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Beam 6 m span with 100 kN secondary beam load

Short answer

ISMB 500. Factored moment 360 kN·m < lateral-torsional buckling capacity 375.3 kN·m (unrestrained length 3 m); shear 165 kN < 669.2 kN; deflection 8.71 mm < L/300 = 20 mm.

Design a simply supported beam having unsupported span of 6m, support width 250 mm. Beam is subjected to imposed load (including self-weight) 20 kN/m and 100 kN from secondary beam at mid-span of beam. Ends and mid of beam is laterally restrained.

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, bearing length of support =250= 250 mm.

Loads and design forces

The imposed load of 2020 kN/m (including self-weight) and the 100 kN load from the secondary beam are taken as service loads. Factored: wu=1.5×20=30w_u = 1.5\times20 = 30 kN/m, Wu=1.5×100=150W_u = 1.5\times100 = 150 kN. Self-weight is already included, so it is not added again. Span L=6L = 6 m, support width 250 mm.

The beam is laterally restrained at both ends and at mid-span, so the unrestrained length is LLT=3.0L_{LT} = 3.0 m (simply supported segment, torsionally restrained, warping free, K=1.0K = 1.0, Table 15). The two segments are identical, so one is checked using the maximum (mid-span) moment with no allowance for the moment gradient, which is conservative.

Design moment (self-weight included in the given load) M=360.0M = 360.0 kN·m, so Zp,req≈Mγm0/fy=360.0×106×1.1/250=1584Z_{p,req} \approx M\gamma_{m0}/f_y = 360.0\times10^6\times1.1/250 = 1584 cm³.

Trial section

Try ISMB 500 (IS 808): D=500D = 500 mm, bf=180b_f = 180 mm, tw=10.2t_w = 10.2 mm, tf=17.2t_f = 17.2 mm, R1=17R_1 = 17 mm; Izz=45200I_{zz} = 45200 cm⁴; Ze=1810Z_e = 1810 cm³; Zp≈Btf(D−tf)+tw(D−2tf)2/4=2048Z_p \approx B t_f (D - t_f) + t_w (D - 2t_f)^2/4 = 2048 cm³; mass 86.986.9 kg/m.

Mu=wL28+WL4=30.00×6.0028+150.0×6.004=360.0 kN⋅mVu=wL2+W2=165.0 kN\begin{aligned} M_u &= \frac{wL^2}{8} + \frac{WL}{4} = \frac{30.00\times6.00^2}{8} + \frac{150.0\times6.00}{4} = 360.0\ \text{kN·m} \\ V_u &= \frac{wL}{2} + \frac{W}{2} = 165.0\ \text{kN} \end{aligned}

Section classification (Table 2)

ε=250/fy=1.00\varepsilon = \sqrt{250/f_y} = 1.00. Flange: b/tf=(180/2)/17.2=5.23<9.4ε=9.4b/t_f = (180/2)/17.2 = 5.23 < 9.4\varepsilon = 9.4. Web: d/tw=42.3<84ε=84d/t_w = 42.3 < 84\varepsilon = 84 (with d=D−2(tf+R1)=431.6d = D - 2(t_f + R_1) = 431.6 mm). The section is plastic, so βb=1.0\beta_b = 1.0.

Moment capacity (cl. 8.2.2)

The compression flange is not continuously restrained, so lateral-torsional buckling governs (cl. 8.2.2). Effective length for LTB LLT=3.00L_{LT} = 3.00 m. Iy=1370I_y = 1370 cm⁴; It=(2bftf3+dtw3)/3=77.5I_t = (2b_ft_f^3 + d t_w^3)/3 = 77.5 cm⁴; Iw=Iyhf2/4=80×1010I_w = I_y h_f^2/4 = 80\times10^{10} mm⁶ (hf=D−tf=482.8h_f = D - t_f = 482.8 mm).

