Question 4 of 7: B1 — Design of the column of a determinate concrete frame
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, May 2017 — 07-Str-A2 Elementary Structural Design. Three hours, closed book (handbooks and textbooks permitted). Seven questions in three parts: Part A (A1–A3, structural steel to CSA S16), Part B (B1–B3, reinforced concrete to CSA A23.3) and Part C (C1, timber to CSA O86). A candidate answers two from Part A, two from Part B and the one question in Part C — five solutions of equal value, with the page-1 mark split A1 (12+8), A2 (8+12), A3 (8+12), B1 (12+8), B2 (10+8+2), B3 (12+8), C1 (8+6+6). All seven are solved here, because the set is a study resource rather than a sitting.
Reference texts.
CSA S16:19, Design of Steel Structures — Clauses 11 (section class), 13.3 (compression), 13.5 (bending), 13.8 (axial force and bending), 13.13 (welds), 14.3 (concentrated forces).
CISC, Handbook of Steel Construction — rolled-section dimensions and properties, weld tables.
CSA A23.3:19, Design of Concrete Structures — Clauses 10 (flexure and axial load), 11 (shear).
CSA O86:19, Engineering Design in Wood — Clause 6 (sawn lumber), Tables 6.3.1B and 6.4.5.
Canadian Wood Council, Wood Design Manual; National Building Code of Canada 2020 (load combinations).
Load factors. NOTE 6 on page 1 states that all loads shown are unfactored. The point loads drawn on Figures A1, B1 and B2 are occupancy loads, so they are factored by 1.5; the only dead load anywhere in this paper is the concrete self-weight of the Question B2 beam, which takes 1.25. This follows NBCC combination 2, 1.25D + 1.5L.
Check — figure page. Two figure readings are flagged where they arise: in Figure B1 the 350 kN load acts at midspan of beam BA (3.5 m from B), not at joint B; and the 80 kN horizontal load acts 4 m below B, i.e. 6 m above the pin at C.
Question 4: B1 — Design of the column of a determinate concrete frame (12 + 8 marks)
Find. Rectangular dimensions for column BC and its longitudinal and transverse reinforcement, satisfying flexure, axial load and shear, with the bar layout shown.
Figure B1 — determinate frame ABC: pin at C, roller at A, rigid corner at B.
Approach. Solve the determinate frame for the column's axial force, moment and shear, factor them, and — because the eccentricity turns out to be enormous — design the section by strain compatibility at the actual Pf rather than with an axial-capacity formula. Then check shear and slenderness.
Solve the frame. Place C at the origin, B at (0, 10) and A at (7, 10). The pin at C supplies two reactions and the roller at A one, so r = 3 on a single rigid body and the frame is determinate. Taking moments about C,
$$7A_y = 350(3.5) + 80(6.0) = 1225 + 480 = 1705 \;\Rightarrow\; A_y = 243.6\ \text{kN}$$
$$C_y = 350 - 243.6 = 106.4\ \text{kN}\ \text{(up)}, \qquad C_x = 80\ \text{kN}\ \text{(to the left)}$$
Internal actions in column BC. Working up from the pin, the only horizontal force below the 80 kN load is Cx, so the column carries a constant shear of 80 kN over the lower 6 m and a moment growing linearly to
$$M = 80 \times 6.0 = 480\ \text{kN}\cdot\text{m}$$
Above the load the two horizontal forces cancel, so the shear is zero and the moment stays at 480 kN·m all the way to B. Reading the same moment along the beam confirms the joint: MB = 243.6(7) − 350(3.5) = 1705 − 1225 = 480 kN·m. The axial force in the column is Cy = 106.4 kN throughout.
Factor the actions. All applied loads are occupancy loads:
$$P_f = 1.5(106.4) = \boxed{159.6\ \text{kN}}, \quad M_f = 1.5(480) = \boxed{720\ \text{kN}\cdot\text{m}}, \quad V_f = 1.5(80) = \boxed{120\ \text{kN}}$$
The eccentricity is e = Mf/Pf = 4510 mm — five times the section depth. This member is a beam that happens to stand upright, and the axial-capacity formula Pr,max = 0.80[…] would be meaningless here.
