\times10^6} = 348.7\ \text{kN·m} \\ 1.2 Z_e f_y/\gamma_{m0} &= 1.2\times1350\times10^3\times250/(1.1\times10^6) = 368.2\ \text{kN·m} \end{aligned}

The smaller value governs: Md=348.7M_d = 348.7 kN·m.

Md=348.7 kN⋅m>Mu=274.8 kN⋅mSafeM_d = 348.7\ \text{kN·m} > M_u = 274.8\ \text{kN·m}\quad \text{Safe}

Shear capacity (cl. 8.4)

Av=Dtw=450×9.4=4230 mm2Vd=Avfy3 γm0=4230×2503×1.1×103=555.0 kN\begin{aligned} A_v &= D t_w = 450\times9.4 = 4230\ \text{mm}^2 \\ V_d &= \frac{A_v f_y}{\sqrt3\,\gamma_{m0}} = \frac{4230\times250}{\sqrt3\times1.1\times10^3} = 555.0\ \text{kN} \end{aligned}

Vu=183.2V_u = 183.2 kN <Vd< V_d; also Vu<0.6Vd=333.0V_u < 0.6V_d = 333.0 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=41.0<67ε=67d/t_w = 41.0 < 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=5×30.00×(6000)4384×2×105×30400×104=8.33 mm\delta = \frac{5 w L^4}{384 E I} = \frac{5\times30.00\times(6000)^4}{384\times2\times10^5\times30400\times10^4} = 8.33\ \text{mm}

δ=8.33\delta = 8.33 mm <L/300=20.00< L/300 = 20.00 mm. OK.

Web bearing/buckling at supports is not checked because the question states the beam is sufficiently stiff against bearing.

Final design

Provide ISMB 450 (72.4 kg/m): Md=348.7M_d = 348.7 kN·m >Mu=274.8> M_u = 274.8 kN·m, Vd=555V_d = 555 kN >Vu=183.2> V_u = 183.2 kN, δ=8.3\delta = 8.3 mm <20.0< 20.0 mm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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