Question 6 of 7: Beam-column CD and the rigid connection at B (14 + 6 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2013, 98-Civ-B2 Advanced Structural Design; 3 hours, closed book (handbooks and textbooks permitted); seven design questions, any five of which constitute a complete paper, all of equal value (20 marks each). All seven are worked below, because the set is a study resource rather than a timed sitting. Design data given on page 1 and used throughout: concrete $f^{\prime}_{c}=30\ \text{MPa}$, structural steel $F_{y}=350\ \text{MPa}$, reinforcing bar $f_{y}=400\ \text{MPa}$; for the prestressed girder $f^{\prime}_{ci}=35\ \text{MPa}$, $f^{\prime}_{c}=50\ \text{MPa}$, $n=6$, $f_{pu}=1750\ \text{MPa}$, $f_{py}=1450\ \text{MPa}$, $f_{pi}=1200\ \text{MPa}$ and losses of 240 MPa. All loads shown on the figures are unfactored.
Reference texts. CSA S16, Design of Steel Structures; CISC, Handbook of Steel Construction; Kulak & Grondin, Limit States Design in Structural Steel; CSA A23.3, Design of Concrete Structures; MacGregor & Bartlett, Reinforced Concrete: Mechanics and Design (Canadian edition); Collins & Mitchell, Prestressed Concrete Structures; Beedle, Plastic Design of Steel Frames; National Building Code of Canada.
Check — load factor. The paper states that the loads shown are unfactored but does not separate dead from live. Every design below therefore applies a single load factor of 1.5 to the given loads, which is the NBCC live-load factor and is the conservative reading when the split is unknown. Self weight, where it is generated by a member being sized here (the reinforced concrete frame of Questions 5 and 6, and the prestressed girder of Question 7), is carried separately at 1.25. If the examiner intended a different split, only the magnitudes change — every mechanism, section classification and interaction equation is unaffected.
Question 6: Beam-column CD and the rigid connection at B (14 + 6 marks)
Given. The reinforced concrete frame of Question 5, now braced at joints A, B, C and D. From the factored elastic analysis the column CD carries 1341 kN of axial compression with 1907 kN·m at its head, and the joint at B transfers 710 kN·m between the 6 m column and the beam.
Given data — beam-column CD and joint B
Quantity
Symbol
Value
Section under test
$b\times h$
600 $\times$ 1500 mm, 9-25M each face
Factored axial load in CD
$C_{f}$
1341 kN
Factored moment at C
$M_{f}$
1907 kN$\cdot$m
Column CD length
$l_{u}$
8 000 mm, braced
Factored moment at B
$M_{f}$
710 kN$\cdot$m
Column shear at B
$V_{col}$
118 kN
Beam top steel at B
$A_{s}$
5-25M $=2500\ \text{mm}^{2}$
Find. (a) whether the BC section also serves as the beam-column CD, and (b) the reinforcement at the rigid connection B.
Beam-column CD: the BC section reused with symmetric reinforcement, 9-25M each face and closed ties.
Approach. Build the axial-force / moment interaction diagram for the section with symmetric steel and locate the design point on it, check that slenderness may be neglected, then treat joint B as a corner subjected to an opening moment and detail it for joint shear and bar anchorage.
Part (a) — make the section symmetric. A beam needs steel where the tension is; a column reverses under load pattern and sway, so the same concrete section is reused with 9-25M on both faces. Strain compatibility with $\varepsilon_{cu}=0.0035$ then gives the interaction diagram: for a chosen neutral axis $c$, $$P_{r}=\alpha_{1}\phi_{c}f^{\prime}_{c}b a+\phi_{s}A_{s}^{\prime}f_{s}^{\prime}-\phi_{s}A_{s}f_{s}$$ with the companion moment taken about mid-depth.
Part (a) — where the design point sits. The balanced point of this section is near $P_{b}=6993\ \text{kN}$, so a factored load of 1341 kN is deep in the tension-controlled region, where axial compression increases the moment capacity by closing the flexural crack. Interpolating the diagram at $C_{f}=1341\ \text{kN}$ gives $$\boxed{M_{r}=2882\ \text{kN}\cdot\text{m}\ \ge\ M_{f}=1907\ \text{kN}\cdot\text{m}}$$ a utilisation of 0.66, against 0.94 for the same section in pure flexure. The section is adequate as the beam-column CD.
Part (a) — slenderness. In the plane of the frame $r=0.3h=450\ \text{mm}$, so $kl_{u}/r=8000/450=17.8$, below the braced-frame threshold $25-10(M_{1}/M_{2})=25$ with $M_{1}=0$ at the pin. Slenderness may be neglected in plane. About the weak axis $kl_{u}/r=44.4$, so either the floor system must brace the column at mid-height or the small minimum-eccentricity moment $C_{f}(15+0.03h)=80\ \text{kN}\cdot\text{m}$ must be magnified and combined; a mid-height tie beam is the cheaper answer and is assumed here.
Part (b) — what kind of corner joint B is. At B the beam hogs and the column carries the same moment, so the tension face runs continuously around the outside of the corner: this is an opening-moment corner, the detail that fails at a fraction of the members’ capacity if the bars are simply lapped around the re-entrant corner, because the resultant of the two bar forces pulls straight out of the concrete.
Part (b) — joint shear. The beam steel delivers $T=A_{s}f_{y}=2500(400)=1000\ \text{kN}$ at yield and the column shear relieves 118 kN, so the joint carries $V_{j}=882\ \text{kN}$. For a corner joint confined on two faces only, $$V_{r}=1.0\lambda\phi_{c}\sqrt{f^{\prime}_{c}}\,A_{j}=1.0(0.65)\sqrt{30}(600)(1500)=3204\ \text{kN}$$ so the joint is at 28 percent of its shear capacity; the 1500 mm column depth is what makes it so comfortable.
Part (b) — anchorage and the corner detail. The 25M beam bars are bent down into the column with standard hooks; $l_{dh}=100d_{b}/\sqrt{f^{\prime}_{c}}=460\ \text{mm}$ against 1 420 mm available inside the column, so the hooks develop easily. Loop the outer bars around the corner with a generous bend radius, add $\boxed{3\text{-}25\text{M}\ \text{diagonal bars}}$ across the re-entrant corner (at least $0.5A_{s}=1250\ \text{mm}^{2}$) to carry the outward resultant back into the section, and continue the column ties, 10M at 300 mm, through the joint.