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07-Str-A2 · May 2013

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)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

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.

C fixed baseB pinnedP (bracket)e6 mColumn and bracketBending momentM = P eM = P e / 2inflexion
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.

  1. Section properties. With $d_i = D - 2t = 406.4 - 19.06 = 387.34$ mm, $$A=\frac{\pi}{4}\left(D^2-d_i^2\right)=11\,882\ \text{mm}^2,\qquad I=\frac{\pi}{64}\left(D^4-d_i^4\right)=234.1\times10^{6}\ \text{mm}^4$$ $$r=\sqrt{I/A}=140.4\ \text{mm},\qquad Z=\frac{D^3-d_i^3}{6}=1\,501\times10^{3}\ \text{mm}^3$$
  2. 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.
  3. Compressive resistance. A column pinned at one end and fixed at the other takes the recommended design value $K = 0.8$, so $$\frac{KL}{r}=\frac{0.8(6\,000)}{140.4}=34.2,\qquad \lambda=\frac{KL}{r}\sqrt{\frac{F_y}{\pi^2E}}=34.2\sqrt{\frac{350}{1.974\times10^{6}}}=0.455$$ $$C_r=\phi A F_y\left(1+\lambda^{2n}\right)^{-1/n} =0.90(11\,882)(350)(1+0.455^{4.48})^{-1/2.24}=\boxed{3\,695\ \text{kN}}$$
  4. Moment resistance. Being Class 2, and with no lateral-torsional buckling possible in a circular tube, $$M_r=\phi Z F_y = 0.90(1\,501\times10^{3})(350)=473\ \text{kN}\cdot\text{m}$$
  5. 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.
  6. Cross-sectional strength (Cl 13.8.2 a). With $C_r$ replaced by $\phi A F_y = 3\,743$ kN, $$\begin{aligned} \frac{P_f}{3\,743}+\frac{0.85(1.0)(0.8P_f)}{473} &\le 1.0\\ P_f\left(2.672\times10^{-4}+1.438\times10^{-3}\right) &\le 1.0 \quad\Rightarrow\quad P_f \le 587\ \text{kN} \end{aligned}$$
  7. 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.
  8. 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.
QuantityValue
$A$ / $I$ / $r$ / $Z$11 882 mm2 / $234.1\times10^{6}$ mm4 / 140.4 mm / $1\,501\times10^{3}$ mm3
$D/t$ and class42.6, Class 2 in flexure, non-slender in compression
$KL/r$ with $K = 0.8$34.2 ($\lambda = 0.455$)
$C_r$3 695 kN
$M_r$473 kN·m
Cross-sectional strength limit587 kN
Member strength limit (governs)585 kN
$M_f$ at that load468 kN·m (0.99 $M_r$)