Mcr=π2EIyLLT2(GIt+π2EIwLLT2)=839.8 kN⋅mλLT=βbZpfyMcr=0.781ϕLT=0.5[1+0.21(λLT−0.2)+λLT2]=0.866χLT=1ϕLT+ϕLT2−λLT2=0.807fbd=χLTfy/γm0=183.3 N/mm2Md=βbZpfbd=375.3 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)} = 839.8\ \text{kN·m} \\ \lambda_{LT} &= \sqrt{\frac{\beta_b Z_p f_y}{M_{cr}}} = 0.781 \\ \phi_{LT} &= 0.5[1 + 0.21(\lambda_{LT} - 0.2) + \lambda_{LT}^2] = 0.866 \\ \chi_{LT} &= \frac{1}{\phi_{LT} + \sqrt{\phi_{LT}^2 - \lambda_{LT}^2}} = 0.807 \\ f_{bd} &= \chi_{LT} f_y/\gamma_{m0} = 183.3\ \text{N/mm}^2 \\ M_d &= \beta_b Z_p f_{bd} = 375.3\ \text{kN·m} \end{aligned} Md=375.3 kN⋅m>Mu=360.0 kN⋅mSafeM_d = 375.3\ \text{kN·m} > M_u = 360.0\ \text{kN·m}\quad \text{Safe}

Shear capacity (cl. 8.4)

Av=Dtw=500×10.2=5100 mm2Vd=Avfy3 γm0=5100×2503×1.1×103=669.2 kN\begin{aligned} A_v &= D t_w = 500\times10.2 = 5100\ \text{mm}^2 \\ V_d &= \frac{A_v f_y}{\sqrt3\,\gamma_{m0}} = \frac{5100\times250}{\sqrt3\times1.1\times10^3} = 669.2\ \text{kN} \end{aligned}

Vu=165.0V_u = 165.0 kN <Vd< V_d; also Vu<0.6Vd=401.5V_u < 0.6V_d = 401.5 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=42.3<67ε=67d/t_w = 42.3 < 67\varepsilon = 67 (cl. 8.4.2.1).

Deflection (Table 6)

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

δ=5wL4384EI+WL348EI=5×20.00×(6000)4384×2×105×45200×104+100000×(6000)348×2×105×45200×104=8.71 mm\delta = \frac{5 w L^4}{384 E I} + \frac{W L^3}{48 E I} = \frac{5\times20.00\times(6000)^4}{384\times2\times10^5\times45200\times10^4} + \frac{100000\times(6000)^3}{48\times2\times10^5\times45200\times10^4} = 8.71\ \text{mm}

δ=8.71\delta = 8.71 mm <L/300=20.00< L/300 = 20.00 mm. OK.

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

Stiff bearing length b1=250b_1 = 250 mm. Clear web depth d=431.6d = 431.6 mm; dispersion of load at 45° to mid-depth at an end support n1=d/2=215.8n_1 = d/2 = 215.8 mm. Effective length 0.7d0.7d (cl. 8.7.1.5), λ=0.7d/(tw/12)=102.6\lambda = 0.7d/(t_w/\sqrt{12}) = 102.6; curve c gives fcd=103.6f_{cd} = 103.6 N/mm².

Fcdw=(b1+n1)twfcd=(250+215.8)×10.2×103.6/103=492.3 kNn2=2.5(tf+R1)=85.5 mmFw=(b1+n2)twfyγm0=(250+85.5)×10.2×2501.1×103=777.7 kN\begin{aligned} F_{cdw} &= (b_1 + n_1) t_w f_{cd} = (250 + 215.8)\times10.2\times103.6/10^3 = 492.3\ \text{kN} \\ n_2 &= 2.5(t_f + R_1) = 85.5\ \text{mm} \\ F_w &= \frac{(b_1 + n_2) t_w f_y}{\gamma_{m0}} = \frac{(250 + 85.5)\times10.2\times250}{1.1\times10^3} = 777.7\ \text{kN} \end{aligned}

Support reaction R=165.0R = 165.0 kN <Fcdw< F_{cdw} and <Fw< F_w. No web stiffener is needed.

Final design

Provide ISMB 500 (86.9 kg/m): Md=375.3M_d = 375.3 kN·m >Mu=360.0> M_u = 360.0 kN·m, Vd=669V_d = 669 kN >Vu=165.0> V_u = 165.0 kN, δ=8.7\delta = 8.7 mm <20.0< 20.0 mm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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