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04-BS-6 · December 2015

Question 7 of 8: Composite Wood-Steel Beam

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

Notes on this paper

National Exams December 2015 — 04-BS-6: Mechanics of Materials (3 hours, closed book, one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper on the official exam; every question is answered below.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed. (beam deflection, torsion, transformation of stress, combined loading, columns); CISC Handbook of Steel Construction (W-shape section properties, attached to this exam).

Question 7: Composite Wood-Steel Beam (20 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.

QuantityValue
Span6 m (3 m + 3 m), point load 70 kN at midspan
Wood core100 mm wide × 300 mm deep, centred; E=10 GPa, σallow=10 MPa
Steel channels (top & bottom)full-width (120 mm) × 10 mm base plate + two 10×30 mm legs meeting the wood; E=200 GPa, σallow=240 MPa
70 kN3 m3 m
Simply supported composite beam with a 70 kN point load at midspan.

Find. Whether the section survives the 70 kN load in BOTH materials, and the maximum load it can carry.

Approach. Use the transformed-section method (steel widths × $n=E_s/E_w$) to get the composite $\bar y$ and $I_{tr}$, then apply $\sigma_{wood}=My/I_{tr}$ and $\sigma_{steel}=nMy/I_{tr}$ at each extreme fibre.

  1. Transform to wood-equivalent, $n=E_s/E_w=20$. The section is symmetric top to bottom about the wood's own mid-depth, so the transformed centroid sits there: $\bar y = 150$ mm from the wood's bottom fibre.
  2. Transformed moment of inertia: $$I_{tr} = 2.523\times10^9\ \text{mm}^4$$ with $y_{wood}=\pm150$ mm to the wood's own extreme fibres and $y_{steel}=\pm190$ mm to the outer steel fibres.
  3. (a) Applied moment and stress check at the 70 kN load: $$M = \frac{PL}{4} = \frac{70(6)}{4} = 105\ \text{kN}\cdot\text{m}$$ $$\sigma_{wood} = \frac{My_{wood}}{I_{tr}} = \frac{(105\times10^6)(150)}{2.523\times10^9} = \pm6.24\ \text{MPa} \;(<10\ \text{MPa allow})$$ $$\sigma_{steel} = \frac{nMy_{steel}}{I_{tr}} = \frac{20(105\times10^6)(190)}{2.523\times10^9} = \pm158.1\ \text{MPa} \;(<240\ \text{MPa allow})$$ $$\boxed{\text{Both materials stay within their allowable stress} \Rightarrow \text{the beam CAN support the 70 kN load}}$$
  4. (b) Maximum load without failure. Find the moment that first exhausts either material's allowable, then convert back through $M=PL/4$: $$M_{wood,allow} = \frac{10\,I_{tr}}{150} = 168.2\ \text{kN}\cdot\text{m}\qquad M_{steel,allow} = \frac{240\,I_{tr}}{20(190)} = 159.4\ \text{kN}\cdot\text{m}$$ Steel governs (lower capacity): $$\boxed{P_{max} = \frac{4\,M_{steel,allow}}{L} = \frac{4(159.4)}{6} = 106.2\ \text{kN}}$$
woodsteel158 MPa (steel)158 MPa (steel)6.2 (wood)-6.2 (wood)
Composite cross-section (wood core capped top and bottom by U-shaped steel channels) with the resulting stress distribution.
QuantityValue
Itr2.523×109 mm4
σwood at 70 kN±6.24 MPa (OK, <10)
σsteel at 70 kN±158.1 MPa (OK, <240)
Governing materialsteel
Pmax106.2 kN