16-Civ-A2 Elementary Structural Design · December 2019
Question 2 of 7: A2 — Shear connection and welded splice for a W200×27
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2019 — 16-Civ-A2 Elementary Structural Design. Three hours, CLOSED BOOK. Seven questions in three parts: Part A (A1–A3, steel to CSA S16), Part B (B1–B3, reinforced concrete to CSA A23.3), Part C (C1, timber to CSA O86). A candidate submits five solutions — two from Part A, two from Part B and the single Part C question — all of equal value. All seven are solved below, because this set is a study resource rather than an exam script. Note 6 on page 1 states that all loads shown are unfactored unless otherwise stated, so every load pattern is factored here before it meets a resistance; Note 7 fixes G40.21 300W steel and 400W reinforcement unless a question says otherwise.
Reference texts.
CSA S16:19, Design of Steel Structures, and CISC Handbook of Steel Construction, 11th ed. — Clauses 13.3 (compression), 13.13 (welds), 17 (composite beams), and the angle/W-shape section tables.
CSA A23.3:19, Design of Concrete Structures, and the Cement Association of Canada Concrete Design Handbook, 4th ed. — Clauses 10 (flexure and columns) and 11 (shear).
CSA O86:19, Engineering Design in Wood, and the Canadian Wood Council Wood Design Manual — Clause 6 (sawn lumber) and the service-condition and size-factor tables.
Kulak & Grondin, Limit States Design in Structural Steel, 11th ed., Chs. 4, 5, 8, 9.
National Building Code of Canada, Table 4.1.3.2 (load combinations).
Check — assumptions declared under Note 1 of the paper. (i) Figure A1 shows a solid vertical between F and C as well as the load arrow at C; that member is required, because without it the truss counts m + r = 12 + 3 = 15 against 2n = 16 and is a mechanism. With it, m + r = 16 = 2n and the truss is determinate, which is how it is solved here. (ii) In A3 the number of shear studs is reported as a bonus; the question asks only for the ultimate moment. (iii) In B1 the two stacked dimensions read as a sum, so the tee is 100 mm flange plus 400 mm of stem, i.e. 500 mm overall, and the beam spacing of 1250 mm governs the effective flange width because no span is given. (iv) In C1 the 1.5 kPa / 1.0 kPa area loads are converted to line loads on the 0.9 m tributary width, and the deflection limits adopted are L/240 on the back span and 2L/180 on the cantilever.
Question 2: A2 — Shear connection and welded splice for a W200×27 (20 marks)
Given. The design starts from a laterally supported W200×27 beam spanning 5.0 m into the flange of a W200×59 column, M20 A325 bolts and E49XX electrodes, and splice actions of 40 kN·m moment with 50 kN shear.
Given data
Item
Value
Beam
W200×27: d = 207, b = 133, t = 8.4, w = 6.4 mm, Zx = 277×10³ mm³
Column
W200×59: d = 210, b = 205, t = 14.2, w = 9.1 mm
Beam span
5.0 m, simply supported, laterally supported
Steel / bolts / electrode
300W; M20 A325; E49XX (Xu = 490 MPa)
Splice actions
Mf = 40 kN·m, Vf = 50 kN
Find. (a) the end reaction the shear connection must carry and a bolted double-angle connection to the column flange that develops it; (b) a flange-and-web fillet-welded splice for the stated moment and shear.
Left: bolted double-angle shear connection, beam web to column flange. Right: welded splice with flange plates above and below and a pair of web plates.
Approach. For (a), work backwards: the largest uniformly distributed load a laterally supported W200×27 can carry over 5 m follows from $M_r = \phi Z F_y$, and 60 % of that load fixes the end reaction. Then check bolts, bearing, the angles and the welds against it. For (b), split the actions the way the section carries them: the flanges take the moment as a couple, the web takes the shear.
Moment resistance of the beam. Laterally supported and Class 1, so $$M_r = \phi Z_x F_y = 0.90\,(277\times10^{3})(300) = \boxed{74.8\ \text{kN}\cdot\text{m}}$$
Maximum uniformly distributed load. For a simple span, $M = wL^{2}/8$, so $$w_{\max} = \frac{8M_r}{L^{2}} = \frac{8(74.8)}{5^{2}} = 23.93\ \text{kN/m}$$ Shear does not limit it: $V_r = \phi A_w (0.66F_y) = 0.90(207)(6.4)(198)/10^{3} = 236$ kN, which corresponds to about 94 kN/m. Flexure governs, as the phrase "laterally supported" implies.
