16-Civ-B2 Advanced Structural Design · December 2015
Question 6 of 7: Reinforced Concrete Design of the Continuous Girder
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 98-Civ-B2 Advanced Structural Design, National Exams December 2015 — 3 hours, closed book (textbooks and design handbooks permitted). Seven design questions of equal value; any five constitute a complete paper. All seven are solved here. Page 1 carries the design data and the mark split; pages 2–3 the question text.
Reference texts. CSA S16:19 Design of Steel Structures; CISC Handbook of Steel Construction, 12th ed.; CSA A23.3:19 Design of Concrete Structures; Collins & Mitchell, Prestressed Concrete Structures; Kulak & Grondin, Limit States Design in Structural Steel, 10th ed.; MacGregor & Bartlett, Reinforced Concrete: Mechanics and Design (Canadian ed.); Hibbeler, Structural Analysis, 10th ed. (plastic analysis, Ch. 18).
Check — load factors. Page 1 states only that “all loads shown are unfactored” and gives no dead/live split. Throughout this paper a single factor of 1.5 is applied to every load printed on Figures 1–4, and 1.25 to any self weight the solver introduces (girder, slab, concrete member). Collapse mechanisms, section classifications and interaction ratios are unaffected by that choice; only the magnitudes scale. A candidate who assumes 1.25D + 1.5L with a stated split will land within a few per cent of the numbers below.
Check — section properties. Every rolled W-shape is modelled from its nominal plate dimensions (d, bf, tf, w), ignoring the root fillets. This is conservative by roughly 2 % of area and keeps every quoted property reproducible without a handbook.
Question 6: Reinforced Concrete Design of the Continuous Girder (10 + 5 + 5 marks)
Given. The Figure 1 girder again: two 8 m spans, built in at A and C, propped at B, with 500 kN unfactored at 4 m and 12 m. Concrete $f'_c = 30$ MPa, rebar $f_y = 400$ MPa, $\phi_c = 0.65$, $\phi_s = 0.85$. Stress-block factors $\alpha_1 = 0.85 - 0.0015f'_c = 0.805$ and $\beta_1 = 0.97 - 0.0025f'_c = 0.895$.
Find. A rectangular section, the flexural steel at every critical section, the shear reinforcement, and a bar layout.
Approach. Re-use the elastic analysis of Question 1 with the concrete self weight added, size the section for the hogging moment, then design the stirrups by the CSA A23.3 simplified method and set out the bars.
Adopt a section and recompute the actions. Try 400 mm × 900 mm ($w_{sw} = 8.64$ kN/m, factored 10.80 kN/m). Symmetry again makes each 8 m span fixed-ended, so the point load contributes $PL/8 = 750$ kN·m at the ends and at mid-span, and the distributed self weight $wL^2/12$ and $wL^2/24$:
$$\boxed{M_f = 807.6\ \text{kN}\cdot\text{m (hogging at A, B, C)}, \quad M_f = 778.8\ \text{kN}\cdot\text{m (sagging)}, \quad V_f = 418.2\ \text{kN}}$$
Two layers of 30M bars with 40 mm cover and 10 M stirrups give $d = 820$ mm.
Size the flexural steel. Equating the internal couple to the factored moment, with $C = \alpha_1\phi_cf'_cba$ and $T = \phi_sA_sf_y$,
$$M_r = \phi_sA_sf_y\left(d - \frac{a}{2}\right), \qquad a = \frac{\phi_sA_sf_y}{\alpha_1\phi_cf'_cb}$$
Solving the resulting quadratic gives $A_s = 3244$ mm2 for the hogging sections and 3113 mm2 for the sagging ones. Provide 5 – 30M (3500 mm2) at both.
Verify the chosen bars. With $A_s = 3500$ mm2, $a = 189.5$ mm and $c = a/\beta_1 = 212$ mm, so
$$\frac{c}{d} = 0.258 \;<\; 0.6 \quad\text{(ductile, tension-controlled)}, \qquad M_r = 863.0\ \text{kN}\cdot\text{m} \;\ge\; 807.6\ \text{kN}\cdot\text{m}$$
The minimum steel requirement, $A_{s,\min} = 0.2\sqrt{f'_c}\,b_th/f_y = 986$ mm2, is comfortably exceeded. Five 30M bars in one layer need $5(29.9) + 4(40) = 310$ mm of clear width against 400 − 2(40) − 2(11.3) = 297 mm, so place them in two layers of 3 and 2, which is what the 820 mm effective depth already assumes.
Design the shear reinforcement. Take $d_v = \max(0.9d, 0.72h) = 738$ mm. The section at $d_v$ from each support carries $V_f = 410.2$ kN. With minimum stirrups present the simplified method allows $\beta = 0.18$ and $\theta = 35^\circ$:
$$V_c = \phi_c\lambda\beta\sqrt{f'_c}\,b_wd_v = 0.65(0.18)\sqrt{30}(400)(738) = 189.2\ \text{kN}$$
$$V_s = 410.2 - 189.2 = 221.0\ \text{kN} \quad\Longrightarrow\quad s = \frac{\phi_sA_vf_yd_v\cot\theta}{V_s} = 324\ \text{mm}$$
Detail the stirrups. Since $V_f = 410$ kN is below $0.125\lambda\phi_cf'_cb_wd_v = 720$ kN, the spacing ceiling is $\min(0.7d_v, 600) = 517$ mm. Adopt 10M closed stirrups at 300 mm through the shear zones, giving
$$V_r = 189.2 + \frac{\phi_sA_vf_yd_v\cot\theta}{300} = \boxed{428\ \text{kN}} \;\ge\; 410.2\ \text{kN}$$
and relax to 450 mm in the low-shear region either side of each load point. Web crushing is remote: $V_{r,\max} = 0.25\phi_cf'_cb_wd_v = 1439$ kN.
Set out the layout. Top steel (5 – 30M) runs continuously over each support and is curtailed where the hogging moment falls below the capacity of the remaining bars — roughly 3.2 m each side of A and C and 3.2 m each side of B — with all bars extended a further $\max(d, 12d_b) = 820$ mm beyond the theoretical cut-off. Bottom steel (5 – 30M) runs beneath each 500 kN load, with at least two bars carried into and anchored at the supports for integrity. Top and bottom bars lap over the support at B, and the built-in ends at A and C require full development of the top steel into the supporting wall (a 90° standard hook with $l_{dh} \approx 550$ mm).
Reinforcement layout and cross-section for the RC girder.
Final Results
Item
Value
Section
400 × 900 mm, d = 820 mm
Design moments
807.6 kN·m hogging; 778.8 kN·m sagging
Flexural steel
5 – 30M top at A, B, C; 5 – 30M bottom under each load
Resistance provided
Mr = 863 kN·m, c/d = 0.258
Design shear
Vf = 410.2 kN at dv from the support
Shear steel
10M closed stirrups at 300 mm (450 mm in low-shear zones)