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22-Mec-B1 Advanced Machine Design · May 2013

Question 2 of 6: Overhung diving board — impact stress and safety factor

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

Notes on this paper

Paper format: National Exams, May 2013 — 07-Mec-B1 Advanced Machine Design. Open book, 3 hours, 100 marks. Part I (Problems 1–2) is compulsory; three of the four Part II problems (3–6) constitute a complete paper. All six problems are solved as a study resource.

Reference texts. R. G. Budynas & J. K. Nisbett, Shigley’s Mechanical Engineering Design, 10th ed. (shafts §7, bolted joints §8, bearings §12, brakes §16); R. L. Norton, Machine Design: An Integrated Approach, 5th ed.; R. C. Hibbeler, Mechanics of Materials, 10th ed. (impact loading, beam deflection); R. C. Juvinall & K. M. Marshek, Fundamentals of Machine Component Design, 5th ed. (journal bearings, friction brakes).



Question 2: Overhung diving board — impact stress and safety factor (30 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. Board cross-section $b=305\text{ mm}$ wide by $h=32\text{ mm}$ thick; pinned support at the wall end, roller support $0.7\text{ m}$ from the pin, free (diving) end $2.0\text{ m}$ from the pin; diver mass $60\text{ kg}$ ($W=588.6\text{ N}$); jump height $h_j=0.25\text{ m}$; static tip deflection under the diver $\delta_{st}=0.10\text{ m}$; board mass $25\text{ kg}$; $S_{ut}=200\text{ MPa}$.

Find. (a) the largest principal (bending) stress under the impact landing; (b) the static factor of safety on $S_{ut}$.

P 2 m 0.7 m critical section
Diving board as a beam with a pin at the wall, a roller at $0.7\text{ m}$, and the diver load $P$ at the $2.0\text{ m}$ free end. The maximum bending moment occurs at the roller.

Approach. Treat the landing as a suddenly-applied (impact) load: obtain the impact factor from energy conservation using the given static deflection, scale the diver’s weight to the dynamic force, find the maximum bending moment at the roller support, and convert to bending stress through the section modulus. At the outer fibre the state is uniaxial, so the largest principal stress equals the bending stress.

  1. Section modulus of the board. Bending is about the axis with the $32\text{ mm}$ dimension as depth: $$S = \frac{b\,h^2}{6} = \frac{0.305\,(0.032)^2}{6} = 5.21\times10^{-5}\text{ m}^3.$$
  2. Impact (dynamic magnification) factor. The diver rises $h_j$ and falls back, delivering energy $W(h_j+\delta_{dyn})=\tfrac12 k\,\delta_{dyn}^2$ with $k=W/\delta_{st}$. Solving gives the classic falling-weight factor $$n = 1 + \sqrt{1 + \frac{2h_j}{\delta_{st}}} = 1 + \sqrt{1 + \frac{2(0.25)}{0.10}} = 1+\sqrt{6} = 3.45.$$
  3. Dynamic force at the free end. $$F_{dyn} = n\,W = 3.45 \times 588.6\text{ N} = 2.03\times10^{3}\text{ N}.$$
  4. Maximum bending moment. With the pin at $0$ and the roller at $0.7\text{ m}$, the overhang from the roller to the load is $2.0-0.7 = 1.3\text{ m}$; taking the free-body of the overhang, the moment is greatest at the roller: $$M_{max} = F_{dyn}\,(2.0-0.7) = 2.03\times10^{3}\times1.3 = 2.64\times10^{3}\text{ N}\cdot\text{m}.$$
  5. Largest principal stress. At the top/bottom fibre the transverse shear is zero, so the bending stress is a principal stress: $$\sigma_1 = \frac{M_{max}}{S} = \frac{2.64\times10^{3}}{5.21\times10^{-5}}.$$ $$\boxed{\sigma_1 \approx 50.7\text{ MPa}.}$$
  6. Static factor of safety. $$n_s = \frac{S_{ut}}{\sigma_1} = \frac{200}{50.7}.$$ $$\boxed{n_s \approx 3.9.}$$
Question 2 — results
QuantitySymbolValue
Impact factor$n$$3.45$
Dynamic tip force$F_{dyn}$$2.03\text{ kN}$
Max bending moment (at roller)$M_{max}$$2.64\text{ kN}\cdot\text{m}$
Largest principal stress$\sigma_1$$50.7\text{ MPa}$
Static safety factor$n_s$$3.9$

Check / assumptions: The energy method uses the diver’s own static deflection ($\delta_{st}=0.10\text{ m}$) as the reference; the board’s 25-kg self-weight is therefore not needed for the impact factor (its constant bending stress adds only a small offset and is neglected, as is common for this energy formulation). The impact factor assumes a rigid, non-rebounding contact and no energy loss.