Choose trial dimensions. Bending is in the plane of the frame, so the depth must lie in that plane. Try 400 mm wide × 900 mm deep with 4–30M in each of the two faces perpendicular to the bending axis (eight bars, 5600 mm2, ρ = 1.56 %, between the A23.3 Clause 10.9.1 limits of 1 % and 8 %). With 40 mm cover and 10M ties,
$$d = 900 - 40 - 11.3 - 14.95 = 833.8\ \text{mm}, \qquad d' = 66.3\ \text{mm}$$
Solve the section by strain compatibility. Set the extreme-fibre strain at 0.0035, guess the neutral-axis depth c, take the concrete compression as α1φcfc'b(β1c) and each bar force as φsEsεsAs capped at φsfy, and iterate until the net axial force equals Pf. That converges at
$$c = 94.9\ \text{mm}, \qquad a = \beta_1 c = 83.8\ \text{mm}$$
At this depth the near-face bars sit 66.3 mm from the compression face, just inside c, so they are in mild compression (211 MPa) while the far-face bars are far past yield in tension.
Moment resistance at that axial load. Taking moments of the three forces about mid-depth,
$$M_r = \boxed{807\ \text{kN}\cdot\text{m}} \;>\; M_f = 720\ \text{kN}\cdot\text{m}$$
a utilisation of 0.89. The section is strongly tension-controlled — c/d = 0.11 — so it will warn before it fails, which is exactly what one wants in a member whose demand is almost pure flexure.
Shear. With dv = max(0.9d, 0.72h) = 750.4 mm and the simplified method (β = 0.18, minimum ties provided),
$$V_c = \phi_c \lambda \beta \sqrt{f_c'}\, b_w d_v = 0.65(1.0)(0.18)\sqrt{35}(400)(750.4) = 208\ \text{kN} \;>\; 120\ \text{kN}$$
The concrete alone carries the shear — and this ignores the favourable axial compression — so minimum ties govern. Their maximum spacing is the least of 16db = 478 mm, 48 tie diameters = 542 mm and the least column dimension = 400 mm. Use 10M ties at 300 mm, closed, with every corner bar and every alternate bar restrained by a tie corner.
Slenderness. The roller at A cannot restrain the frame horizontally on its own, but a sway of the column would rotate the rigid joint at B and therefore lift or drop A, which the roller prevents — so the frame is non-sway. Taking k = 1.0 conservatively and r = 0.3h = 270 mm,
$$\frac{k l_u}{r} = \frac{10\,000}{270} = 37.0 \;>\; 34 - 12\left(\frac{M_1}{M_2}\right) = 34$$
so Clause 10.15 requires a magnifier to be evaluated. With Ec = 4500√35 = 26 622 MPa, EI = 0.4EcIg and Pc = π2EI/(klu)2 = 25 540 kN, and with Cm = 0.6 + 0.4(0) = 0.6,
$$\delta = \frac{C_m}{1 - P_f/(0.75P_c)} = \frac{0.6}{1 - 159.6/19\,155} = 0.605 \;\Rightarrow\; \delta = 1.0$$
The axial load is so small beside Pc that no magnification arises; the design moment stays at 720 kN·m and the section stands.
Reinforcement layout. A 400 × 900 mm column, the 900 mm dimension in the plane of the frame. Four 30M bars in each 400 mm face, one in each corner and two evenly spaced between, with 40 mm clear cover. Closed 10M ties at 300 mm throughout, reduced to 150 mm over the 900 mm above C and below B to confine the bar cages at the pin and at the rigid joint. The eight bars must be lapped into the beam at B and anchored into the pin detail at C.
Quantity
Value
Reactions
Ay = 243.6 kN, Cy = 106.4 kN, Cx = 80 kN
Column moment at B (unfactored)
480 kN·m (constant above the 80 kN load)
Factored actions on BC
Pf = 159.6 kN, Mf = 720 kN·m, Vf = 120 kN
Eccentricity Mf/Pf
4510 mm — flexure-dominated
Section
400 × 900 mm
Longitudinal steel
8–30M (4 per face), ρ = 1.56 %
Neutral axis / Mr at Pf
c = 94.9 mm; Mr = 807 kN·m (util. 0.89)
Vc
208 kN > 120 kN — minimum ties govern
Transverse steel
10M closed ties @ 300 mm (150 mm at the ends)
Slenderness
klu/r = 37.0; magnifier δ = 1.0
Check — sidesway assumption. The non-sway classification rests on the roller at A restraining vertical movement and the joint at B being rigid. If the frame were instead treated as free to sway (k = 2.0), klu/r would rise to 74 and Pc would drop to 6385 kN — but even then Pf/(0.75Pc) = 0.033 and δ would still compute below 1.0. The conclusion is insensitive to the assumption because the axial load is tiny.