NivaarExam PrepOfficial exam papers ↗

16-Civ-A2 Elementary Structural Design · May 2013

Question 5 of 7: B2 — Moment and Shear Resistances of a Triple-T Floor Section

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examinations, May 2013 — 98-Civ-A2 Elementary Structural Design, 3-hour duration, CLOSED BOOK (handbooks and textbooks permitted, no notes). Seven questions are printed: Part A (A1–A3, steel), Part B (B1–B3, reinforced concrete) and Part C (C1, timber). The candidate answers two from Part A, two from Part B and the one question in Part C — five solutions in total, all of equal value. All seven are solved here, because the set is a study resource. All loads shown on the figures are unfactored; NBCC load combination 1.25D + 1.5L is applied throughout. Solutions are to CSA-S16 (steel), CAN/CSA-A23.3 (concrete) and CSA-O86 (timber), as the paper directs.

Reference texts.

Check — assumptions carried through this paper. (1) The 60 kN, 50 kN, 40 kN, 200 kN, 250 kN and 300 kN forces on Figures A1–B3 are specified live loads, so a load factor of 1.5 is used; concrete self-weight is factored at 1.25. (2) Steel members are assumed continuously laterally supported unless an unbraced length is printed — no unbraced lengths appear on this paper. (3) In Figure B2 the "65 typical" dimension is taken as the distance from the tension face to the centroid of the bottom bars, and the 15M stirrups are assumed at 300 mm on centre in each stem (the figure gives no spacing). (4) CSA O86 Table 6.3.1B Beam-and-Stringer specified strengths for D.Fir-L No.1 are used in C1.

Question 5: B2 — Moment and Shear Resistances of a Triple-T Floor Section (12 + 8 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Flange 1 600 mm wide × 200 mm thick; overall depth 800 mm; three stems each 200 mm wide with 500 mm clear between them, so $3(200)+2(500) = 1\,600$ mm confirms the flange width. Bottom reinforcement 6–25M ($A_s = 3\,000$ mm²), top reinforcement 6–15M, 15M stirrups, "65 typical" to the bottom steel. $f_c' = 35$ MPa, $f_y = 400$ MPa.

Find. The factored moment resistance $M_R$ and shear resistance $V_R$ of the section.

6–25M (2 per stem) 6–15M 1600 800 200 500 500 200 200
Figure B2 — triple-T floor section: 1 600 × 200 mm flange over three 200 mm stems at 500 mm clear spacing, overall depth 800 mm.

Approach. Treat the section as a T-beam with the flange in compression: compute the depth of the stress block from the tension steel and confirm it falls inside the flange, so the section behaves as a rectangular beam of width 1 600 mm; then compute the shear resistance using the combined web width of the three stems.

  1. Effective depth and tension force. Taking the "65 typical" dimension as the distance from the tension face to the centroid of the bottom bars, $d = 800-65 = 735$ mm. The 6–25M bars give $$T_r=\phi_sA_sf_y=0.85(3\,000)(400)=1\,020\ \text{kN}$$
  2. Depth of the compression block. Equating $T_r$ to the compressive resultant over the full flange width, $$a=\frac{T_r}{\alpha_1\phi_cf_c'b_f}=\frac{1\,020\,000}{0.7975(0.65)(35)(1\,600)}=\frac{1\,020\,000}{29\,029}=35.1\ \text{mm}$$ Since $a = 35.1$ mm is much less than the 200 mm flange thickness, the compression zone lies wholly within the flange and the section is analysed as a rectangular beam 1 600 mm wide — the stems play no part in flexure.
  3. Confirm ductile, under-reinforced behaviour. The neutral axis depth is $c = a/\beta_1 = 35.1/0.8825 = 39.8$ mm, so $$\varepsilon_s=0.0035\,\frac{d-c}{c}=0.0035\,\frac{735-39.8}{39.8}=0.061$$ which is thirty times the yield strain of 0.002. The steel is deeply yielded, so the assumed stress $f_y$ is valid and the failure would be extremely ductile. Minimum reinforcement, $A_{s,min} = 0.2\sqrt{35}(600)(800)/400 = 1\,420$ mm², is also satisfied by the 3 000 mm² provided.
  4. Moment resistance. The lever arm between the steel and the flange compression resultant is $d - a/2$: $$M_R=T_r\left(d-\frac{a}{2}\right)=1\,020\left(0.735-\frac{0.0351}{2}\right)=1\,020(0.7174)$$ $$\boxed{M_R=732\ \text{kN}\cdot\text{m}}$$
  5. Effective shear depth and web width. All three stems resist shear together, so $b_w = 3(200) = 600$ mm, and $$d_v=\max(0.9d,\,0.72h)=\max(0.9\times735,\;0.72\times800)=\max(661.5,\;576)=661.5\ \text{mm}$$
  6. Concrete contribution. The stems carry 15M stirrups, so at least minimum transverse reinforcement is present and the simplified method gives $\beta = 0.18$, $\theta = 35^\circ$: $$V_c=\phi_c\lambda\beta\sqrt{f_c'}\,b_wd_v=0.65(1.0)(0.18)\sqrt{35}(600)(661.5)=275\ \text{kN}$$
  7. Stirrup contribution. With one 15M double-leg stirrup in each of the three stems, $A_v = 3(2)(200) = 1\,200$ mm², and taking the spacing as 300 mm on centre, $$V_s=\frac{\phi_sA_vf_yd_v\cot\theta}{s}=\frac{0.85(1\,200)(400)(661.5)(1.428)}{300}=1\,285\ \text{kN}$$
  8. Shear resistance and upper bound. Adding the two contributions, $$\boxed{V_R=V_c+V_s=275+1\,285=1\,560\ \text{kN}}$$ This must not exceed the crushing limit of the diagonal compression field, $V_{r,max} = 0.25\phi_cf_c'b_wd_v = 0.25(0.65)(35)(600)(661.5) = 2\,258$ kN, and it does not, so the calculated value stands. Note how lopsided the section is: it can resist 1 560 kN of shear but only 732 kN·m of moment, because the six 25M bars are the true bottleneck while the 600 mm of combined web is generous.

Check: the figure labels the stirrups "15M" but prints no spacing, and dimensions the bottom cover as "65 typical". The calculation above assumes 15M double-leg stirrups at 300 mm on centre in each stem and takes 65 mm to the centroid of the bottom steel. If 65 mm is clear cover instead, $d$ falls to about 711 mm and $M_R$ drops to roughly 708 kN·m; if the stirrups are at 400 mm, $V_R$ falls to about 1 240 kN. Both remain far above the crushing check.

QuantityValue
Flange / stems1 600 × 200 mm / 3 × 200 mm, $b_w$ = 600 mm
$d$ / $d_v$735 mm / 661.5 mm
$T_r$ / $a$ / $c$1 020 kN / 35.1 mm / 39.8 mm
Steel strain $\varepsilon_s$0.061 (yielded, ductile)
$M_R$732 kN·m
$V_c$ / $V_s$275 kN / 1 285 kN
$V_R$1 560 kN (limit 2 258 kN)