Design reaction for the connection. At 60 % of that load, $$w = 0.60(23.93) = 14.36\ \text{kN/m},\qquad V_f = \frac{wL}{2} = \frac{14.36(5)}{2} = \boxed{35.9\ \text{kN}}$$
Bolt group. Try two M20 A325 bolts through the beam web in double shear (one angle each side), at 70 mm pitch with 35 mm end distances, so each angle is 140 mm long. With threads intercepted by the shear planes, $$V_r = 0.60\,\phi_b\, n\, m\, A_b\, F_u (0.70) = 0.60(0.80)(1)(2)(314)(830)(0.70)/10^{3} = 175\ \text{kN per bolt}$$ Two bolts give 350 kN against 35.9 kN required — the connection is governed by detailing rules, not by strength, which is normal for a shear tab on a light beam.
Bearing on the beam web. The 6.4 mm web is the thin part: $$B_r = 3\,\phi_{br}\, t\, d\, F_u = 3(0.80)(6.4)(20)(450)/10^{3} = 138\ \text{kN per bolt}$$ so 276 kN for the pair. Adequate.
Angles. Two L90×90×8, each 140 mm long. Gross shear of the pair is $$V_r = 2\,\phi(0.66F_y)A_g = 2(0.90)(198)(8)(140)/10^{3} = 399\ \text{kN}$$ and the block-shear and net-section paths are far above the 35.9 kN demand at this size.
Weld to the column flange. Each angle is fillet welded along its two vertical edges to the W200×59 flange. Take two 6 mm fillets, 140 mm long, loaded longitudinally ($\theta = 0$): $$V_r = 2\left[0.67\,\phi_w\,(0.707D L)\,X_u\right] = 2\left[0.67(0.67)(0.707)(6)(140)(490)\right]/10^{3} = 261\ \text{kN}$$ The 6 mm leg is the S16 Table 7 minimum for the 14.2 mm flange it is welded to, so it cannot be reduced.
Splice, part (b) — flange couple. Assign the whole moment to the flanges. The couple acts on the lever arm between flange centroids, $d - t$: $$T_f = \frac{M_f}{d - t} = \frac{40\times10^{6}}{207 - 8.4} = \boxed{201.4\ \text{kN}}$$
Flange splice plates. A 120×10 plate fits inside the 133 mm flange with room for the fillet on each side: $$T_r = \phi A_g F_y = 0.90(120)(10)(300)/10^{3} = 324\ \text{kN} \;>\; 201.4\ \text{kN}\quad(\text{utilisation }0.62)$$
Flange welds. Each end of the plate is welded with two 120 mm longitudinal fillets down the sides plus one 120 mm transverse fillet across the end. Using $V_r = 0.67\phi_w(0.707DL)X_u(1 + 0.50\sin^{1.5}\theta)$ with 6 mm legs, $$V_r = 2(133) + 126 = 392\ \text{kN} \;>\; 201.4\ \text{kN}$$ The transverse run earns the 1.50 directional multiplier; the side runs do not.
Web splice plates and welds. Give the web the shear alone. Two 6×150 plates, one each side: $$V_r = 2\,\phi(0.66F_y)A = 2(0.90)(198)(6)(150)/10^{3} = 321\ \text{kN} \;>\; 50\ \text{kN}$$ and four 5 mm longitudinal fillets 150 mm long give $V_r = 467$ kN. Both are far above the 50 kN demand, so the plate size is set by giving the welds room rather than by strength.
Final results
Quantity
Value
Mr of the W200×27
74.8 kN·m
Maximum UDL over 5 m
23.93 kN/m (flexure governs)
Design UDL at 60 %
14.36 kN/m
(a) Connection shear Vf
35.9 kN
(a) Connection selected
2 — L90×90×8 × 140 long, 2-M20 A325 (double shear), 6 mm fillets to the column flange