Question 3 of 7: Maximum factored bracket load on a round HSS column
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. 07-Str-A2 Elementary Structural Design, National
Examinations May 2013, three-hour duration. The paper is printed on three pages: page 1 carries
the notes and the marking scheme, page 2 the seven questions, page 3 the five hand-drawn figures.
Part A (steel, questions A1–A3), Part B (reinforced concrete, questions B1–B3) and
Part C (timber, question C1) are answered by doing two of three from Part A, two of
three from Part B and the one question in Part C — five solutions in all, all
questions of equal value. Because this set is a study resource, all seven questions are
solved below. Note 3 of the paper fixes the design standards: steel to CSA S16, concrete
to CSA A23.3, timber to CSA O86 (latest editions). Note 6 states that all loads shown are
unfactored.
Reference texts. CSA S16, Design of Steel Structures, with the
CISC Handbook of Steel Construction (section tables, Class H HSS, fillet-weld tables);
CSA A23.3, Design of Concrete Structures; CSA O86, Engineering Design in Wood,
with the CWC Wood Design Manual; National Building Code of Canada (load combinations);
MacGregor and Bartlett, Reinforced Concrete: Mechanics and Design (Canadian edition);
Salmon, Johnson and Malhas, Steel Structures: Design and Behavior.
Check — load factors used throughout. The
paper states that all loads shown are unfactored but nowhere splits them into dead and live.
Every applied load in Figures A2, B1, B2 and B3 is therefore taken as a specified live load
and factored by 1.5, and self-weight (where the question asks for it)
by 1.25, per NBCC load combination case 2, 1.25D +
1.5L. If a grader intends a different split the factored actions scale linearly and every
design step below is unchanged. Self-weight of the steel members in A2 and A3 is neglected; for the
W610x241 of A2 it would add about 4 per cent to the moment at B.
Question A3: Maximum factored bracket load on a round HSS column (12 + 8 marks)
Given. Circular hollow section, outside diameter $D = 406.4$ mm, wall
$t = 9.53$ mm, G40.21 350W Class H, so $F_y = 350$ MPa, $E = 200\,000$ MPa, $\phi = 0.90$ and the
column-curve exponent $n = 2.24$ (CSA S16 Cl 13.3.1, Class H). Height $L = 6\,000$ mm, pinned at the
top and fixed at the base; bracket eccentricity $e = 0.8$ m.
Find. The largest factored vertical bracket load $P_f$ the column can
carry.
The column as a propped cantilever. The bracket applies P at 0.8 m eccentricity at the top, so M = Pe there and, by carry-over to the fixed base, Pe/2 of opposite sign; the member bends in double curvature.
Approach. Compute the section properties and classify the tube; get
$C_r$ from the CSA S16 column equation with $K = 0.8$ and $M_r = \phi Z F_y$; establish the moment
diagram produced by the eccentric bracket; then solve the beam-column interaction equations of
Cl 13.8.2 for the load that makes the utilisation exactly unity.
Section properties. With $d_i = D - 2t = 406.4 - 19.06 = 387.34$ mm,
$$A=\frac{\pi}{4}\left(D^2-d_i^2\right)=11\,882\ \text{mm}^2,\qquad
I=\frac{\pi}{64}\left(D^4-d_i^4\right)=234.1\times10^{6}\ \text{mm}^4$$
$$r=\sqrt{I/A}=140.4\ \text{mm},\qquad Z=\frac{D^3-d_i^3}{6}=1\,501\times10^{3}\ \text{mm}^3$$
Classify the tube. $D/t = 406.4/9.53 = 42.6$. CSA S16 Table 2 sets the
class limits for a circular hollow section in flexure at $13\,000/F_y = 37.1$ (Class 1),
$18\,000/F_y = 51.4$ (Class 2) and $66\,000/F_y = 188.6$ (Class 3), so the section is
Class 2 and the plastic moment may still be used. For axial compression the
non-slender limit is $23\,000/F_y = 65.7 > 42.6$, so the whole area is effective.
Compressive resistance. A column pinned at one end and fixed at the other
takes the recommended design value $K = 0.8$, so
$$\frac{KL}{r}=\frac{0.8(6\,000)}{140.4}=34.2,\qquad
\lambda=\frac{KL}{r}\sqrt{\frac{F_y}{\pi^2E}}=34.2\sqrt{\frac{350}{1.974\times10^{6}}}=0.455$$
$$C_r=\phi A F_y\left(1+\lambda^{2n}\right)^{-1/n}
=0.90(11\,882)(350)(1+0.455^{4.48})^{-1/2.24}=\boxed{3\,695\ \text{kN}}$$
Moment resistance. Being Class 2, and with no lateral-torsional buckling
possible in a circular tube,
$$M_r=\phi Z F_y = 0.90(1\,501\times10^{3})(350)=473\ \text{kN}\cdot\text{m}$$
The moment the bracket produces. The bracket delivers $M = P_f e$ to the
top of the column. The pin there restrains translation but not rotation, so the member is a propped
cantilever loaded by an end moment: the base carries half that moment with the opposite sign, and
the member bends in double curvature with $M_f = P_f(0.8)$ at the top. Since the frame is braced,
$\kappa = +0.5$ and $\omega_1 = 0.6-0.4(0.5) = 0.4$; because Cl 13.8.4 does not permit $U_1$ below
unity for the member check, take $U_{1x} = 1.0$. For information,
$C_e = \pi^2EI/L^2 = 12\,834$ kN, so the second-order magnification is small in any case.
Cross-sectional strength (Cl 13.8.2 a). With $C_r$ replaced by
$\phi A F_y = 3\,743$ kN,
$$\begin{aligned}
\frac{P_f}{3\,743}+\frac{0.85(1.0)(0.8P_f)}{473} &\le 1.0\\
P_f\left(2.672\times10^{-4}+1.438\times10^{-3}\right) &\le 1.0
\quad\Rightarrow\quad P_f \le 587\ \text{kN}
\end{aligned}$$
Overall member strength (Cl 13.8.2 b). Using the buckling resistance,
$$\begin{aligned}
\frac{P_f}{3\,695}+\frac{0.85(1.0)(0.8P_f)}{473} &\le 1.0\\
P_f\left(2.706\times10^{-4}+1.438\times10^{-3}\right) &\le 1.0
\quad\Rightarrow\quad \boxed{P_f \le 585\ \text{kN}}
\end{aligned}$$
The member check governs, though only just, because the column is stocky.
Confirm the bending check separately. At $P_f = 585$ kN the applied moment
is $M_f = 585(0.8) = 468$ kN·m against $M_r = 473$ kN·m, so the tube is at 99 per cent
of its bending capacity and at only 16 per cent of its compressive capacity. The answer is
therefore governed almost entirely by flexure from the 0.8 m bracket arm, which is worth saying
explicitly: halving the eccentricity would roughly double the permissible load.