16-Civ-B2 Advanced Structural Design · December 2016
Question 3 of 7: Plastic design of the rigid frame and its footing (16 + 4 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 98-Civ-B2 Advanced Structural Design,
December 2016, three hours, closed book (design handbooks and textbooks are permitted,
no notes). Seven design questions; any five constitute a complete paper and all
questions are of equal value (20 marks each). Because the whole paper is a study
resource, all seven questions are solved here. Page 1 states that all
loads shown on the figures are unfactored, and supplies the design data used
throughout.
Reference texts.
CSA S16:19, Design of Steel Structures — Clauses 11 (classification),
13.4 (shear), 13.5 (bending), 13.7 (bracing for plastic design), 13.8 (axial
compression and bending), 14 (plate girders), 17 (composite beams).
CISC, Handbook of Steel Construction, 12th ed. — section properties and
the beam-column selection tables.
National Building Code of Canada 2020, Part 4 — load combinations.
M. P. Collins and D. Mitchell, Prestressed Concrete Structures —
permissible-stress design and tendon-zone construction.
R. C. Hibbeler, Structural Analysis, 10th ed. — continuous-beam and
rigid-frame analysis.
Design data (page 1 of the examination paper)
Quantity
Symbol
Value
Concrete
f'c
30 MPa
Structural steel
Fy
350 MPa
Reinforcing bar
fy
400 MPa
Prestressed concrete at transfer
fci
35 MPa
Prestressed concrete
f'c
50 MPa
Modular ratio
n
6
Strand tensile strength
fult
1750 MPa
Strand yield strength
fy
1450 MPa
Initial strand stress
finitial
1200 MPa
Loss of prestress
Δfp
240 MPa
Effective strand stress
fse = 1200 − 240
960 MPa
Check — load factors. Page 1 says only that
“all loads shown are unfactored”; it gives no dead/live split, so no NBCC
combination can be formed exactly. Every solution below applies a single factor of
1.5 to the loads printed on the figures and 1.25 to
self weight that the solver itself introduces (girder, slab, frame members), and states
that assumption where it is used. The choice scales the required resistances but changes
neither the collapse mechanisms, the section classifications, nor any interaction
ratio, so the engineering conclusions are unaffected. Serviceability checks
(prestress stresses, deflections, bearing pressure) use the unfactored loads as
printed.
Question 3: Plastic design of the rigid frame and its footing (16 + 4 marks)
Given. A pin-based portal frame 12 m high spanning
10 m, carrying a 150 kN horizontal load at B together with 600 kN at each column head
and 400 kN at each of the two interior beam points; the beam is proportioned for
1.5Mp and each column for 2Mp.
Question data
Quantity
Symbol
Value
Column height
h
12 m
Beam span, B to C
L
10 m (3 m + 4 m + 3 m)
Horizontal load at B
H
150 kN → 225 kN factored
Vertical loads at B and C
P
600 kN → 900 kN factored
Interior beam loads
P
400 kN → 600 kN factored
Relative capacities
Mp,beam : Mp,col
1.5 : 2
Allowable bearing pressure
qall
500 kPa
Find. (a) The reference plastic moment
Mp that just produces collapse under the factored loads, and rolled sections
delivering 1.5Mp in the beam and 2Mp in the columns;
(b) the plan size, thickness and reinforcement of the spread footing at A.
Figure 3 — pin-based portal frame, 12 m columns and a 10 m beam; the beam is 1.5Mp and each column 2Mp.
Approach. Enumerate the independent mechanisms, form
the combination that cancels a hinge, then confirm the upper bound with a statically
admissible moment field — with pinned bases the frame is only once redundant, so
the two-hinge combined mechanism is complete and the two bounds coincide.
Part (a) — factor the loads and note where hinges can form.
Applying 1.5 to every load on the figure gives $H=225$ kN, 900 kN at each column
head and 600 kN at each interior beam point. At a joint the hinge forms in the
weaker member, and here the beam ($1.5M_p$) is weaker than the columns ($2M_p$),
so every joint hinge is a beam hinge of capacity $1.5M_p$.
Evaluate the beam mechanism. With a hinge at the 3 m load, end
rotations are $\theta$ at B and $3\theta/7$ at C, and the sagging displacements are
$3\theta$ and $9\theta/7$:
$$600(3\theta)+600\!\left(\tfrac{9}{7}\theta\right)
=1.5M_p\!\left(\theta+\theta+\tfrac{3}{7}\theta+\tfrac{3}{7}\theta\right)
\ \Rightarrow\ M_p=\frac{2571.4}{4.286}=\boxed{600\ \text{kN}\cdot\text{m}}$$
The mirror-image hinge at the 7 m load returns the same 600 kN·m, as it must
for a symmetrically loaded beam.
