NivaarExam PrepOfficial exam papers ↗

07-Str-A2 · May 2017

Question 2 of 7: A2 — Moments of resistance of a built-up plate section

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examinations, May 2017 — 07-Str-A2 Elementary Structural Design. Three hours, closed book (handbooks and textbooks permitted). Seven questions in three parts: Part A (A1–A3, structural steel to CSA S16), Part B (B1–B3, reinforced concrete to CSA A23.3) and Part C (C1, timber to CSA O86). A candidate answers two from Part A, two from Part B and the one question in Part C — five solutions of equal value, with the page-1 mark split A1 (12+8), A2 (8+12), A3 (8+12), B1 (12+8), B2 (10+8+2), B3 (12+8), C1 (8+6+6). All seven are solved here, because the set is a study resource rather than a sitting.

Reference texts.

Load factors. NOTE 6 on page 1 states that all loads shown are unfactored. The point loads drawn on Figures A1, B1 and B2 are occupancy loads, so they are factored by 1.5; the only dead load anywhere in this paper is the concrete self-weight of the Question B2 beam, which takes 1.25. This follows NBCC combination 2, 1.25D + 1.5L.

Check — figure page. Two figure readings are flagged where they arise: in Figure B1 the 350 kN load acts at midspan of beam BA (3.5 m from B), not at joint B; and the 80 kN horizontal load acts 4 m below B, i.e. 6 m above the pin at C.

Question 2: A2 — Moments of resistance of a built-up plate section (8 + 12 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. From the figure, all plates 25 mm thick, G40.21-350W (Fy = 350 MPa):

ElementSize (mm)Area (mm2)Position
Top flange600 × 2515 000300 + 300 about the y–y centreline
Webs (2)25 × 25012 500at x = ±200 mm (100 + 400 + 100 = 600)
Bottom flanges (2)200 × 2510 000centred on each web
Overall depth30037 50025 + 250 + 25

Find. Mrx and Mry, the factored moments of resistance of the cross-section about its two centroidal axes.

x–xy–yC30030040030020025 mm plate
Figure A2 — built-up section from 25 mm plates; C is the elastic centroid.

Approach. Locate the elastic centroid, compute Ix and Iy, classify every plate element under S16 Table 2, then — the section being Class 1 — find each plastic modulus from the equal-area axis and take Mr = φZFy.

  1. Locate the centroid. Measuring y upward from the underside of the bottom flanges, $$\bar{y} = \frac{10\,000(12.5) + 12\,500(150) + 15\,000(287.5)}{37\,500} = \boxed{168.3\ \text{mm}}$$ so the x–x axis sits 168.3 mm above the bottom and 131.7 mm below the top. The section is symmetric about y–y, so that axis is the vertical centreline.
  2. Second moments of area. Summing Iown + Ad2 over the five plates, $$I_x = 526.5\times10^{6}\ \text{mm}^{4}, \qquad I_y = 1384.0\times10^{6}\ \text{mm}^{4}$$ This is the first thing to notice about the section: it is wide and shallow, so Iy is 2.6 times Ix and y–y is the strong axis, not x–x. The corresponding radii of gyration are rx = 118.5 mm and ry = 192.1 mm, both needed in Question A3.
  3. Classify the elements. With √Fy = 18.71, the Class 1 limits of S16 Table 2 are 145/√Fy = 7.75 for a flange outstand, 525/√Fy = 28.1 for a plate supported on both edges in uniform compression, and 1100/√Fy = 58.8 for a web in flexure. The actual ratios are
    Elementb/t or h/wClass 1 limit
    Top-flange outstand past a web, 87.5/253.57.75
    Top flange between the webs, 375/2515.028.1
    Web, 250/2510.058.8
    Bottom-flange outstand, 87.5/253.57.75
    Every element is comfortably Class 1, so the full plastic moment may be used about both axes.
  4. Locate the plastic neutral axis for x–x. The plastic axis divides the section into equal areas, not equal first moments. Half the area is 18 750 mm2; the two bottom flanges supply 10 000 mm2, and the two webs then supply 50 mm2 for every millimetre of height: $$y_p = 25 + \frac{18\,750 - 10\,000}{2 \times 25} = \boxed{200\ \text{mm from the bottom}}$$ This sits 31.7 mm above the elastic centroid — the two axes coincide only in a doubly symmetric section.
  5. Plastic modulus about x–x. Taking each part's area times the distance from its own centroid to yp, $$Z_x = 10\,000(187.5) + 8750(87.5) + 3750(37.5) + 15\,000(87.5) = \boxed{4.094\times10^{6}\ \text{mm}^{3}}$$
  6. Plastic modulus about y–y. Symmetry puts the plastic axis on the centreline, so $$Z_y = 2(7500)(150) + 2(6250)(200) + 2(5000)(200) = \boxed{6.750\times10^{6}\ \text{mm}^{3}}$$
  7. Moments of resistance. The question asks for the resistance of the cross-section, so no lateral-torsional reduction applies: $$M_{rx} = \phi Z_x F_y = 0.90 \times 4.094\times10^{6} \times 350 = \boxed{1290\ \text{kN}\cdot\text{m}}$$ $$M_{ry} = \phi Z_y F_y = 0.90 \times 6.750\times10^{6} \times 350 = \boxed{2126\ \text{kN}\cdot\text{m}}$$
  8. Sanity-check with the elastic moduli. Sx = 526.5×106/168.3 = 3.128×106 mm3 to the bottom fibre and Sy = 1384.0×106/300 = 4.613×106 mm3, giving shape factors of 1.31 and 1.46. Both are far above the 1.12 typical of a rolled I-shape, which is exactly what one expects when so much of the area sits close to the neutral axis.
QuantityValue
Area, A37 500 mm2
Centroid above the bottom fibre, ŷ168.3 mm
Ix / Iy526.5 / 1384.0 ×106 mm4
rx / ry118.5 / 192.1 mm
Plastic neutral axis (x–x), yp200 mm from the bottom
Zx / Zy4.094 / 6.750 ×106 mm3
Section classClass 1 (every element)
Mrx1290 kN·m
Mry2126 kN·m