Evaluate the sway mechanism. The pinned bases need no hinge, so
only the two beam ends yield while the frame sways $\Delta=12\theta$:
$$225(12\theta)=1.5M_p(\theta+\theta)\ \Rightarrow\
M_p=\frac{2700}{3}=\boxed{900\ \text{kN}\cdot\text{m}}$$
Combine to cancel the hinge at B. Adding the beam and sway
mechanisms with equal rotations at B removes that hinge from both, saving
$2(1.5M_p)\theta$ of internal work while the external work simply adds:
$$M_p=\frac{2571.4+2700}{4.286+3-3}=\frac{5271.4}{4.286}
=\boxed{1230\ \text{kN}\cdot\text{m}}$$
Combining the sway with the other beam hinge gives only 870 kN·m, so
the mechanism above governs. Stopping at the independent mechanisms would have
under-designed the frame by 37 per cent.
Confirm with the lower bound. Global statics gives
$V_D=1770$ kN and $V_A=1230$ kN. Imposing $M=+1.5M_p=1845$ kN·m at the 3 m
hinge fixes the redundant, $H_A=-71.25$ kN, hence $H_D=-153.75$ kN, and then
$$M_C=12H_D=-1845\ \text{kN}\cdot\text{m}=-1.5M_p$$
exactly, so both hinge conditions are met by one statically admissible
field. The remaining moments, $M_B=855$ and $M(7\ \text{m})=765$ kN·m, and
the leeward column top at 1845 kN·m against a capacity of 2460 kN·m,
all lie inside their capacities. Upper and lower bounds coincide, so
$M_p=1230$ kN·m is the exact collapse value.
Select the beam. Plastic design requires Class 1 sections
(Clause 13.5), and
$$Z_{\text{req}}=\frac{1.5M_p}{\phi F_y}=\frac{1845\times10^6}{0.9(350)}
=5.86\times10^6\ \text{mm}^3$$
Modelling W610×195 from its nominal plate dimensions
(622 × 327, 24.4 mm flange, 15.4 mm web) gives $Z=6.03\times10^6$
mm3, hence $\phi M_p=1900$ kN·m. Its flange
$b/2t=6.70$ and web $h/w=37.2$ are both Class 1, and the beam axial force
(154 kN, under 2 per cent of $C_y$) needs no moment reduction.
Check the beam bracing for plastic design. Clause 13.7 limits
the unbraced length adjacent to a hinge to
$L_{cr}=(25\,000+15\,000\kappa)r_y/F_y$. With $r_y=75.8$ mm the three segments give
$L_{cr}=3908$, 4067 and 6760 mm against actual lengths of 3000, 4000 and 3000 mm.
Every segment passes, the 3 m to 7 m segment only just, so the bracing stated in the
question is exactly what the plastic design needs.
Select the columns. The required capacity is
$2M_p=2460$ kN·m, i.e. $Z\ge7.81\times10^6$ mm3.
W840×251 (859 × 292, 24.4 mm flange, 15.6 mm web) gives
$Z=8.51\times10^6$ mm3 and $\phi M_p=2680$ kN·m, with
$b/2t=5.98$ (Class 1) and a web at $h/w=51.9$ against the beam-column Class 1 limit
of 54.0 at $C_f/\phi C_y=0.209$. Question 6 examines this member in detail.
Part (b) — size the footing on bearing. The base at A is
pinned, so it carries axial load and shear only: $V_A=1230/1.5=820$ kN and
$H_A=71.25/1.5=47.5$ kN in service. Trying a 1.5 m square, 400 mm thick pad
(self weight 21.6 kN), the shear applied at the underside gives
$e=47.5(0.4)/841.6=22.6$ mm, well inside the middle third ($B/6=250$ mm), and
$$q_{\max}=\frac{841.6}{1.5^2}\!\left(1+\frac{6(0.0226)}{1.5}\right)
=\boxed{408\ \text{kPa}}\ \le\ 500\ \text{kPa}$$
Check the footing in shear and flexure. The net factored
pressure is $q_{nf}=1230/2.25=546.7$ kPa and, with 75 mm cover, $d=315$ mm. Punching
on a perimeter $b_0=3960$ mm at $d/2$ from a 900 × 450 mm base plate gives
$V_f=722$ kN against
$V_r=0.38\phi_c\lambda\sqrt{f'_c}\,b_0d=1688$ kN. One-way shear at $d$ from the
plate face gives $V_f=172$ kN against $V_r=294$ kN. The cantilever moment is
$$M_f=\frac{546.7(1.5)(0.525)^2}{2}=113\ \text{kN}\cdot\text{m}
\ \Rightarrow\ A_s=1082\ \text{mm}^2$$
which is below $A_{s,\min}=0.002A_g=1200$ mm2, so minimum steel governs:
provide 6–15M each way in the bottom. Sliding is not critical
($0.5\times842=421$ kN against 47.5 kN).
State what the wording of part (b) can and cannot mean. The
question names support A, which carries the smaller vertical reaction; the base at D
takes 1770 kN factored and would need a 1.8 m square on the same bearing pressure.
In practice both bases are detailed identically, so the 1.8 m pad would be used
throughout; the 1.5 m pad answers the question exactly as asked.
Statically admissible collapse moment field in the beam: hinges at the 3 m load and at joint C, both at 1.5Mp = 1845 kN·m.
Spread footing at A — 1.5 m square by 400 mm thick, 6–15M each way in the bottom mat.